  (10/09/2008<) FAA issued AD No 2008-18-10 on 09/09/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-90-30 Airplanes - This AD requires a detailed inspection for certain defects of the upper fasteners of the aft mount support fitting of the left and right engines and corrective actions if necessary. |
(10/09/2008) FAA issued Emergency AD No 2008-18-05 on 08/09/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes - This AD requires inspecting the drive assembly of the aft elevator standby loop of the elevator standby cable system for interference between the clevis and bolt of the bellcrank assembly, correct orientation of the pull-pull cable clevis bolt, and excessive freeplay of the bellcrank assembly bearing, and corrective actions if necessary. This AD also requires modifying the pull-pull cable clevis in the drive assembly of the aft elevator standby loop for certain airplanes. |
(09/09/2008) FAA issued AD No 2008-17-17 on 28/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes - This AD requires a one-time inspection of certain fuselage skins at section 41 to find any external doublers that cover the inspection areas and to identify the external doublers that end on a stringer and those that do not, and related investigative and corrective actions if necessary. |
 (09/09/2008) FAA issued Emergency AD No 2008-19-51 on 08/09/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Rolls-Royce Corporation (formerly Allison Engine Company) AE 3007 A series Engines, known to be installed on, but not limited to, Embraer EMB-135 and EMB-145 series aircraft; This AD requires repetitive Eddy Current Inspections (ECI) on High Pressure Turbine (HPT) Stage 2 Wheels. |
 (08/09/2008) Transport Canada issued AD No. CF-2008-29 on 20/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models CL-215-6B11 (CL-215T) aircraft serial numbers 1056 through 1125, and CL-215-6B11 (CL-415) aircraft serial numbers 2001 through 2990; Rudder Lower Torque Tube Upper Bearing Corrosion |
(03/09/2008) FAA issued AD No 2008-17-15 on 28/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -800, and -900 Series Airplanes - This AD requires installing hot short protector (HSP) support brackets and equipment for the fuel quantity indicating system (FQIS) fuel densitometer and other specified actions as applicable. This AD also requires revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness to incorporate AWL No. 28-AWL-07. |
(03/09/2008) FAA issued AD No 2008-17-16 on 28/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10 and DC-10-10F Airplanes, Model DC-10-15 Airplanes, Model DC-10-30 and DC-10-30F (KC-10A and KDC-10) Airplanes, Model DC-10-40 and DC-10-40F Airplanes, Model MD-10-10F and MD-10-30F Airplanes, and Model MD-11 and MD-11F Airplanes - This AD requires modifying the fuel boost pumps. |
(02/09/2008) Transport Canada issued AD No. CF-2008-15R1 on 20/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models CL-600-2B19 series aircraft; AFM Change - Operations in Cold Weather or Icing Conditions - Enhancement to Takeoff Operational Safety Margins |
(02/09/2008) Transport Canada issued AD No. CF-2008-16R1 on 20/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models CL-600-1A11, CL-600-2A12 and CL-600-2B16 series aircraft; AFM Change - Operations in Cold Weather or Icing Conditions - Enhancement to Takeoff Operational Safety Margins |
(28/08/2008) FAA issued Emergency AD No 2008-18-52 on 27/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
MD Helicopters, Inc. (MDHI) Model 500N helicopters, serial numbers (S/N) -001 through -107 with a prefix of "LN," Model 600N helicopters, S/N -003 through -076 with a prefix of "RN," with Yaw Stability Augmentation System (YSAS) adapter tubes, part number (P/N) 500N7218-1, installed; and MD900 helicopters, S/N 900-00008 through 900-00128, with Vertical Stabilizer Control System (VSCS) adapter tubes, P/N 500N7218-1, installed, certificated in any category. Adapter tubes that have a date stamp of August 15, 2008 or later are not included in the applicability of this AD. |
(27/08/2008) FAA issued AD No 2008-16-12 on 05/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200 Series Airplanes - This AD requires repetitive inspections for any wrinkle in certain external skin panels, and for cracking at the fuselage bulkhead shear tie end fastener locations at certain stations of Section 48 of the fuselage; and doing related investigative and corrective actions if necessary. |
(21/08/2008) FAA issued AD No 2008-16-01 on 31/07/2008.
General Electric Co. (GE) CF34-8E Series Turbofan Engines - EASA has decided to not adopt FAA AD 2008-16-01 (see attached letter). |
(20/08/2008) FAA issued AD No 2008-17-03 on 19/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes - This AD requires repetitive inspections to detect cracking of the body station 303.9 frame, and corrective action if necessary. This AD also provides for optional terminating action for the repetitive inspections. |
(19/08/2008) Transport Canada issued AD No. CF-2007-10R1 on 18/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
All Bombardier Inc. Model CL-600-2B19, serial number 7003 thru 7990 and 8000 and subsequent - The AD CF-2007-10 has been revised to enhance the Flaps System performance through the introduction of modified flaps actuators (internal seal), change to temperature limitations, and change to flaps operating speeds. In addition, this AD revision also adds an additional maintenance requirement following a flap fail event and introduction of a cockpit placard associated with new operating limitations. |
(19/08/2008) FAA issued Emergency AD No 2008-17-51 on 14/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Model MD900 helicopters, serial numbers 900-00008 through 900-00128, with part number (P/N) 900C3010045-105 forward directional control cable (control cable), P/N 900C2010582-103 rotating cone control rod, and P/N 9000F2318021 (all dash numbers) tailboom assembly, installed, certificated in any category - This AD requires actions to be complied with before further flight, unless done previously.
NOTE: For showing compliance with paragraph (b) of this FAA AD 2008-17-51, where it says that "The inspection must be done by an inspector qualified under the guidelines established by MIL-STD-410E, ATA Specification 105, AIA-NAS-410, or an FAA-accepted equivalent for qualification standards of NDT inspection/Evaluation Personnel", it should be understood, in the European context, that European Norm 4179 or any equivalent duly accepted by the EU Member State National Aviation Authority are also acceptable guidelines for qualification standards of NDT Inspection / Evaluation Personnel. |
(18/08/2008) FAA issued AD No 2008-11-07 on 29/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes - This AD requires installation of an automatic shutoff system for the center tank fuel boost pumps, and installation of a placard in the airplane flight deck if necessary. This AD also requires revisions to the Limitations and Normal Procedures sections of the airplane flight manual to advise the flightcrew of certain operating restrictions for airplanes equipped with an automated center tank fuel pump shutoff control. This AD also requires a revision to the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness to incorporate AWLs No. 28-AWL-20 and No. 28-AWL-26. This AD also requires replacement of the fuel control panel assembly with a modified part, installation of two secondary pump control relays for the center tank fuel pumps, other specified actions, and concurrent modification of the fuel control panel assembly.
NOTE: Terminating Action for Certain Airplanes - Paragraph (p) of the FAA AD 2008-11-07 allows the installation of TDG Aerospace Inc Universal Fault Interrupter (UFI) in accordance with FAA STC ST01950LA as a terminating action. For European registered aircraft the reference STC is EASA.IM.A.S.02314 and is accepted as the same terminating action. General Note: EASA through the acceptance of the FAA AD grants no approval for the referenced FAA STC: European installations must comply with the EASA validation requirements as specified in the EASA STC: EASA.IM.A.S.02314. |
(18/08/2008) FAA issued AD No 2008-16-11 on 13/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-8-61, DC-8-61F, DC-8-63, DC-8-63F, DC-8-71F, and DC-8-73F Airplanes - For certain airplanes, this AD requires non-destructive testing (NDT) to detect cracks of the door jamb corners of the forward and aft service doors, and doing applicable related investigative and corrective actions. For certain other airplanes, this AD requires inspecting and repairing if necessary or replacing previously repaired door jamb corners with an applicable repair. |
(18/08/2008) FAA issued AD No 2008-03-05 on 05/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes; and Model 767-200 and -300 Series Airplanes; Equipped With Certain Goodrich Evacuation Systems - For certain airplanes, this AD requires replacing the evacuation system shear-pin restraints with new ones. For certain other airplanes, this AD requires an inspection for manufacturing lot numbers; and a general visual inspection of the shear-pin restraints for discrepancies, and corrective actions if necessary. |
(18/08/2008) FAA issued AD No 2008-16-14 on 13/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747- 200C, 747-200F, 747-300, 747-400, 747SR, and 747SP Series Airplanes - This new AD supersedes an existing airworthiness directive (AD) that currently requires inspecting to detect cracking in certain lower lobe fuselage skin lap joints, doing repetitive inspections for cracking at certain fastener locations having countersunk fasteners, and replacing countersunk fasteners with protruding head fasteners at certain fastener locations. This new AD requires replacing a previous highfrequency eddy current (HFEC) inspection method with a new HFEC inspection method, adding a one-time inspection for cracking of certain airplanes, and terminating the adjustment factor for the inspection compliance times based on cabin differential pressure. This AD also requires inspecting additional lap joints. |
 (12/08/2008) ANAC Brazil issued AD No 2005-03-02R1, effective 11/08/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ 170-100 STD, ERJ 170-100 LR, ERJ 170-100 SU, ERJ 170-100 SE, ERJ 170-200 STD, ERJ 170-200 LR and ERJ 170-200 SU aircraft models - Modification of the aircraft maintenance plan. |
(11/08/2008) FAA issued AD No 2008-07-07 on 26/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
DTAA, Inc. [Approval Holder for FAA STC SA1350NM] - Boeing Model 727-200 series Airplanes Equipped with an Auxiliary Fuel Tank System Installed in Accordance with Supplemental Type Certificate SA1350NM. This AD requires deactivating auxiliary fuel tank systems installed in accordance with Supplemental Type Certificate SA1350NM. NOTE: At the time of adoption, EASA does not have information to indicate that DTAA, Inc. STC SA1350NM has been approved or accepted by any EU Member State or associated country for application in Europe. |
(11/08/2008) FAA issued AD No 2008-07-09 on 28/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Southeast Aero-Tek, Inc. [Approval Holder for FAA STC's as listed in AD 2008-07-09] - Boeing Model 727-100, -200, and -200F Series Airplanes; and McDonnell Douglas DC-9 series Airplanes - Equipped With Auxiliary Fuel Tanks Installed in Accordance With Certain Supplemental Type Certificates. This AD requires deactivation of Southeast Aero-Tek, Inc. auxiliary fuel tanks. NOTE: At the time of adoption, EASA does not have information to indicate that the Southeast Aero-Tek, Inc. STC's listed in AD 2008-07-09 have been approved or accepted by any EU Member State or associated country for application in Europe. |
(11/08/2008) FAA issued AD No 2008-12-03 on 04/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Rogerson Aircraft Corporation [Approval Holder for FAA STC's as listed in AD 2008-12-03] - Boeing Model 707 series, 727-100 and -200 series, 737-200, -300, and -400 series, and 767-200 series Airplanes; Airbus (formerly British Aerospace - BAC) One-Eleven series Airplanes; and McDonnell Douglas DC-9 series Airplanes - Equipped With Auxiliary Fuel Tanks Installed in Accordance With Certain Supplemental Type Certificates. This AD requires deactivation of Rogerson Aircraft Corporation auxiliary fuel tanks. NOTE: At the time of adoption, EASA does not have information to indicate that the Rogerson Aircraft Corporation STC's listed in AD 2008-12-03 have been approved or accepted by any EU Member State or associated country for application in Europe. |
(07/08/2008) FAA issued AD No 2008-16-13 on 05/08/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes - This AD requires replacing the pushrods for the left and right elevator tab control mechanisms with new, improved pushrods. |
(04/08/2008) FAA issued AD No 2008-15-03 on 30/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
MD Helicopters, Inc. Model 369A, OH-6A, 369D, 369E, 369F, 369FF, 369H, 369HE, 369HM, and 369HS Helicopters - This AD requires repetitive tap inspections of each tail rotor (T/R) blade abrasion strip. |
(04/08/2008) FAA issued AD No 2008-16-02 on 30/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Hawker Beechcraft Corporation Model 390 Airplanes - This AD requires to repetitively do a post-flight check after every flight and replace or modify (upload software) the stall warning AOA transmitters. |
(30/07/2008) Transport Canada issued AD No. CF-2008-28 on 10/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. DHC-8 Models 102, 103, 106, 201, 202, 301, 311, 314 and 315, Serial Numbers 003 thru 644, and Bombardier Inc. DHC-8 Models 400, 401 & 402, Serial Numbers 4003, 4004, 4006 and 4008 thru 4164 - Spoiler Cable Disconnect Sensing Device - Incorrect Assembly |
(22/07/2008) FAA issued AD No 2008-14-08 on 10/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747- 200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes - This AD requires repetitive inspections for broken or missing fasteners in the single-row hinge fasteners of the forward and aft cargo doors, and related investigative/corrective actions. |
(22/07/2008) FAA issued AD No 2008-14-14 on 17/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400 and 747-400D Series Airplanes - This AD requires a general visual inspection of the power feeder wire bundle of the auxiliary power unit (APU) where it crosses the hydraulic system 4 return tube to determine if parts are installed to provide separation between the wire bundle and hydraulic tube. This AD also requires related investigative and corrective actions if necessary. |
(22/07/2008) FAA issued AD No 2008-15-05 on 21/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400, and -500 Series Airplanes - This AD requires inspecting to determine if certain carriage spindles are installed, repetitive inspections for corrosion and indications of corrosion on affected carriage spindles, and if necessary, related investigative action and corrective action. This AD also provides optional terminating action.
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(22/07/2008) FAA issued AD No 2008-14-15 on 16/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
International Aero Engines AG (IAE) V2500 Series Turbofan Engines - This AD requires removing certain No. 4 bearing oil system components from service at the next shop visit or by an end date determined by the engine model.
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(22/07/2008) FAA issued AD No 2008-14-07 on 10/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Lycoming Engines, Fuel Injected Reciprocating Engines - The FAA is superseding an existing airworthiness directive (AD) for certain fuel
injected reciprocating engines manufactured by Lycoming Engines. That AD currently requires inspection, and replacement if necessary, of externally mounted fuel injector fuel lines. This AD requires the same actions but adds additional engine models and clarifies certain compliance time wording. This AD also exempts engines that have a Maintenance and Overhaul Manual with an Airworthiness Limitations Section that requires inspection and replacement, if necessary, of externally mounted fuel injector lines. |
(22/07/2008) ANAC Brazil issued AD No 2008-03-01R1, effective 14/07/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ 170 aircraft of models -100 STD, -100 LR, -100 SU, -100 SE, -200 STD, -200 LR and -200 SU. - Rework of engines FADEC to return to the installation of software 8Ev5.30. |
(16/07/2008) FAA issued AD No 2008-13-12 on 08/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes - This AD requires various repetitive inspections for cracking of the upper frame to side frame splice of the fuselage, and other specified and corrective actions if necessary. This AD also provides for an optional preventive modification, which terminates the repetitive inspections. |
(16/07/2008) FAA issued AD No 2008-13-25 on 08/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300 and -400 Series Airplanes - This AD requires testing and inspecting a certain web panel of the main wheel well pressure deck to determine the material type and thickness; and related investigative and corrective actions if necessary. |
(16/07/2008) FAA issued AD No 2008-14-13 on 10/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cirrus Design Corporation Model SR20 and SR22 Airplanes - This AD requires you to replace the cabin door rod ends with new parts including a redesigned non-binding hinge pin that replaces the existing pin at the upper door hinge. |
(14/07/2008) FAA issued AD No 2008-13-29 on 08/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes - This AD requires repetitive inspections for cracking of the overwing frames from stations 845 to 905 (MD-87 stations 731 to 791), left and right sides, and corrective actions if necessary. |
(11/07/2008) Transport Canada issued AD No. CF-2008-25 on 03/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Model CL-600-2C10 aircraft, serial numbers 10003 through 10169 and CL-600-2D24 aircraft, serial numbers 15001 through 15030 - This directive mandates the installation of conduit and the addition of spacers to protect fuel tank wiring. |
(11/07/2008) Transport Canada issued AD No. CF-2008-24 on 03/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Model CL-600-2C10 aircraft, serial numbers 10003 through 10169 and CL-600-2D24 aircraft, serial numbers 15001 through 15030 - This directive mandates separation of the high power wiring from the fuel system wiring at the centre fuel tank front spar area and the installation of additional clamping and support for the high power wiring. |
(11/07/2008) Transport Canada issued AD No. CF-2008-27 on 04/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
All models of Viking Air Limited DHC-7 aircraft, Serial Numbers 1 through 113 with Modifications 7/2444 and 7/2445 incorporated - This directive mandates repetitive inspection for proper installation of fluorescent tubes and prohibits installation of non-arc-protected replacement fluorescent lamp ballasts. |
(11/07/2008) FAA issued AD No 2008-13-26 on 08/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Lockheed Model 1329 Series Airplanes - This AD requires determining the part number on the steering cylinder assembly for the nose landing gear (NLG), determining the total flight cycles accumulated on the NLG steering cylinder assembly, repetitively replacing the assembly, inspecting for missing tow turning limit markings, and performing corrective actions if necessary. |
(11/07/2008) FAA issued AD No 2008-13-22 on 02/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400, 747-400D, and 747-400F Series Airplanes – This AD requires replacement of an electronic flight instrument system/engine indicating and crew alerting system (EFIS/EICAS) interface unit (EIU) located on the E2-6 shelf of the main equipment center with a new or modified EIU. |
(09/07/2008) FAA issued AD No 2008-13-21 on 02/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 767-200, -300, and -400ER Series Airplanes - This AD requires an inspection to determine the manufacturer and manufacture date of the oxygen masks in the passenger service units and the flight attendant and lavatory oxygen boxes, as applicable. This AD also requires related investigative/corrective actions if necessary. |
(09/07/2008) FAA issued AD No 2008-13-20 on 02/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes Equipped With Rolls Royce RB211-535E Engines - This AD requires repetitive inspections for signs of damage of the aft hinge fittings and attachment bolts of the thrust reversers, and related investigative and corrective actions if necessary. |
(09/07/2008) FAA issued AD No 2008-14-11 on 08/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200, -200LR, -300, and -300ER Series Airplanes Approved for Extended-Range Twin-Engine Operational Performance Standards (ETOPS) - This AD requires a one-time inspection to determine the part number of the cargo compartment fire suppression filter/regulator. This AD also requires, for certain airplanes, a revision of the ''Maximum Diversion Time in Minutes'' for ETOPS operation specified in the Operations Specifications. For certain airplanes, this AD also provides for optional replacement of the cargo compartment fire suppression filter/regulator, which would allow revision of the ''Maximum Diversion Time in Minutes'' for ETOPS operation specified in the Operations Specifications to restore the airplane's full ETOPS capability. |
(08/07/2008) Transport Canada issued AD No. CF-2008-22 on 24/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models DHC-8-400, DHC-8-401, and DHC-8-402 Serial Numbers 4003, 4004, 4006 and 4008 through 4184 - This directive mandates incorporation of new weight-on-wheels (WOW) and steering harnesses that have a new conduit construction. |
(08/07/2008) Transport Canada issued revised AD No. CF-2007-30R1 on 24/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models DHC-8-400, DHC-8-401 and DHC-8-402 Serial Numbers 4003, 4004, 4006 and 4008 through 4159 - This revision amends the effectivity of paragraph B to be the same as that of paragraph A, since only those aircraft with serial numbers 4003, 4004, 4006 and 4008 through 4159 have ever had elevator overload bungee Part Number (P/N) 289000000 installed. In addition, a typographical error in paragraph B has been corrected; "P/N 289006200" has been amended to read "P/N 289000000". |
(08/07/2008) Transport Canada issued SECURITY-SENSITIVE AD No. CF-2008-26 on 03/07/2008 to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. (De Havilland Canada) Models DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, DHC-8-314 and DHC-8-315, all serial numbers, with Cockpit Door Electronic Strike System installed in accordance with Transport Canada STC SA03-70 Issue 1 or Issue 2. - Cockpit Door Electronic Strike System - Modification.
Note: At the time of publication, EASA records indicate that the application for validation of Jazz Air, Inc. STC SA03-70 Issue 3 is in process. No information is available that indicates that this STC has been previously approved or accepted at Issue 1 or 2 by any EU Member State.
For reasons of security, no PDF version of this AD is posted, but the NAA of the EU Member State of Registry will provide any affected operator with a copy of the AD by FAX upon request. |
(04/07/2008) FAA issued AD No 2008-13-17 on 02/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Hawker Beechcraft Corporation (Type Certificates No. 3A15, No. 3A16, No. A23CE, and No. A30CE Previously Held by Raytheon Aircraft Company) F33 Series and Models G33, V35B, A36, A36TC, B36TC, 95-B55, D55, E55, A56TC, 58, 58P, 58TC, G58, and 77 Airplanes - This AD requires you to replace certain circuit breaker toggle switches with improved design circuit breaker toggle switches. |
(04/07/2008) FAA issued AD No 2008-13-28 on 02/07/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Hartzell Propeller Inc. ( )HC-( )(2,3)Y(K,R)-2 Two- and Three-Bladed Compact Series Propellers - This AD requires initial and repetitive eddy current inspections (ECI), of the area around the lubrication holes of the hub blade sockets. |
(02/07/2008) FAA issued AD No 2008-11-09 on 29/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 727 Airplanes - This AD requires repetitive inspections for any cracking of or damage to the left side and right side flight deck No. 2, No. 4, and No. 5 windows, as necessary, and corrective actions if necessary. |
(01/07/2008) FAA issued AD No 2008-12-16 on 18/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
M7 Aerospace LP SA226 and SA227 Series Airplanes - This AD requires you to inspect electrical wires/components, hydraulic and bleed air tube assemblies at left-hand (LH) and right-hand (RH) inboard wing leading edge/battery box areas, LH/RH wing stations 51.167 to 81.174, and at all feed-through locations into the LH/RH inboard keelson. If chafing/arcing is found, this AD requires you to reposition, repair, and/or replace all chafed electrical wires, components, and hydraulic and bleed air tube assemblies, asrequired. This AD also requires you to reposition the battery lead cables, cover four-gauge wires leaving the battery box with firesleeving and secure with clamps, and protect the battery power cable. |
(01/07/2008) Transport Canada issued AD No. CF-2008-23 on 09/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Pratt & Whitney Canada (P&WC): JT15D-5 engines which are before and include serial number PCE-100411; JT15D-5 engines which are before and include serial number PCE-JA0818 ; All JT15D-5B engines ; All JT15-D-5F engines ; JT15D-5R engines which are before and include serial number PCE-JG0104 ; All JT15D-5 engines converted to model JT15D-5R by incorporation of P&WC Service; Bulletin (SB) 7605 or later revisions. For all affected engines as specified in the applicability section of this directive, unless already accomplished, incorporate P&WC ASB number A7611 Revision No. 1 dated 16 Junes 2008, or later revisions approved by the Chief, Continuing Airworthiness, National Aircraft Certification, Transport Canada. Note: Compliance with P&WC ASB A7611 dated 26 March 2008 prior to the effective date of this directive satisfies the corrective actions requirement of this directive. |
(26/06/2008) FAA issued AD No 2008-13-06 on 25/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cessna Aircraft Company Models 208 and 208B Airplanes - This AD requires you to inspect the left and right wing wire bundle(s) and repair or replace damaged wire. This AD also requires inspecting the wire bundles for correct attachment to the anchor points and correcting any deficient attachments. |
(24/06/2008) FAA issued AD No 2008-11-14 on 29/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10F, DC-10-30F (KC-10A and KDC-10), DC-10-40F, MD-10-10F, and MD-10-30F Airplanes; and Model MD-11 and MD-11F Airplanes - Requiring installation of control cable freeze protection by making certain changes. |
(24/06/2008) FAA issued AD No 2008-13-03 on 19/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400, 747-400D, and 747-400F Series Airplanes - This new AD supersedes an existing airworthiness directive (AD) that currently requires reviewing airplane maintenance records, doing repetitive inspections for cracking of the yaw damper actuator portion of the upper and lower rudder power control modules (PCMs), replacing the PCMs if necessary, and reporting all airplane maintenance records review and inspection results to the manufacturer. This new AD limits the applicability, reduces the initial inspection threshold and repetitive interval, removes the reporting requirement, and requires installation of a secondary retention device for the yaw damper modulating piston. Installation of the secondary retention device terminates the repetitive inspection requirements. |
(23/06/2008) FAA issued AD No 2008-12-05 on 11/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 777 Airplanes - Requiring an inspection to determine the manufacturer and manufacture date of the oxygen masks in the center and outboard passenger service units, crew rests, and lavatory and flight attendant oxygen boxes, as applicable. Also requiring related investigative/corrective actions if necessary |
(19/06/2008) FAA issued AD No 2008-12-17 on 18/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Lockheed Model L-1011 Series Airplanes - This new AD requires an inspection of the fuel level control switch, wiring harnesses, and harness conduit for any visible damage, wear or chafing, broken or missing O-rings, or indications of electrical arcing; an inspection to determine the part number of the wiring harness conduit; and corrective actions if necessary. This new AD also requires replacing certain sleeving with new, improved sleeving over the wiring harness of the fuel level control switch. |
(17/06/2008) Transport Canada issued AD No. CF-2008-20 on 12/06/2008 to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Model CL-600-2B19 aircraft: - serial numbers 7003 through 7067, 7069 through 7939 that have not incorporated the modification of the refuel/defuel shutoff valves according to the original issue of Bombardier Service Bulletin (SB) 601R-28-053; and serial numbers 7989, 7990, and 8000 through 8034 - This directive mandates the modification of the refuel/defuel system |
(17/06/2008) Transport Canada issued AD No. CF-2008-21 on 12/06/2008 to be considered accepted by EASA under provisions of ED Decision 02/2003
All Bombardier Inc. CL-600-2B19 Aircraft – Corrective Actions: 1. Within 30 days after the effective date of this directive, revise the Transport Canada approved maintenance schedule by incorporating the new inspection requirements of Airworthiness Limitations (AWL) Number 57-21-161, as introduced by Temporary Revision (TR) 2B-2136 of the Canadair Regional Jet Maintenance Requirement Manual (MRM), Appendix B, “Airworthiness Limitations”. 2. Initial compliance with the new AWL task shall be carried out in accordance with the applicable Phase-In Schedule detailed in TR 2B-2136 of the MRM. |
(17/06/2008) FAA issued AD No 2008-16-18 R1 on 13/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes - The existing AD currently requires installing a warning placard on the TAWS/RMI and revising the Limitations section of the airplane flight manual (AFM). The existing AD also requires installing upgraded software in the TAWS/RMI. This new AD allows installing later revisions of the software described in the existing AD. |
(16/06/2008) Transport Canada issued AD No. CF-2005-15R1 on 06/06/2008 to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models DHC-8-400, DHC-8-401 and DHC-8-402, Serial Numbers 4003 through 4154 - Corrective Action: A. Cleaning of Pitot Static Probe Drain Hole, B. Cleaning of Pitot Lines, C. Modification of Pitot Static System |
(12/06/2008) FAA issued AD No 2008-12-04 on 11/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes - Requiring various repetitive inspections to detect cracks along the chemically milled steps of the fuselage skin or missing or loose fasteners in the area of the preventative modification or repairs, replacement of the time-limited repair with the permanent repair if applicable, and applicable corrective actions if necessary, which would end certain repetitive inspections. |
(12/06/2008) FAA issued AD No 2008-09-18 on 02/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Taylorcraft, Inc. Models A, B, and F Series Airplanes - Requiring you to inspect the wing strut attach fittings for corrosion or cracks and requiring repair or replacement if corrosion or cracks are found. |
(11/06/2008) FAA issued AD No 2008-11-15 on 29/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes; Model DC-9-10 Series Airplanes; Model DC-9-20 Series Airplanes; Model DC-9-30 Series Airplanes; Model DC-9-40 Series Airplanes; Model DC-9-50 Series Airplanes; Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) Airplanes; Model MD-88 Airplanes; and Model MD-90-30 Airplanes - Revising the FAA-approved maintenance program, or the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness, as applicable, to incorporate new AWLs for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. |
(05/06/2008) FAA issued AD No 2008-11-18 on 02/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cirrus Design Corporation Model SR20 Airplanes - Requiring you to perform an inspection and replacement as necessary of the heat exchanger. |
(04/06/2008) FAA issued AD No 2008-11-06 on 29/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes - Installing an additional support bracket for the gray water drain hose; replacing the screw of the support bracket with a new screw for the potable water supply hose; installing a spacer; doing a detailed inspection to detect interference or wear damage on hoses, lines and/or cables; and doing corrective actions if necessary. |
(04/06/2008) ANAC Brazil issued AD No 2008-05-01, effective 13/06/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer EMB-120 aircraft models of serial numbers (S/N) 120001 to 120359 - Revision of the Airplane Flight Manual (AFM); inspection of fuel booster pumps electrical harness installed on left (LH) and right (RH) tanks; and installation of clamps on tank structure and tie-raps to attach these electrical harnesses. |
(04/06/2008) FAA issued AD No 2008-11-17 on 02/06/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Air Tractor, Inc. AT-200, AT-300, AT-400, AT-500, AT-600, and AT-800 Series Airplanes - Requiring the installation of a modified skid plate kit or modification to skid plate kits that are already installed, including those already installed on AT-402B, AT-502B, AT-602, and AT-802A series airplanes during production. |
(04/06/2008) FAA issued AD No 2008-11-13 on 29/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200, -200LR, -300, and -300ER Series Airplanes - Revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness by incorporating new limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements.
This AD also requires the initial performance of certain repetitive inspections specified in the AWLs to phase in those inspections, and repair if necessary. |
(04/06/2008) FAA issued AD No 2008-11-02 on 21/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Lockheed Model L-1011 Series Airplanes - Revising the FAA-approved maintenance program by incorporating new airworthiness limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the accomplishment of certain fuel system modifications, the initial inspections of certain repetitive fuel system limitations to phase in those inspections, and repair if necessary. |
(02/0 6/2008) Transport Canada issued revised AD No. CF-2008-17R1 on 26/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Eurocopter Canada Ltd. (formerly MBB Canada Ltd.) Model BO 105 LS-A3 helicopters - Tension-Torsion Straps (TTS) Failure |
(30/05/2008) Transport Canada issued revised AD No. CF-2004-21R3 on 23/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bell Helicopter Textron Canada (BHTC) Helicopters, Models 222, 222B, 222U, 230, and 430. |
(30/05/2008) FAA issued AD No 2008-11-08 on 29/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes - Requiring repetitive inspections for any cracking of or damage to the left side and right side flight deck No. 2, No. 4, and No. 5 windows, as necessary, and corrective actions if necessary. |
(30/05/2008) FAA issued AD No 2008-09-04 on 22/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model DC-8-50 Series Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-60 Series Airplanes; Model DC-8-60F Series Airplanes; Model DC-8-70 Series Airplanes; and Model DC-8-70F Series Airplanes - Revising the FAA-approved maintenance program to incorporate new airworthiness limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. |
(28/05/2008) Transport Canada issued AD No. CF-2008-19 on 08/05/2008 , to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models: CL-600-2C10, serial numbers 10003 – 10216 ; CL-600-2D15 and CL-600-2D24, serial numbers 15001 – 15040 - Water Ingress into the Cockpit |
(28/05/2008) Transport Canada issued AD No. CF-2008-18 on 09/05/2008 , to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models: CL-600-1A11 – Serial Numbers 1004 through 1085 ; CL-600-2A12 – Serial Numbers 3001 through 3066 ; CL-600-2B16 – Serial Numbers 5001 through 5194 ; CL-600-2B16 – Serial Numbers 5301 through 5635 - This directive mandates the amendment of the AFM procedures, in addition to checking the part numbers and serial numbers of the installed wing anti-ice piccolo ducts and replacing them as necessary. |
(28/05/2008) Transport Canada issued AD No. CF-2008-11R1 on 09/05/2008 , to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. DHC-8 aircraft, Models 400, 401 and 402, serial numbers 4001, 4003 through 4176 - Wing to Fuselage Attachment Joints - Barrel Nut Cracking - This revision mandates the removal of the affected barrel nuts and the application of the CIC in accordance with the ASB A84-57-19, Revision “B”, issued 06 March 2008. |
(22/05/2008) FAA issued AD No 2008-11-03 on 21/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, and -200C Series Airplanes - Revising the FAA-approved maintenance inspection program to include inspections that will give no less than the required damage tolerance rating for each structural significant item (SSI), doing repetitive inspections to detect cracks of all SSIs, and repairing cracked structure. |
(22/05/2008) FAA issued AD No 2008-11-04 on 21/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes - Requiring repetitive inspections for cracking in and around the upper and lower hinge cutouts of the forward entry and forward galley service doorways, and corrective actions.
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(22/05/2008) ANAC Brazil issued AD No 2007-03-01R1, effective 09/06/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ 170-100 LR, ERJ 170-100 STD and ERJ 170-100 SU aircraft models, as identified in Embraer Service Bulletins (SB) Nos. 170-21-0017 Rev. 01, dated 15 Feb. 2006, and 170-21-0018 Rev. 03, dated 10 Mar. 2008 - Inspection, repair and replacement, if necessary, of the smoke seal of the aft avionics compartment. |
(22/05/2008) ANAC Brazil issued AD No 2006-05-04R1, effective 09/06/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ 170-100 LR, ERJ 170-100 STD, ERJ 170-100 SE, ERJ 170-100 SU, ERJ 170-200 LR, ERJ 170-200 STD and ERJ 170-200 SU aircraft models in operation - Visual inspection of cargo doors prior to each departure; removal of the cover plate fromthe cargo doors surround trim lining; rework of cargo doors surround trim liner; and, inspection of fore and aft cargo doors lateral locking mechanism. |
(21/05/2008) FAA issued AD No 2008-10-06 on 08/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400, -400D, and -400F Series Airplanes - Revising the FAA-approved maintenance program by incorporating new airworthiness limitations (AWLs) for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the initial inspection of certain repetitive AWL inspections to phase in those inspections, and repair if necessary. |
(21/05/2008) FAA issued AD No 2008-10-07 on 08/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP Series Airplanes - Revising the FAA-approved maintenance program by incorporating new airworthiness limitations (AWLs) for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the initial inspection of certain repetitive AWL inspections to phase in those inspections, and repair if necessary |
(21/05/2008) FAA issued AD No 2008-10-11 on 08/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes - Revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness by incorporating new limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the initial inspection of certain repetitive AWL inspections to phase-in those inspections, and repair if necessary. |
(21/05/2008) FAA issued AD No 2008-10-09 on 08/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes - Revising the FAA-approved maintenance program to incorporate new airworthiness limitations (AWLs) for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the initial inspection of a certain repetitive AWL inspection to phase in that inspection, and repair if necessary. |
(21/05/2008) FAA issued AD No 2008-10-10 on 08/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes - Revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness by incorporating new limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the initial inspection of a certain repetitive AWL inspection to phase in that inspection, and repair if necessary. |
(20/05/2008) Transport Canada issued AD No. CF-2007-17 on 09/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Eurocopter Canada Ltd. Model BO 105 LS-A3 helicopters – Tension-Torsion Straps (TTS) Failure
NOTE: Model BO 105 LS-A3 helicopters that have been modified in accordance with LBA STC (EMZ) 0654/3058 must continue to comply with the requirements of existing LBA AD 1999-290/3. |
(19/05/2008) FAA issued AD No 2008-09-13 on 02/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400, and -500 Series Airplanes - Revising the FAA-approved maintenance inspection program to include inspections that will give no less than the required damage tolerance rating for each structural significant item (SSI), doing repetitive inspections to detect cracks of all SSIs, and repairing cracked structure. |
(19/05/2008) FAA issued AD No 2008-09-14 on 02/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, -800 and -900 Series Airplanes - Inspecting ground blocks GD261 and GD264 for corrosion, measuring the electrical bond resistance between the ground blocks and the airplane structure, separating the ground wires for the fuel boost pump circuit between ground blocks GD261 and GD264, and doing corrective actions. |
(19/05/2008) FAA issued AD No 2008-09-15 on 02/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes - Requiring repetitive inspections for any cracking of or damage to the left side and right side flight deck No. 2, No. 4, and No. 5 windows and corrective actions. |
(16/05/2008) Transport Canada issued AD No. CF-2007-13R1 on 13/05/2008 , to be considered accepted by EASA under provisions of ED Decision 02/2003
Bell Helicopter Textron Canada (BHTC), Models 206B series (including those converted from 206A) - Power Turbine RPM Steady State Operation Avoidance
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(16/05/2008) FAA issued AD No 2008-10-12 on 08/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Air Tractor, Inc. AT-400, AT-500, AT-600, and AT-800 Series Airplanes - This AD would retain the inspection actions of AD 2007-13-17 for Model AT-602, AT-802, and AT-802A airplanes, including the compliance times and effective dates; establish new inspection actions for the AT-400 and AT-500 series airplanes; incorporate a mandatory terminating action for all airplanes; and terminate the reporting requirement of AD 2007-13-17. |
(15/05/2008) FAA issued AD No 2008-09-20 on 08/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-200F, 747-300, 747-400, and 747-400D Series Airplanes - Requiring a detailed inspection to detect missing fasteners from the shear clip at a certain stub frame to auxiliary sill joint, and applicable related investigative and corrective actions. |
(14/05/2008) FAA issued AD No 2008-10-04 on 08/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Sikorsky Aircraft Corporation Model S-61A, S-61D, S-61E, and S-61V Helicopters - Installing an electric chip detector on each engine and an on-board chip detector annunciation system. The AD also requires revising the Rotorcraft Flight Manual (RFM) to add procedures for crew response to the illumination of an onboard chip detector warning light. This AD also requires testing the engine chip detector system at specified intervals. |
(14/05/2008) FAA issued AD No 2008-09-10 on 28/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Air Tractor, Inc. Models AT-300, AT-301, AT-302, AT-400, and AT-400A Airplanes - This AD retains the wing spar lower cap replacement and reporting requirements from AD 2003-06-01 and adds a repetitive eddy-current inspection. FAA issued this AD to detect and correct cracks in the wing centerline splice joint. If not detected and corrected, these cracks could result in the wing separating from the airplane during flight. |
(14/05/2008) FAA issued AD No 2008-10-02 on 02/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series Airplanes - Requiring you to inspect the alternate static air source selector valve to assure that the part number identification placard does not obstruct the alternate static air source selector valve port. If the part number identification placard obstructs the port, this AD requires you to remove the placard, assure that the port is unobstructed, and report to the FAA if obstruction is found. |
(07/05/2008) FAA issued AD No 2008-09-07 on 23/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes and Model 767-200, 767-300, and 767-300F Series Airplanes - Revising the Limitations section of the airplane flight manual to advise the flight crew of procedures to follow to ensure that a fuel filter impending bypass condition due to gross fuel contamination is detected in a timely manner |
(07/05/2008) FAA issued AD No 2008-09-11 on 02/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200, -300, and -300ER Series Airplanes - Requiring a one-time inspection to determine the material of the forward and aft gray water drain masts. For airplanes having composite gray water drain masts, this AD also requires installation of a bonding jumper between a ground and the clamp on the tube of the forward and aft gray water composite drain masts. |
(07/05/2008) FAA issued AD No 2008-09-17 on 02/05/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, and MD-10-10F Airplanes - Requiring repetitive inspections for the presence of stray nickel or chrome plating deposits on the air filler valve bore of certain main landing gear (MLG) shock strut cylinders, and if necessary, related investigative and corrective actions. Doing the corrective action terminates the repetitive inspections. |
(06/05/2008) FAA issued AD No 2008-05-01 on 28/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
General Electric Company CF34-8C1/-8C5/-8C5B1/-8E5/-8E5A1, and CF34-10E Series Turbofan Engines - Requiring a onetime test of the FMU for a miswired (reversed polarity) condition of the input wires to the overspeed solenoid. |
(28/04/2008) FAA issued AD No 2008-08-11 on 28/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
MD Helicopters, Inc. Model MD900 Series Helicopters - Modifying the pilot and co-pilot dual-control directional pedal assemblies, or the pilot single-control directional pedal assembly (directional control pedal assembly) |
(23/04/2008) FAA issued AD No 2008-08-26 on 21/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 767 Airplanes - Requiring a one-time inspection to determine the material of the forward and aft gray water drain masts. For airplanes having composite gray water drain masts, this AD also requires installation of a ground bracket and a bonding jumper between a ground bracket and the clamp on the tube of the forward and aft gray water composite drain masts |
(23/04/2008) FAA issued AD No 2006-12-10R1 on 22/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400 Series Airplanes - This new AD retains all the requirements of the existing AD (Inspecting the support bracket of the crew oxygen cylinder installation to determine the manufacturing date marked on the support, and performing corrective action if necessary) and expands the applicability of the existing AD to include certain airplanes that are not on the U.S. Register. |
(23/04/2008) FAA issued AD No 2008-09-05 on 22/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes - Inspecting the trunnion fork assembly of the wing landing gears to determine the part number and serial number and to determine the category of the trunnion fork assemblies. For certain airplanes, this AD also requires, if necessary, various inspections to detect discrepancies of the trunnion fork assemblies, related investigative/corrective actions, and a terminating action. |
(23/04/2008) FAA issued AD No 2008-08-25 on 21/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400F and -400 Series Airplanes - Installing drains and drain tubes to eliminate water accumulation in the dripshield above the M826 Card File in the main equipment center |
(22/04/2008) FAA issued AD No 2008-08-24 on 21/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes - Replacing the drain tube assemblies and support clamps on the aft fairing of the engine struts. |
(22/04/2008) FAA issued AD No 2008-08-23 on 21/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-200C Series Airplanes - Revising the FAA-approved maintenance inspection program to include inspections that will give no less than the required damage tolerance rating for each structural significant item (SSI), doing repetitive inspections to detect cracks of all SSIs, and repairing cracked structure |
(22/04/2008) FAA issued AD No 2008-08-22 on 21/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes - Requiring a one-time inspection to determine the material of the forward and aft gray water drain masts. For airplanes having composite gray water drain masts, this AD requires installation of a bonding jumper between a ground and the clamp on the tube of the forward and aft gray water composite drain masts |
(22/04/2008) FAA issued AD No 2008-08-17 on 21/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Kelly Aerospace Power Systems Turbochargers - Requiring a onetime visual inspection of suspect turbochargers for an excessive gap between the turbocharger turbine housing flange and the exhaust tube flange, and replacement of turbochargers that fail the gap inspection. |
(21/04/2008) FAA issued AD No 2008-08-02 on 14/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 727 Airplanes - Requiring repetitive inspections for cracking or corrosion of the threaded end of the lower segment of the main landing gear (MLG) side strut, and corrective actions if necessary. Also requiring prior or concurrent inspection for cracking or corrosion of the threads and thread relief area of the lower segment, corrective action if necessary, and re-assembly using corrosion inhibiting compound. |
(17/04/2008) FAA issued AD No 2008-06-28 revised on 14/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100) - Requiring a check of the maintenance records and inspection of the PFD (if necessary) to determine if an affected serial number PFD is installed. If an affected serial number PFD is installed, this AD requires you to incorporate information that limits operation when certain conditions for the PFD or backup instruments exist. |
(16/04/2008) FAA issued AD No 2008-08-10 on 14/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes - For certain airplanes, replacing the outboard stabilizing fitting and certain adjacent components of the main landing gear (MLG) support beam. Also requiring repetitive inspections for discrepancies of the outboard stabilizing fitting, walking beam hanger, and rear spar attachment, and corrective actions if necessary. For certain airplanes, this AD provides an alternative one-time inspection of the outboard stabilizing fitting for discrepancies, and corrective actions if necessary, which would extend the compliance time for the replacement of the outboard stabilizing fitting. For certain other airplanes, this AD also requires performing a torque check of the aft pin of the outboard stabilizing fitting, and corrective actions if necessary. |
(16/04/2008) FAA issued AD No 2008-08-01 on 14/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0 - The FAA is superseding three existing airworthiness directives (ADs) for McCauley Propeller Systems which currently require fluorescent penetrant inspections (FPI) and eddy current inspections (ECI) of propeller blades for cracks, and if any crack indications are found, removing the blade from service. This AD requires the same initial inspections, but extends the compliance times and intervals, adds repetitive inspections, and mandates a life limit for the blades. |
(16/04/2008) FAA issued AD No 2008-08-14 on 14/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO Series Reciprocating Engines, Teledyne Continental Motors (TCM) TSIO-360-RB Reciprocating Engines, and Superior Air Parts, Inc. IO-360 Series Reciprocating Engines With Certain Precision Airmotive LLC RSA-5 and RSA-10 Series Fuel Injection Servos - Amendment adopting emergency airworthiness directive (AD) 2008-06-51 |
(16/04/2008) FAA issued AD No 2008-08-12 on 14/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes - Requiring repetitive inspections of the anchor tab of the bulkhead seal assemblies of the wing thermal anti-ice (TAI) system for cracks at certain outboard stations of the left and right wings, and corrective action if necessary. Also providing optional terminating action for the repetitive inspections
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(16/04/2008) FAA issued AD No 2008-08-08 on 14/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes - Requiring an inspection to determine the manufacturer and manufacture date of the oxygen masks in the passenger service units and the lavatory and attendant box assemblies, and corrective action |
(07/04/2008) FAA issued AD No 2008-07-10 on 07/04/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Hawker Beechcraft Corporation Models B200, B200GT, B300, and B300C Airplanes - Requiring you to fabricate and install a placard incorporating information that limits operation when there is known or forecast icing and requiring you to replace a section of the pneumatic supply tube for the tail deice system with a new tube of a different material |
(02/04/2008) FAA issued AD No 2008-05-11 on 04/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Alexandria Aircraft, LLC Models 17-30, 17-31, 17-30A, 17-31A, and 17-31ATC Airplanes - This new AD supersedes AD 76-23-03 R1. Reducing the exhaust system inspection interval; requiring a more detailed inspection of the muffler; and requiring replacement, reconditioning, or repair of the exhaust system if cracks or defects are found. Also requiring P-lead rerouting. |
(28/03/2008) FAA issued AD No 2008-06-29 on 24/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400, and -500 Series Airplanes - Requiring repetitive inspections of the downstop assemblies on the main tracks of the No. 2, 3, 4, and 5 slats and the inboard track of the No. 1 and 6 slats to verify if any parts are missing, damaged, or in the wrong order. Also requiring other specified actions, and related investigative and corrective actions.
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(28/03/2008) FAA issued AD No 2008-06-21 on 19/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10 and DC-10-10F Airplanes, Model DC-10-15 Airplanes, Model DC-10-30 and DC-10-30F (KC-10A and KDC-10) Airplanes, Model DC-10-40 and DC-10-40F Airplanes, Model MD-10-10F and MD-10-30F Airplanes, and Model MD-11 and MD-11F Airplanes - Revising the FAA-approved maintenance program, or the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness, as applicable, to incorporate new AWLs for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. For certain airplanes, also requiring the initial accomplishment of a certain repetitive AWL inspection to phase in that inspection, and repair. |
(28/03/2008) FAA issued AD No 2008-06-23 on 18/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-8-55, DC-8F-54, and DC-8F-55 Airplanes; and Model DC-8-60, DC-8-70, DC-8-60F, and DC-8-70F Series Airplanes - Re-defining and more clearly describing the optional actions for extending the repetitive inspection intervals. |
(20/03/2008) FAA issued AD No 2008-06-24 on 19/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400, and -500 Series Airplanes - Requiring an inspection to determine the manufacturer and manufacture date of the oxygen masks in the passenger service unit and the lavatory and attendant box assemblies, corrective action, and other specified action. |
(19/03/2008) FAA issued AD No 2008-06-19 on 18/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Honeywell International Inc. ATF3-6 and ATF3-6A Series Turbofan Engines - Removing from service those LPC aft shafts and installing a serviceable LPC aft shaft |
(17/03/2008) FAA issued AD No 2008-05-17 on 12/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
MD Helicopters, Inc. Model 600N Helicopters - Requiring interim initial and repetitive inspections of tailboom parts, installing six inspection holes in the aft fuselage skin panels, installing tailboom attachment bolt washers, modifying both access covers, and replacing broken attachment bolts. Modifying the fuselage aft section as an optional terminating action. Modifying the fuselage aft section within the next 24 months to strengthen the tailboom attachment fittings and upper longerons. |
(14/03/2008) FAA issued AD No 2008-06-14 on 13/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing 757-200, -200CB and -200PF series aircraft – Fuselage Bonded Skin Panels and Tear Straps – Inspection/Repair |
(13/03/2008) FAA issued AD No 2008-06-06 on 12/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 767 Airplanes - Requiring the following actions for the drive mechanism of the horizontal stabilizer: Repetitive detailed inspections for discrepancies and loose ball bearings; repetitive lubrication of the ballnut and ballscrew; repetitive measurements of the freeplay between the ballnut and the ballscrew; and corrective action. Also requiring initial and repetitive inspections of the ballscrew-to-ballnut freeplay for certain airplanes. |
(13/03/2008) FAA issued AD No 2008-06-03 on 12/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, -800 and -900 Series Airplanes;and Model 757-200, -200PF, -200CB, and -300 Series Airplanes Requiring inspection to determine if certain motor-operated shutoff valve actuators for the fuel tanks are installed, and related investigative and corrective actions. This AD also requires revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness to incorporate AWL No. 28-AWL-21, No. 28-AWL-22, and No. 28-AWL- 24 (for Model 737-600, -700, -700C, -800 and -900 series airplanes); and No. 28-AWL-23, No. 28-AWL-24, and No. 28-AWL-25 (for Model 757-200, -200PF, -200CB, and -300 series airplanes) |
(13/03/2008) FAA issued AD No 2008-06-09 on 12/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-200 Series Airplanes - Requiring repetitive inspections to detect cracking of the support fittings of the Krueger flap actuators, and corrective actions. This AD also requires eventual replacement of any existing aluminum support fitting on each wing with a steel fitting, and modification of the aft attachment of the actuator. Doing these actions terminates the repetitive inspection requirements. |
(13/03/2008) FAA issued AD No 2008-05-09 on 04/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cessna Aircraft Company 172, 182, and 206 Series Airplanes - Removing the crew seats, modifying the seat base/back attach brackets, and reinstalling the seats of the affected airplanes |
(13/03/2008) FAA issued AD No 2008-04-21 on 28/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400, and -500 Series Airplanes - Requiring repetitive inspections for cracking of the body buttock line (BBL) 0.07 floor beam between body station (BS) 651 and BS 676 and between BS 698 and BS 717, and related investigative and corrective actions. Providing optional terminating action for the repetitive inspections. |
(10/03/2008) FAA issued AD No 2008-04-11 on 22/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 707 Series, 720 and 720B Series Airplanes; Requiring revising the FAA-approved maintenance program by incorporating new airworthiness limitations (AWLs) for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the initial inspection of a certain repetitive AWL inspection to phase in that inspection, and repair |
(10/03/2008) FAA issued AD No 2008-04-10 on 22/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 727 Series Airplanes; Requiring revising the FAA-approved maintenance program by incorporating new airworthiness limitations (AWLs) for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88 requirements. This AD also requires the initial inspection of a certain repetitive AWL inspection to phase in that inspection, and repair. |
(06/03/2008) FAA issued AD No 2008-05-05 on 04/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, 737-700, 737-700C, 737-800, and 737-900 Series Airplanes - Requiring an inspection of the vertical fin lugs, skin, and skin edges for discrepancies; an inspection of the flight control cables, fittings, and pulleys in section 48 for signs of corrosion; an inspection of the horizontal stabilizer jackscrew, ball nut, and gimbal pins for signs of corrosion; and corrective actions |
(06/03/2008) FAA issued AD No 2008-05-06 on 04/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes - Requiring repetitive inspections for fatigue cracking in the longitudinal floor beam web, upper chord, and lower chord located at certain body stations, and repair |
(06/03/2008) FAA issued AD No 2008-05-03 on 04/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, -100B, -100B SUD, -200B, -200C, -200F, -300, 747SP, and 747SR Series Airplanes Powered by General Electric (GE) CF6-45/50 and Pratt & Whitney (P&W) JT9D-70, JT9D-3 or JT9D-7 Series Engines - Requiring repetitive inspections to find cracks and broken fasteners of the rear engine mount bulkhead of the inboard and outboard nacelle struts, and repair if necessary. For certain airplanes, mandating a terminating modification for certain inspections of the inboard and outboard nacelle struts. |
(05/03/2008) FAA issued AD No 2008-05-10 on 03/03/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 757-200, -200PF, and -200CB Series Airplanes - Requiring repetitive inspections of the shim installation between the vertical flange and bulkhead, and repair if necessary. Also requiring, for certain airplanes, an inspection for cracking of the four critical fastener holes in the horizontal flange, and repair if necessary. This new AD retains the requirements of the existing AD, and requires that the existing action be performed on airplanes without conclusive records of previous inspections. |
(04/03/2008) FAA issued AD No 2007-26-04 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes - Requiring repetitive detailed and high-frequency eddy current inspections for cracking around the heads of the fasteners on the forward fastener row of certain areas of the station (STA) 259.5 circumferential butt splice, and repair if necessary. Also requiring a preventive modification, which eliminates the need for the repetitive inspections. |
(03/03/2008) FAA issued AD No 2008-04-06 on 22/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 707 Airplanes and Model 720 and 720B Series Airplanes - Requiring repetitive inspections for any cracking of or damage to the left side and right side flight deck No. 2, No. 4, and No. 5 windows, as necessary, and corrective actions |
(03/03/2008) FAA issued AD No 2008-04-09 on 22/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Taylorcraft A, B, and F Series Airplanes - Requiring you to do an initial visual inspection of the left and right wing front and aft lift struts for cracks and corrosion and replace any cracked strut or strut with corrosion that exceeds certain limits. If the strut is replaced with an original design vented strut, AD 2007-16-14 requires you to repetitively inspect those struts thereafter. |
(03/03/2008) FAA issued AD No 2008-04-12 on 28/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 767-200, -300, -300F, and -400ER Series Airplanes - Reworking the surface of the ground stud bracket of the left and right transformer rectifier units (TRUs) and the airplane structure mounting surface, and measuring the resistance from the bracket to the structure and the ground lugs to the bracket using a bonding meter. Installation of a new ground stud bracket using faying surface bonding. |
(03/03/2008) FAA issued AD No 2008-03-20 on 11/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400, and -500 Series Airplanes - Modifying the doormounted escape system of the forward right side door slide compartment. |
(28/02/2008) Transport Canada issued AD No. CF-2008-05R1 on 27/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models DHC-8-401 and DHC-8-402 (Model DHC-8-400 is not validated in EU) aircraft, serial numbers 4001, 4003, 4004 and 4006 through 4081; Elevator Centering Torsion Spring Failure |
(26/02/2008) Transport Canada issued AD No. CF-2008-13 on 14/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models DHC-8-401 and DHC-8-402 (Model DHC-8-400 is not validated in EU) aircraft, serial numbers 4003, 4004, 4006 and 4008 through 4129 inclusive; Spoiler Cable Disconnect Sensing Circuit - Modification |
(25/02/2008) Transport Canada issued AD No. CF-2008-12 on 08/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models CL-600-1A11, CL-600-2A12 and CL-600-2B16 series aircraft; AFM Change - Stick Pusher Capstan Shaft Failure – AMM Chapter 5 Airworthiness Limitations |
(22/02/2008) FAA issued corrected AD No 2004-07-22R1 on 14/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes - One of the Boeing ADs requires revising the FAA-approved maintenance inspection program to include inspections that will give no less than the required damage tolerance rating for each structural significant item, and repair of cracked structure. The other Boeing AD requires implementing a corrosion prevention and control program |
(22/02/2008) FAA issued corrected AD No 90-25-05R1 on 14/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes - necessary. One of the Boeing ADs requires revising the FAA-approved maintenance inspection program to include inspections that will give no less than the required damage tolerance rating for each structural significant item, and repair of cracked structure. The other Boeing AD requires implementing a corrosion prevention and control program. |
(21/02/2008) FAA issued AD No 2008-02-05 on 23/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200 and -300 Series Airplanes Equipped With Rolls-Royce RB211-TRENT 800 Series Engines - Revising the airplane flight manual to provide the flightcrew with new ground procedures for shedding core ice during long taxi periods in freezing fog with visibility of 300 meters or less. For airplanes unable to perform the shedding procedure after prolonged taxiing in freezing fog with visibility of 300 meters or less, this AD requires certain investigative and corrective actions. |
 (19/02/2008) The State of Israel CAA issued AD No 85-001R3 on 18/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Gulfstream Aerospace L.P. (GALP; formerly Israel Aircraft Industries) models 1121/1121A/1121B/1123/1124/1124A, all serial numbers. Horizontal Stabilizer Aft Spar Splice Fitting (Hinge Assembly) Part Number 453005-501 Inspection/Replacement |
(19/02/2008) Transport Canada issued AD No. CF-2007-25R1 on 13/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Pratt & Whitney Canada Model PW305A and PW305B Engines - High Pressure Compressor (HPC) Drum Rotor Cracks |
(18/02/2008) FAA issued AD No 2008-03-12 on 05/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-50, -60, -60F, -70, and -70F Series Airplanes; Model DC-9-10, -20, -30, - 40, and -50 Series Airplanes; Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) Airplanes; and Model MD-88 Airplanes Requiring an initial general visual or dye penetrant inspection, repetitive dye penetrant inspections, and replacement, as necessary, of the rudder pedal bracket. For certain airplanes, replacing the rudder pedal bracket assemblies with new, improved parts, which would terminate the repetitive inspections. For certain airplanes, requiring initial inspection at a reduced threshold, removing an inspection option, and lengthening the repetitive inspection intervals. |
(18/02/2008) ANAC Brazil issued AD No 2006-11-01R2, effective 25/02/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-190 aircraft models in operation and equipped with low pressure check valves (LPCV) Hamilton Sundstrand part number (P/N) 1001447-3. - Replacement of the right hand (RH) and left hand (LH) LPCVs; and revision of the approved maintenance plan. |
(18/02/2008) ANAC Brazil issued AD No 2006-05-05R1, effective 25/02/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-170 aircraft models in operation, equipped with Air Data Smart Probes (ADSP) P/N 2015G2H2H-4( ), 2015G2H2H-5( ), 2015G2H2H-6( ) or 2015G2H2H-7( ). - Inspection of the pitot drain hole and removal of moisture in the ADSP pressure lines. |
(18/02/2008) ANAC Brazil issued AD No 2008-01-02, effective 25/02/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-190 aircraft models of serial numbers 19000004, 19000006 thru 19000028 and 19000030 thru 19000039. - Rework and inspection of wings lower skin stringers. |
(18/02/2008) ANAC Brazil issued AD No 2008-01-04, effective 03/03/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-190 aircraft models in operation, of serial numbers 19000002, 19000004 thru 19000132 and 19000135. - Inspection of the forward and rearward doors emergency evacuation slide packs and, if applicable, removal of the tie-down straps |
(18/02/2008) ANAC Brazil issued AD No 2005-09-03R2, effective 25/02/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-170 aircraft models in operation and equipped with low pressure check valves (LPCV) Hamilton Sundstrand part number (P/N) 1001447-3. Replacement of the right hand (RH) and left hand (LH) LPCVs; and revision of the approved maintenance plan. |
(18/02/2008) ANAC Brazil issued AD No 2006-05-08R1, effective 25/02/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-190 aircraft models in operation, equipped with Air Data Smart Probes (ADSP) P/N 2015G2H2H-4( ), 2015G2H2H-5( ), 2015G2H2H-6( ) or 2015G2H2H-7( ). - Inspection of the pitot drain hole and removal of moisture in the ADSP pressure lines. |
(18/02/2008) ANAC Brazil issued AD No 2008-01-03, effective 03/03/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-170 aircraft models in operation, of serial numbers 17000002, 17000004 thru 17000013, and 17000015 thru 17000196. Inspection of the forward and rearward doors emergency evacuation slide packs and, if applicable, removal of the tie-down straps. |
(14/02/2008) Transport Canada issued AD No. CF-2008-07 on 25/01/2008 , to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier CL-600-2C10, CL-600-2D15 and CL-600-2D24 aircraft, all serial numbers - Fuel System Safety - Introduction of Critical Design Configuration Control Limitations |
(14/02/2008) Transport Canada issued AD No. CF-2008-09 on 05/02/2008 , to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Model:CL-600-2B19 - Serial numbers 7305 through 7990 and 8000 and subsequent. Air-Driven Generator - Internal Wiring |
(14/02/2008) Transport Canada issued AD No. CF-2008-10 on 05/02/2008 , to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models: CL-600-2C10 - Serial numbers 10004 and subsequent.CL-600-2D15 and CL-600-2D24 - Serial numbers 15002 and subsequent. Air-Driven Generator - Internal Wiring |
(08/02/2008) FAA issued AD No 2008-03-16 on 05/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cirrus Design Corporation Models SR20 and SR22 Airplanes - Requiring you to inspect the rudder, aileron, and rudder-aileron interconnect rigging; correct any out-of-rig condition; replace the attaching hardware for the rudder-aileron interconnect arm; and report any out-of-rig condition found. |
(07/02/2008) FAA issued AD No 2008-03-10 on 24/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cessna Aircraft Company Models 525, 525A, and 525B Airplanes - Lower wing skin structure |
(07/02/2008) Transport Canada issued Emergency AD No. CF-2008-11 on 05/02/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models DHC-8-401 and DHC-8-402 (Model DHC-8-400 is not validated in EU) aircraft; Wing-to-Fuselage Attachment Joints – Barrel Nut Cracking |
(06/02/2008) FAA issued AD No 2008-02-13 on 24/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 727 Airplanes - Requiring repetitive external high frequency eddy current (HFEC) inspections of the crown skin for cracks at certain stringer attachment holes, and repair |
(06/02/2008) FAA issued corrected AD No 2007-23-12 on 10/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 707 Airplanes and Model 720 and 720B Series Airplanes -Correcting an error in an existing airworthiness directive (AD) that was published in the Federal Register on November 13, 2007 (72 FR 63800). The error resulted in the wrong appendix information. Accomplishing an airplane survey to define the configuration of certain system installations, and repair of any discrepancy found. Modifying the fuel system by installing lightning protection for the fuel quantity indication system (FQIS), ground fault relays for the fuel boost pumps, and additional power relays for the center tank fuel pumps and uncommanded on-indication lights at the flight engineer's panel. |
(05/02/2008) FAA issued AD No 2008-02-19 on 31/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731 Series Turbofan Engines – High Pressure Turbine Rotor Assemblies Identification/Replacement |
(01/02/2008) FAA issued AD No 2008-03-02 on 31/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cessna Aircraft Company Models 172R and 172S Airplanes - Requiring you to inspect the fuel return line assembly for chafing; replace the fuel return line assembly if chafing is found; and inspect the clearance between the fuel return line assembly and both the right steering tube assembly and the
airplane structure, adjusting as necessary. |
 (31/01/2008) CAA New Zealand issued AD No. DCA/750XL/4A on 31 January 2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Pacific Aerospace Corporation (PAC) 750XL aircraft, s/n 101 through 108; Fuselage – Frame Station 384.62 Rivets – Inspection/Replacement |
(28/01/2008) FAA issued AD No 2008-02-16 on 24/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 767-200 and 767-300 Series Airplanes - Reworking certain duct assemblies in the environmental control system (ECS). |
(28/01/2008) FAA issued AD No 2008-02-14 on 24/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400, -400D, and -400F Series Airplanes; Boeing Model 757 Airplanes; and Boeing Model 767 Airplanes - Requiring an inspection of certain lighted pushbutton switches in the flight compartment for configuration 'D' master modules and part numbers and corrective action. This AD also provides an option to inspect panel assemblies for part numbers. |
(25/01/2008) FAA issued AD No 2008-02-12 on 24/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes - Requiring modification of the conduit for the forward boost pump of the center fuel tank. |
(25/01/2008) FAA issued AD No 2008-02-17 on 24/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
General Electric Company CF6-50, -80A1/A3, and -80C2A Series Turbofan Engines - Requiring initial and repetitive inspections and checks of the thrust reverser actuation systems. This AD requires revised inspection thresholds and intervals, and would require the same actions and additional inspections of the thrust reverser actuation system locking features. |
(25/01/2008) FAA issued AD No 2008-02-18 on 24/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cessna Aircraft Company 172 and 182 Series Airplanes - Requiring you to replace the pick-up collar support and nylon screws for the BRS-172 and BRS-182 Parachute System. |
(24/01/2008) FAA issued AD No 2008-02-06 Correction on 22/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
GARMIN International GSM 85 Servo Gearbox Units - Requiring you to inspect the GSM 85 servo gearbox for foreign object debris and return the unit to the manufacturer for replacement if you find debris. Please consider that the product has ETSO approval EASA.IM.21O.452 as well |
(24/01/2008) FAA issued AD No 2007-07-12 on 03/04/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Honeywell Flight Management Systems (FMSs) Served by Honeywell NZ-2000 Navigation Computers Approved Under Technical Standard Order (TSO) TSOC115a, and IC-800 Integrated Avionics Computers Approved Under TSOs C9c, C52a, and C115a; as Installed on Various Transport Category Airplanes - Identifying affected computers by part number and software modification level and revising the Limitations section of applicable airplane flight manuals to provide procedures for retaining optimum position determination and intended navigation. |
(23/01/2008) FAA issued AD No 2008-02-08 on 22/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes - Requiring electrical bonding of the fill valves for the right and left main fuel tanks, the fill valve and pipe assembly for the center wing fuel tank, and the defuel shutoff valve. |
(21/01/2008) Transport Canada issued AD No. CF-2007-09 on 17/05/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bell Helicopter Textron Canada (BHTC) Model 222, 222B and 222U helicopters; Tail Rotor Driveshaft (Thomas Couplings) Disc Assemblies – Inspection / Replacement |
(28/01/2008) Transport Canada issued AD No. CF-2008-06 on 15/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models DHC-8-401 and DHC-8-402 (Model DHC-8-400 is not validated in EU) aircraft, all serial numbers; Fuel System Safety - Introduction of Critical Design Configuration Control Limitations |
(17/01/2008) ANAC Brazil issued AD No 2007-12-02, effective 24/01/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-190 aircraft models in operation equipped with Ram Air Turbine (RAT) part number (P/N) 1703781 and serial numbers (S/N) 0005 and 0101 thru 0419 - Inspection, reidentification and replacement of the RAT |
(17/01/2008) ANAC Brazil issued AD No 2007-12-01, effective 24/01/2008, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-170 aircraft models in operation equipped with Ram Air Turbine (RAT) part number (P/N) 1703781 and serial numbers (S/N) 0005 and 0101 thru 0419 -I nspection, reidentification and replacement of the RAT. |
(16/01/2008) Transport Canada issued AD No. CF-2008-04 on 11/01/2008 , to be considered accepted by EASA under provisions of ED Decision 02/2003
Bell Helicopter Textron Canada (BHTC) Model 407 helicopters; Tailboom P/N 407-030-801-107 and 407-530-014-101/-103 Inspection |
(16/01/2008) Transport Canada issued AD No. CF-2007-31 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Viking Air Ltd. (formerly De Havilland Canada) DHC-6 series, all Models, all serial numbers; Wing Front Spar Adapter Assembly |
(15/01/2008) FAA issued AD No 2005-24-03R1 on 08/03/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, and -800 Series Airplanes - Inspecting/measuring the length of the attachment fasteners between the nacelle support fittings and the lower wing skin panels, and related investigative/corrective actions |
(15/01/2008) FAA issued AD No 2007-26-12 on 03/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Robinson Helicopter Company Models R22, R22 Alpha, R22 Beta, R22 Mariner, R44 and R44 II Helicopters - Requiring a one-time visual inspection for skin separation along the leading edge of blade skin aft of the skin-to-spar bond line on the lower surface of each blade and in the tip cap area. Requiring a ''tap test'' for detecting a separation or void in both bonded areas. Repainting any exposed area of the blades. If any separation or void is detected, replacing the blade before further flight is required. Before each flight, checking for any exposed (bare metal) along the skin-to-spar bond line on the lower surface of each blade near the tip. If any bare metal is found, a mechanic must inspect the area. |
(15/01/2008) FAA issued AD No 2007-26-02 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 757-200, -200CB, and -300 Series Airplanes - Requiring repetitive detailed inspections with a borescope for cracks of the intercostal tee clips; or repetitive detailed inspections for cracks of the intercostal tee clips and attachment fasteners at the number 3 and number 4 doorstops of the passenger door cutouts; and related investigative and corrective actions. Also providing an optional terminating action for the repetitive inspections |
(14/01/2008) Transport Canada issued AD No. CF-2008-03 on 03/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. (formerly De Havilland Canada) DHC-8 Series 100, 200 and 300 aircraft; Fuel System Safety - Introduction of Critical Design Configuration Control Limitations |
(14/01/2008) FAA issued AD No 90-25-05R1 on 10/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes - Requiring the implementation of a corrosion prevention and control program |
(14/01/2008) FAA issued AD No 2007-26-17 on 10/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes - Doing a detailed inspection of the left and right longeron extension fittings, and corrective action |
(14/01/2008) FAA issued AD No 2008-01-03 on 10/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Learjet Model 45 Airplanes - Revising the Airworthiness Limitations section of the airplane maintenance manual to incorporate certain inspections and compliance times to detect fatigue cracking of certain principal structural elements (PSEs) |
(09/01/2008) FAA issued AD No 2004-07-22R1 on 07/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747- 200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes - Requiring that the FAA-approved maintenance inspection program be revised to include inspections that will give no less than the required damage tolerance rating for each structural significant item, and repair of cracked structure |
(08/01/2008) Transport Canada issued AD No. CF-2008-02 on 03/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models CL-600-2C10 and CL-600-2D24 aircraft; Fuel System Safety - Insufficient Electrical Bonding between Fuel Tubes and Insufficient Lightning Current Capability of Fuel Tube Couplings |
(08/01/2008) Transport Canada issued AD No. CF-2008-01 on 03/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models CL-600-2C10 and CL-600-2D24 aircraft; Fuel System Safety - Fuel Tank Climb Vent Loop Fuel Leak onto Anti-Ice Duct |
(07/01/2008) FAA issued AD No 2007-26-09 on 26/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Hartzell Propeller Inc. Compact Series Propellers - Requiring initial blade inspections, with no repetitive inspections; rework of all ''Y'' shank aluminum blades including cold rolling of the blade shank retention radius, blade replacement and modification of pitch change mechanisms for certain propeller models; and changing the airplane operating limitations with specific models of propellers installed. |
(07/01/2008) FAA issued AD No 2007-26-16 on 03/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cessna Model 680 Airplanes - Inspecting the routing of the aft fairing wire bundle assembly for adequate separation between the wiring and the hydraulic line; inspecting for chafing or damage of the wire bundle assembly and for damage to the hydraulic line, and doing corrective actions. |
(07/01/2008) Transport Canada issued AD No. CF-2007-35 on 21/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. (Canadair) Models CL-600-2B19 aircraft, all serial numbers; Fuel System Safety - Introduction of Critical Design Configuration Control Limitations. |
(07/01/2008) Transport Canada issued AD No. CF-2007-34 on 21/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. (Canadair) Models CL-600-2B19 aircraft, serial numbers 7003 through 7067, and 7069 through 7929; Fuel System Safety - Insufficient Electrical Bonding for Lightning Protection Inside Fuel Tanks. |
(07/01/2008) Transport Canada issued AD No. CF-2007-36 on 21/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. (Canadair) Models CL-600-2B19 aircraft, serial numbers 7003 through 7067, and 7069 through 7982; Fuel System Safety - Chafing of Fuel Quantity Gauging System Wiring |
(07/01/2008) FAA issued AD No 2007-26-20 on 03/01/2008, to be considered accepted by EASA under provisions of ED Decision 02/2003
Pratt & Whitney (PW) PW4164, PW4168, and PW4168A Turbofan Engines - Removing certain LPT stage 4 disks, listed by serial number at the next piece-part exposure or within 7,500 cycles-since-new (CSN). |
(07/01/2008) FAA issued AD No 2007-26-07 on 28/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-200B, 747-300, 747-400, 747-400D, and 747-400F Series Airplanes Equipped with General Electric CF6-80C2 Engines - Requiring repetitive inspections of the left- and right-hand flipper door assemblies of the engine core cowls for migrated pins and damaged flipper doors, and corrective actions. Modification of the hinge assemblies terminates the repetitive inspections. |
(04/01/2008) Transport Canada issued AD No. CF-2007-24R1 on 21/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Pratt & Whitney Canada Model PW206 and PW207 Series Engines - Compressor Turbine Disk Inspection and Retaining Nut Replacement |
(04/01/2008) FAA issued AD No 2007-26-06 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-200B, 747-300, and 747-400 Series Airplanes - Requiring an inspection to determine the manufacturer and manufacture date of the oxygen masks in the passenger service units of the outboard and center main deck, the flight attendant service units, flightcrew rest, upper and lower module of the door 5 overhead crew rest, lavatory modules, and miscellaneous ceiling panels, as applicable, and related investigative/corrective actions |
(04/01/2008) FAA issued AD No 2007-26-03 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-200C and -200F Series Airplanes - Installing mounting brackets, support angles, and moisture curtains in the main equipment center |
(04/01/2008) FAA issued AD No 2007-25-20 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30 and DC-10-30F (KC-10A and KDC-10) Airplanes; Model DC-10-40 and DC-10-40F Airplanes; and Model MD-11 and MD-11F Airplanes - For certain airplanes, modifying the thrust reverser command wiring of the number 2 engine. For certain other airplanes, modifying the thrust reverser system wiring from the flight compartment to engines 1, 2, and 3 thrust reversers. Installing thrust reverser locking systems on certain airplanes |
(04/01/2008) Transport Canada issued AD No. CF-2007-33 on 03/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. Models DHC-8-401 and DHC-8-402 (Model DHC-8-400 is not validated in EU) aircraft, all serial numbers; Fuel System Safety - Introduction of Maintenance Tasks |
(04/01/2008) Transport Canada issued AD No. CF-2007-32 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier Inc. (De Havilland Canada) Models DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DH C-8-202, DHC-8-301, DHC-8-311, DHC-8-314 and DHC-8-315 aircraft, all serial numbers; Fuel System Safety - Introduction of Maintenance Tasks |
(21/12/2007) FAA issued AD No 2007-23-10 on 15/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -800 and -900 Series Airplanes - Requiring an inspection of the fillet sealant at the inboard and outboard sides of the receptacles in the wheel wells of the main landing gear, and related investigative/corrective actions |
(21/12/2007) FAA issued AD No 2007-25-16 on 10/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-81 (MD-81) and DC-9-82 (MD-82) Airplanes - Inspecting for cracking of the fuselage skin at the upper corners of the forward passenger doorjamb, installing or replacing doublers as applicable, and doing applicable repairs. |
(20/12/2007) FAA issued AD No 2007-26-05 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200, -200LR, -300, and -300ER Series Airplanes - Doing initial and repetitive inspections for cracking of the elevator actuator fittings, and replacing any cracked fitting with a new fitting |
(20/12/2007) FAA issued AD No 2007-26-01 on 17/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Thrush Aircraft, Inc. Model S2R Series Airplanes - Requiring repetitive visual inspections of the vertical and horizontal stabilizer attach fitting, attach fitting bolts, and the vertical fin aft spar for cracks or corrosion. Requiring also immediate replacement of the vertical and horizontal stabilizer attach fittings and attach fitting bolts if cracked or corroded parts are found, and the inspection of the vertical fin aft spar with repair or replacement if cracks or corrosion are found. Requiring the eventual replacement of the vertical and horizontal stabilizer attach fittings and attach fitting bolts if no corrosion or cracks are found as terminating action for the repetitive inspections. |
(20/12/2007) Transport Canada issued AD No. CF-2007-27R1 on 19/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Diamond Aircraft Industries Inc. Model DA20-C1 aircraft powered by Teledyne Continental Motors (TCM) IO-240-B13B or IO-240-B17B model engines – Fuel System Maintenance Actions, AFM Revision and Placards Replacement - In-Flight Engine Shutdown. |
(18/12/2007) FAA issued AD No 2007-25-03 on 10/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -800, and -900 Series Airplanes - Requiring repetitive inspections of either the aft side or forward side of the aft pressure bulkhead for oil can conditions or bulges, a onetime inspection of the aft pressure bulkhead to identify any previously installed web repair, and corrective actions |
(18/12/2007) FAA issued AD No 2007-22-02 on 26/10/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bell Helicopter Textron, Inc. Model 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP Helicopters
Inspecting each affected tail rotor blade (blade) forward tip weight retention block (tip block) and the aft tip closure (tip
closure) for adhesive bond voids, removing any blade with an excessive void from service and modifying certain blades
by installing shear pins and tip closure rivets. |
(18/12/2007) FAA issued AD No 2007-15-04 on 24/07/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-800 Series Airplanes - Flight Spoiler Actuator Check / Operational Test / Replacement. |
(18/12/2007) ANAC Brazil issued AD No 2007-11-04R1 - Amdt 1224 - Embraer EMB-145( ) (CORRECTION), effective 21/12/2007, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer EMB-145 and EMB-135 aircraft models of serial numbers (S/N) 145002 thru 145362, 145364 thru 145590, and 145592 thru 14500987
- Inspection of Pitot 1/2 and TAT 1/2 current sensor relays and sockets; replacement of the A1 and C1 socket electrical contacts, or of the entire socket; and sockets reidentification. |
(13/12/2007) FAA issued AD No 2007-23-18 on 23/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400, and 747-400D Series Airplanes - Requiring repetitively inspecting for cracking or discrepancies of the fasteners in the tension ties, shear webs, and frames at body stations 1120 through 1220, and performing related investigative and corrective actions. |
(13/12/2007) FAA issued AD No 2007-24-05 on 28/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan Engines - Requiring preflight operational procedures and a terminating action. |
(12/12/2007) FAA issued AD No 2007-25-18 on 10/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400 and 747-400D Series Airplanes - For certain airplanes, modifying the stowage bin ladder of zone E, installing new intercostals, removing existing tie rods, and installing new tie rods. For certain other airplanes, modifying the lateral shear beam. |
(12/12/2007) FAA issued AD No 2007-25-19 on 10/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400 Series Airplanes - AD requiring repetitive inspections to detect discrepancies of the forward and rear heat exchanger shells of the air distribution system of the crew rest area, and applicable corrective actions. AD also requiring an inspection to identify the part number, shop code, and build date of the forward and rear heat exchanger shells of the air distribution system of the crew rest area, and applicable corrective actions, which end the repetitive inspections. |
(12/12/2007) FAA issued AD No 2007-25-17 on 10/12/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP Series Airplanes - Requiring repetitive inspections for cracking of the station (STA) 1241 bulkhead fittings just above the canted pressure deck; a one-time determination of the edge margin at seven fastener positions on each side of the airplane; and related investigative/corrective actions. |
(11/12/2007) FAA issued AD No 2007-23-16 on 20/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cessna Aircraft Company, Model 525B Airplanes - Incorporating electrical power relay circuit protection kit part number (P/N) SB525B-24-02 |
(07/12/2007) ANAC Brazil issued CORRECTED AD No. 2007-11-02, effective 12/12/2007, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-190 series aircraft - Pressure Equalization Valves Inspection / Installation. |
(07/12/2007) ANAC Brazil issued CORRECTED AD No 2007-04-02R1, effective 21/12/2007, which is considered accepted by EASA under provisions of ED Decision 02/2003
Embraer ERJ-190 aircraft models - Amendment 39-1222 - Replacement of the hydraulic system tubes attachment clamps, located inside the wing fuel tanks, by other ones with a new P/N. |
(06/12/2007) FAA issued AD No 2007-24-07 on 28/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003.
General Electric Company (GE) CF6-80C2B1 Turbofan Engine - Stripping of thermal spray coating required, inspection of dovetail slots, and reapplication of thermal spray coating on certain stage 1 fan disks |
| (06/12/2007) ANAC Brazil issued AD No 2007-04-01R1, effective 21/12/2007, which is considered accepted by EASA under provisions of ED Decision 02/2003. Embraer ERJ-170 aircraft models - Amendment 39-1221 - Replacement of the hydraulic system tubes attachment clamps located inside the wing fuel tanks by other ones with a new P/N . |
(04/12/2007) FAA issued AD No 2007-24-14 on 29/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Hartzell Propeller Inc. Model HC-E5N-3( ), HC-E5N-3( )(L), and HC-E5B-5( ) Propellers - Requiring a onetime eddy current inspection of the propeller hub mounting bolt holes and replacement of the propeller hub if cracked. |
(04/12/2007) FAA issued AD No 2007-24-13 on 29/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Cirrus Design Corporation Model SR22 Airplanes - Requiring to install a drain hole in the left and right outboard wing tips. |
(03/12/2007) FAA issued AD No 2007-24-08 on 28/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 767 Airplanes - Requiring repetitive measurements of the rudder and elevator freeplay, repetitive lubrications of rudder and elevator components, and related investigative/corrective actions. Requiring revised repetitive measurements of the rudder freeplay and the elevator freeplay for each of the power control actuators (PCAs) that move the rudder and elevator, corrective and related investigative actions, and repetitive lubrications of the rudder and elevator components
Requiring also related concurrent actions for some airplanes |
(03/12/2007) FAA issued AD No 2007-24-01 on 28/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Hawker Beechcraft Model 400A Series Airplanes - Inspecting the galley cabinets to determine if a certain part number is installed or if a certain size of wire already exists, and doing related investigative/corrective actions |
(30/11/2007) ANAC Brazil issued AD No. 2007-11-01, effective 12 August 2007, which is considered accepted by EASA under provisions of ED Decision 02/2003.
Embraer ERJ-170 series aircraft; Pressure Equalization Valves Inspection / Installation. |
(29/11/2007) CAA New Zealand issued AD No. DCA/750XL/3A, effective on 29 November 2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Pacific Aerospace Corporation (PAC) 750 XL - Wiring Loom Protective Sleeve - Inspection and Installation |
(27/11/2007) Transport Canada issued AD No. CF-2007-29 on 22/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier CL-600-2B19 aircraft – Fuel System Safety - Introduction of Maintenance Tasks |
(27/11/2007) Transport Canada issued AD No. CF-2007-28 on 22/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Bombardier CL-600-2C10, CL-600-2D15 and CL-600-2D24 aircraft – Fuel System Safety - Introduction of Maintenance Tasks |
(26/11/2007) FAA issued AD No 2007-24-02 on 21/11/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes - Repetitive detailed inspections required for damage of the electrical wire and sleeve that run to the fuel boost pump through a conduit in the fuel tank, and arcing damage of the conduit and signs of fuel leakage into the conduit; replacement of the sleeve with a new, smaller-diameter sleeve; and related investigative and corrective actions. |
(20/11/2007) FAA issued AD No
2007-23-13 on 15/11/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
Cessna Model 560 Airplanes - Installing new minimum
airspeed placards to notify the flightcrew of the proper
airspeeds for operating in both normal and icing
conditions. Revising the airplane flight manual to
provide limitations and procedures for operating in icing
conditions, for operating with anti-ice systems selected
''on'' independent of icing conditions, and for
recognizing and recovering from inadvertent stall.
Providing an optional terminating action for the placard
installation. |
(19/11/2007) FAA issued AD No
2007-23-11 on 15/11/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
Boeing Model 777 Airplanes - Requiring repetitive
measurements of the freeplay of certain joints of the
trailing edge flap supports; repetitive lubrication of
the support joints; and related investigative and
corrective actions. |
(16/11/2007) FAA issued
AD No 2007-23-09 on 15/11/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767-200, -300, and -300F Series Airplanes -
Requiring a one-time inspection of each fuel quantity
indication system (FQIS) wire harness connector for
corrosion of the shield-to-backshell connection,
corrosion on the ground jumper, and damage to the ground
jumper; a loop resistance test of each FQIS wire harness;
and related investigative and corrective actions. |
(16/11/2007) FAA issued
AD No 2007-23-08 on 15/11/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400, 747-400D, and 747-400F Series
Airplanes; Model 757-200 Series Airplanes; and Model
767-200, 767-300, and 767-300F Series Airplanes -
Inspecting required to determine the date code of the
time delay relay for the cargo fire suppression system,
and replacing the relay. |
(07/11/2007) The State
of Israel CAA issued AD No 24-07-10-11 on 31/10/2007, to
be considered accepted by EASA under provisions of ED
Decision 02/2003
Gulfstream Aerospace L.P. (GALP; formerly Israel Aircraft
Industries) Model G150 aircraft; LH Electrical DC Power
Box Feeder Cable -
Inspection/Relocation. |
(06/11/2007) ANAC
Brazil issued AD No 2006-11-03R2 Corrected, effective
30/10/2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003
All Embraer ERJ-190 aircraft models in operation and
equipped with Primus EPIC software load versions 4.3,
4.4, 4.5, 4.6 or 4.7. Functional check of the FGCS and
installation of an updated Primus EPIC software
version. |
(30/10/2007) FAA issued
AD No 2007-19-07 on 24/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757-200, -200PF, and -200CB Series
Airplanes
Inspections required to detect scribe lines and cracks of
the fuselage skin, lap joints, circumferential butt
splice strap, and external and internal approved repairs;
and related investigative/corrective actions |
(30/10/2007) ANAC
Brazil issued AD No 2006-03-03R1, effective 09/11/2007,
which is considered accepted by EASA under provisions of
ED Decision 02/2003
All Embraer ERJ-190 aircraft models - Inclusion of a
temporary limitation to the ANAC-approved Airplane Flight
Manual (AFM) to prohibit a throttle movement into the
forward thrust range immediately following a thrust
reverser application; and installation of a new engine
Full-Authority Digital Engine Control (FADEC)
software. |
(30/10/2007) ANAC
Brazil issued AD No 2006-11-02R2, effective 30/10/2007,
which is considered accepted by EASA under provisions of
ED Decision 02/2003
All Embraer ERJ 170 aircraft models equipped with Primus
EPIC software load version 17.3, 17.4, 17.5, 17.6 or
17.7. - Functional check of the FGCS and installation of
an updated Primus EPIC software version. |
(29/10/2007) FAA issued
AD No 2007-21-15 on 16/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 707 Airplanes and Model 720 and 720B Series
Airplanes - Identifying the material used in the elevator
hinge support fittings of the horizontal stabilizer
trailing edge, doing repetitive detailed inspections for
cracking of the fittings and corrective actions; and
doing an eventual terminating action. |
(29/10/2007) FAA issued
AD No 2007-21-04 on 12/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 727 Airplanes - Doing an initial detailed
inspection for cracks in the aft pressure bulkhead web;
repairing any discrepancy; doing repetitive detailed
inspections, and doing related investigative actions |
(25/10/2007) FAA issued
AD No 2007-22-07 on 24/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
General Electric Company (GE) CF6-80C2D1F Turbofan
Engines - Removing previous software versions from the
engine electronic control unit (ECU). |
(25/10/2007) FAA issued
AD No 2007-21-18 on 24/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-8-53, DC-8-55, DC-8F-54, and
DC-8F-55 Airplanes; and Model DC-8-60, DC-8-60F, DC-8-70,
and DC-8-70F Series Airplanes - One-time inspection
required to determine the configuration of the airplane.
Repetitive inspections required for cracking of the tee
or angle doubler, and corrective actions |
(24/10/2007) Transport
Canada issued AD No. CF-2007-23 on 18/10/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Model CL-600-2B19 aircraft
- FUEL TANK SAFETY - Insufficient
Electrical Bonding between Fuel Tubes and Insufficient
Lightning Current Capability of Fuel Tube Couplings |
(23/10/2007) FAA issued
AD No 2007-21-13 on 16/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 and 767 Airplanes |
(18/10/2007) FAA issued
AD No 2007-21-08 on 16/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Hawker Beechcraft Model Hawker 800XP Airplanes |
(18/10/2007) ANAC
Brazil issued AD No. 2000-08-01R3, effective 6 August
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003.
Embraer EMB-145 ( ) and EMB-135 ( )
Visual inspection on the electrical connector pins and
the elastomeric inserts; replacement of the affected fuel
pumps, if needed; and, application of anti-corrosion
product on the electrical connectors |
(18/10/2007) ANAC
Brazil issued AD No. 2007-07-01, effective 21 August
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003.
Embraer aircraft models EMB-145( )
Required action:Updating of the aircraft approved
maintenance program according to the Maintenance Review
Board Report (MRBR) |
(18/10/2007) ANAC
Brazil issued AD No. 2007-07-02, effective 21 August
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003.
All Embraer EMB-145( ) and EMB-135( ) aircraft models, of
all serial numbers (S/N).
NOTE: This AD is not applicable to
EMB-145LR aircraft model modified according to Brazilian
Supplemental Type Certificate (CHST) Nos. 2002S06-09,
2002S06-10 and 2003S08-01.
Required action:Updating of the aircraft approved
maintenance program according to the Maintenance Review
Board Report (MRBR) or Maintenance Planning Guide (MPG)
as applicable |
(18/10/2007) ANAC
Brazil issued AD No. 2007-07-03, effective 21 August
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003.
Embraer aircraft model EMB-145LR of serial numbers (S/N)
145104, 145122, 145140, 145154, 145257, 145263, 145365
and 145392, modified according to Brazilian Supplemental
Type Certificate (CHST) Nos. 2002S06-09 or 2002S06-10,
and of S/N 145374, 145671, 145729 and 145757, modified
according to CHST No. 2003S08-01. Required action: Rework
of the APU firewall. |
(15/10/2007) FAA issued AD No
2007-21-06 on 11/10/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
General Electric Company (GE) CF6-80C2A5F Turbofan
Engines |
(15/10/2007) FAA issued
AD No 2007-15-05 on 24/07/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Series Airplanes -
FUEL TANK SAFETY - AFM/Placards Change
- Fuel Pump / Fuel Tank Deactivation -
Fuel Pump Housing Electrical Connector |
(15/10/2007) FAA issued
AD No 2007-15-07 on 30/07/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Series Airplanes -
Fuselage Skin High Frequency Eddy Current (HFEC)
Repetitive Inspections |
(15/10/2007) FAA issued
AD No 2007-21-05 on 11/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
International Aero Engines (IAE) V2500 Series Turbofan
Engines |
(12/10/2007) FAA issued
AD No 2007-21-02 on 11/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon Aircraft Company Models 58P and 58TC
Airplanes |
(04/10/2007) FAA issued
AD No 2007-20-07 on 03/10/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Hawker Beechcraft Corporation (Type Certificate No.
A00010WI Previously Held by Raytheon Aircraft Company)
Model 390 Airplanes |
(03/10/2007) FAA issued
AD No 2007-17-13 on 28/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, -200B, -200C, and -200F Series
Airplanes |
(03/10/2007) FAA issued
AD No 2007-19-19 on 21/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747- 100B SUD, 747-200B,
747-200C, 747-200F, 747-300, 747SR, and 747SP Series
Airplanes |
(03/10/2007) FAA issued
AD No 2007-19-17 on 21/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-11, MD-11F, DC-10-10,
DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and
KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F
Airplanes |
(03/10/2007) FAA issued
AD No 2007-19-16 on 21/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
(03/10/2007) FAA issued
AD No 2007-19-15 on 21/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-10-10F and MD-10-30F
Airplanes, Model MD-11 and MD-11F Airplanes, and Model
717-200 Airplanes |
(03/10/2007) FAA issued
AD No 2007-20-01 on 26/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100B SUD, 747-200B, 747-200C, 747-200F,
747-300, 747-400, 747-400D, 747-400F, and 747SP Series
Airplanes |
(03/10/2007) FAA issued
AD No 2007-15-10 Correction on 21/09/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 747 Airplanes |
(24/09/2007) FAA issued
AD No 2007-19-06 on 18/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
General Electric Company Aircraft Engine Group (GEAE)
CF6-45A Series, CF6-50A, CF6-50C Series and CF6-50E
Series Turbofan Engines |
(20/09/2007) FAA issued
AD No 2007-19-05 on 18/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Hawker Beechcraft Model 400, 400A, and 400T Series
Airplanes - Engine Cowling Panels Attachment Fasteners
Modification |
(19/09/2007) CAA New
Zealand issued AD No. DCA/750XL/13, effective on 26 April
2007, to be considered accepted by EASA under provisions
of ED Decision 02/2003
Pacific Aerospace Corporation (PAC) 750 XL
- Aileron Inboard Hinge Attachment
- Inspection and Modification |
(18/09/2007) Transport
Canada issued AD No. CF-2007-22 on 14/09/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bell Helicopter Textron Canada (BHTC) Model 427
helicopters - Vertical Fin and Tail
Rotor Gearbox Support Attachment
Inspection/Modification |
(14/09/2007) FAA issued
AD No 2007-19-03 on 12/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes
- Power Conversion Distribution Unit
(PCDU) Inspection/Modification |
(14/09/2007) Transport
Canada issued AD No. CF-2007-17 on 04/09/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Model CL-600-2B19 -
FUEL TANK SAFETY - Application of
Sealant to Collector Fuel Tank Bolts and Transfer Ejector
Pumps |
(14/09/2007) Transport
Canada issued AD No. CF-2007-18 on 04/09/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Model CL-600-2B19 -
FUEL TANK SAFETY - Fuel Boost Pump
Reducer Coupling Inspection/Replacement |
(14/09/2007) Transport
Canada issued AD No. CF-2007-12 on 24/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bell Helicopter Textron Canada (BHTC) Model 230
helicopters- Tail Rotor Pitch Change
Mechanism Inspection & Rigging Procedure
Amendment |
(13/09/2007) FAA issued
AD No 2007-19-02 on 12/09/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10, MD-10
and MD-11 Series Airplanes - FUEL TANK
SAFETY - No.2 Fuel Transfer Pump
Adapter Surface & Housing Electrical Resistance
Inspection/Modification |
(12/09/2007)
FAA issued AD No 2007-18-10 on 11/09/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
General Electric (GE) CF6-80E1 Series
Turbofan Engines - Compressor Rear
Frame (CRF) Identification/Inspection/Replacement |
(07/09/2007)
FAA issued AD No 2007-17-12 on 28/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 777 Series Airplanes
- Horizontal Stabiliser Drive
Mechanism Inspection |
(06/09/2007) FAA issued
AD No 2007-11-02 on 28/08/2007 , to be considered accepted
by EASA under provisions of ED Decision 02/2003
Enstrom Helicopter Corporation Model F-28A, F-28C, F-28F,
TH-28, 280, 280C, 280F, 280FX, 480 and 480B Helicopters -
Main Rotor Push-Pull Control Rod
Inspection/Repair/Replacement |
 (05/09/2007) CTA Brazil
AD No. 2006-10-01R1 to be considered accepted by EASA
under provisions of ED Decision 02/2003
All Embraer EMB-110( ) aircraft models in
operation.
Wing-to-Fuselage & Vertical Stabilizer-to-Fuselage
Attachments, Rib 1 Half-wing and Passenger Seat Tracks
- Inspection/Repair |
(04/09/2007) FAA issued
AD No 2007-17-21 on 24/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney JT9D-7R4 series Turbofan Engines
- Second Stage High Pressure Turbine
(HPT) Vane Assembly Identification/Replacement; and
Second Stage HPT Air Seal Assembly Inspection |
(04/09/2007) FAA issued
AD No 2007-17-02 on 14/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Allied Ag Cat Productions, Inc. (FAA Type Certificate No.
1A16 formerly held by Ag-Cat Corporation; Schweizer
Aircraft Corporation; Gulfstream American; Grumman
American) G-164 series aircraft - Fuel
Shut-Off Valve Control Modification |
(04/09/2007) FAA issued
AD No 2007-18-03 on 28/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400 and -500 Series Airplanes
- Flight Crew Seats Locks and Seat
Tracks Inspection/Rework |
(03/09/2007) FAA issued
AD No 2007-18-06 on 31/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney JT9D-7R4 series Turbofan Engines
- Fan Blade
Identification/Inspection/Replacement |
(03/09/2007) FAA issued
AD No 2007-17-09 on 21/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
- Elevator Nose-down Trim Maximum
Deflection Reduction and Elevator Trim Indicator Scale
Dial Modification
NOTE: The FAA is the "˜State of
Design"™ authority for the MU-2B s/n
aircraft that were originally manufactured in the USA by
Mitsubishi Aircraft International. Inc. and certified
under FAA TC A10SW. These are identified in the AD as
"˜category 2"™
airplanes. For this reason, EASA regards this FAA AD as
being a "˜State of
Design"™ AD for the category 2
airplanes. For the category 1 airplanes, Japan Civil
Aviation Bureau (JCAB) AD TCD-3740A-98, which is a
revision of original AD TCD-3740-92, is regarded by EASA
as being a "˜State of
Design"™ AD and has therefore already
been "˜adopted"™ in
the European Union, as per current EU regulations. |
(03/09/2007) FAA issued
AD No 2007-17-18 on 28/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas DC-9 series and Model MD-88 Airplanes
- Static Port Heater Assembly
Inspection/Test/Replacement |
(03/09/2007) FAA issued
AD No 2007-17-19 on 28/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-90-30 Airplanes
- Static Port Heater Assembly
Inspection/Test/Replacement |
(03/09/2007) FAA issued
AD No 2007-07-07 R1 on 28/08/2007, to be considered
accepted by EASA under provisions of ED Decision
02/2003
General Electric Company CF34-1A, -3A,
-3A1, -3A2, -3B, and -3B1 Turbofan Engines
- Fan Disk
Identification/Inspection/replacement [Life
Limitation] |
(03/09/2007) FAA issued
AD No 2007-17-17 on 28/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Learjet Model 31, 31A 35, 35A (C-21A), 36, 36A, 45, 55,
55B and 55C airplanes - Engine Pylon
& Fire Wall Inspection/Sealing |
(03/09/2007) FAA issued
AD No 2007-17-11 on 28/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes
- Fuel Tank In-line Float Switch Fuses
and Wire Protection Installation [FUEL TANK SAFETY] |
(03/09/2007) FAA issued
AD No 2007-17-01 on 14/08/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
General Electric (GE) CF6-80E1 Series Turbofan Engines
Engine Electronic Control Unit (ECU) Software Update
Installation |
(27/08/2007) Transport
Canada issued AD No. CF-2007-02 R1 on 23/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bell Helicopter Textron Canada (BHTC) Model 206 -
Transmission Pylon Support Spindle -
Identification/Replacement |
(27/08/2007) Transport
Canada issued AD No. CF-2005-10 R3 on 24/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bell Helicopter Textron Canada (Bell) 206A and 206B
series helicopters - Fuel Distribution
System |
(27/08/2007)
FAA issued AD No 2007-16-18 on 21/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 767
Airplanes - Detection and correction of damage to wires
in the forward and aft lower lobe cargo
compartments. |
| (23/08/2007) Transport
Canada issued AD No. CF-2007-11 on 09/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bombardier Inc. (formerly De
Havilland Canada) Models DHC-8-102, DHC-8-103, DHC-8-106,
DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, DHC-8-314,
DHC-8-315, DHC-8-400, DHC-8-401 and DHC-8-402 aircraft -
Flight Compartment - Utility and Observer Lights
Modifications |
(23/08/2007)
FAA issued AD No 2007-11-07 [Correction] on 21/08/2007,
to be considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 737-100,
-200, -200C, - 300, -400, and -500 Series Airplanes
- FUEL TANK SAFETY - Fuel Boost Pump
Electrical Wiring & Sleeve
Inspection/Replacement |
(22/08/2007) CAA New
Zealand issued AD No. DCA/750XL/10 on 27 March 2007, to
be considered accepted by EASA under provisions of ED
Decision 02/2003
Pacific Aerospace Corporation 750 XL -
Cockpit Windows - Inspection and
Modification |
(22/08/2007) CAA New
Zealand issued AD No. DCA/750XL/11 on 27 March 2007, to
be considered accepted by EASA under provisions of ED
Decision 02/2003
Pacific Aerospace Corporation 750 XL -
Rudder Trim Tab Pivot - Inspection and
Modification |
(21/08/2007)
FAA issued AD No 2007-17-05 on 21/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Sikorsky Aircraft
Corporation Model S-92A Helicopters - Tail Rotor Pitch
Change Shaft & Bearing Assembly
Inspection/Replacement |
(17/08/2007)
FAA issued AD No 2007-16-03 on 03/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
M7 Aerospace LP
(formerly Fairchild Aircraft Inc.; Swearingen Aviation
Corp.) Model SA226 and SA227 series aircraft
- AFM Change / Pitch Trim Actuator
Inspection/Replacement |
(16/08/2007)
FAA issued AD No 2007-16-14 on 13/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Taylorcraft Model A,
B and F Series Airplanes (FAA TCDS A-643, A-696, A-699,
A-700 and 1A9) - Wing Forward &
Aft Lift Struts Inspection/Replacement |
| (15/08/2007) ANAC
Brazil issued AD No. 2001-06-01 R4 Corrected, effective
23 August 2007, which is considered accepted by EASA
under provisions of ED Decision 02/2003. Embraer
EMB-120( ) aircraft models in operation. Revision of the
applicable airplane flight manual (AFM) establishing an
operational limitation for using the autopilot;
installation of two placards on the cockpit frontal
panel; and modification of the elevator trim system. |
| (15/08/2007) ANAC
Brazil issued AD No. 2007-02-01 R1, effective 27 August
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer ERJ-170( )
aircraft models in operation, equipped with firewall
hydraulic shutoff valves part numbers (P/N) 975287-3 or
975287-5. Additional operational check of the firewall
hydraulic shutoff valves is required. |
| (15/08/2007) ANAC
Brazil issued AD No. 2007-08-03, effective 27 August
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer ERJ-170( )
aircraft models in operation. Removal of some wiring
connections in the electrical connectors of both Inertial
Reference Units is required. |
| (15/08/2007) ANAC
Brazil issued AD No. 2007-02-02R1, effective 27 August
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer ERJ-190( )
aircraft models in operation, equipped with firewall
hydraulic shutoff valves part numbers (P/N) 975287-3 or
975287-5.Additional operational check of the firewall
hydraulic shutoff valves is required. |
| (15/08/2007) ANAC
Brazil issued AD No. 2007-08-04, effective 27 August
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer ERJ-190( )
aircraft models in operation. Removal of some wiring
connections in the electrical connectors of both Inertial
Reference Units is required. |
(15/08/2007)
FAA issued AD No 2007-16-19 on 13/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model
747-200B, 747-300 and 747-400 Series Airplanes
- Fuselage Aft Tension Tie Channels
Inspection/Repair |
(13/08/2007)
FAA issued AD No 2007-16-13 on 09/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 757-200,
-200PF, and -200CB Series Airplanes - Engine
Strut-to-Diagonal Brace Fitting & Aft Torque Bulkhead
Shim Installation -
Inspection/Repair |
(13/08/2007)
FAA issued AD No 2007-16-12 on 09/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 757-200
and -300 Series Airplanes - Electrical System
Modifications & Components Replacement |
(10/08/2007)
FAA issued AD No 2007-16-08 on 09/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 747-100,
747-100B, 747-100B SUD, 747-200B, 747-200C, 747-300,
747-400, 747-400D, and 747SR Series Airplanes - Fuselage
Station 800 Frame Assembly Inspection/Repair |
(10/08/2007)
FAA issued AD No 2007-16-05 on 09/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 737-100,
-200, -200C, -300, -400, and -500 Series Airplanes -
Elevator Tab Control Rod Assemblies Inspection |
(08/08/2007) FAA issued AD No 2007-16-10 on 08/08/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Teledyne
Continental Motors Model IO-550-N, TSIO-520-BE,
TSIO-550-A, TSIO-550-B, TSIO-550-C, TSIO-550-E, and
TSIO-550-G Reciprocating Engines -
Turbocharger Identification/Replacement |
| (01/08/2007) FAA issued AD No
2007-16-01 on 31/01/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Enstrom Helicopter Corporation Model
F-28, F-28A, F-28C, F-28C-2, F-28C-2R, F-28F, F-28F-R,
280, 280C, 280F, 280FX, TH-28, 480, and 480B Helicopters
- Main Rotor Blade Retention Pin
Identification/Replacement |
| (17/07/2007) FAA issued AD No
2007-13-09 on 29/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 McDonnell Douglas
Model 717-200 Airplanes - Centre Tank
Fuel Booster Pump Container Modification |
| (17/07/2007) FAA issued AD No
2007-13-10 on 29/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 McDonnell Douglas
Model DC-10-30 and DC-10-30F Airplanes
- FUEL TANK SAFETY
- Aft Supplemental Tank Conduit Fuel
Pump Wire Harness Modification |
| (17/07/2007) FAA issued AD No
2007-13-01 on 20/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 McDonnell Douglas
Model 717-200 Airplanes - Pitot Static
Heating System Wiring Modification |
| (17/07/2007) FAA issued AD No
2007-12-23 on 14/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 MD Helicopters,
Inc. (formerly Hughes) Model 369 Series and 500N
helicopters - Landing Gear Strut
Inspection/Replacement & LG Fairing Support Assembly
Rework |
| (17/07/2007) FAA issued AD No
2007-13-17 on 22/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Air Tractor, Inc.
Models AT-602, AT- 802, and AT-802A Airplanes - Cracked
engine mounts |
| (17/07/2007) FAA issued AD No
2007-13-04 on 20/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Boeing Model 747
Series Airplanes - FUEL TANK SAFETY
- Integrated Display System (IDS)
Modification and AFM Change - Centre
Wing Fuel Tank & Horizontal Stabilizer Fuel Tank -
Maintaining Minimum Fuel Levels & De-Fuelling
Procedures |
| (17/07/2007) The State
of Israel CAA issued AD No 55-07-06-07 R1 on 26/06/2007,
to be considered accepted by EASA under provisions of ED
Decision 02/2003 Gulfstream Aerospace L.P. (GALP;
formerly Israel Aircraft Industries) Models 1125 Astra,
Astra SPX and G100 aircraft; Inspection and Replacement
of Horizontal Stabilizer Upper Scissor Fitting Attachment
Bolts.. |
| (17/07/2007) FAA issued AD No
2007-14-03 on 12/07/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Cirrus Design
Corporation Models SR20 and SR22 Airplanes - Cirrus
Airplane Parachute System (CAPS) Pick-Up Collar Support
and Nylon Screws Replacement |
| (02/07/2007) FAA issued AD No
2007-13-02 on 20/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 McDonnell Douglas
Model DC-8-60 and -70 Series Airplanes
- FUEL TANK SAFETY
- Centre Wing Fuel Tank
- Sump Heater, Scavenge Valve and
Scavenge Pump Deactivation |
| (02/07/2007) Transport
Canada issued AD No. CF-2005-28R1 on 14/06/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bell Helicopter Textron Canada
(BHTC), Models 206L-3 and 206L-4 - Power Turbine RPM
Steady State Operation Avoidance |
| (02/07/2007) FAA issued AD No
2007-12-25 on 20/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Gulfstream
Aerospace Corporation Model GIV-X, GV and GV-SP Series
Airplanes - AFM Change; Forward Water
Drain/Supply Valves Functional Checks |
| (02/07/2007) FAA issued AD No
2007-13-05 on 20/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Boeing Model
777-200, 777-200LR, 777-300, and 777- 300ER Series
Airplanes - Flight Control Surfaces
Freeplay Checks/Lubrication |
(02/05/2007) FAA issued
AD No 2007-09-51 on 19/06/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
MD Helicopters, Inc. (formerly Hughes) Model 369 Series
helicopters - Tail Rotor Blade
Assembly Identification/Inspection/Replacement |
 (02/07/2007) JCAB issued AD No TCD
4889-2-2007 on 21/06/2007 to be considered accepted by
EASA under provisions of ED Decision 02/2003
Mitsubishi MU-2 - AFM Change - Engine Torque Indication
System (Torque Transmitter) -
Inspection/Repair/Replacement |
| (02/07/2007) ANAC
Brazil issued AD No. 2004-03-01 R1, effective 09 July
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer EMB-121( )
Aircraft Models in Operation - Inspection of the Nose
Landing Gear Rotating Cylinder |
| (02/07/2007) FAA issued AD No
2007-12-21 on 19/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Hawker Beechcraft
Corporation (formerly Raytheon Aircraft Company) Model
390 Airplanes - Hydraulic Pump Outlet
Tube & Dampener Supports Inspection/Modification |
| (02/07/2007) FAA issued AD No
2007-12-11 on 11/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Boeing Model 747
Series Airplanes - Main Entry Doors
Girt Bar Support Fittings
Inspection/Repair/Replacement |
| (02/07/2007) ANAC
Brazil issued AD No. 2001-04-02 R3, effective 13 July
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer EMB-145( )
and EMB-135( ) Aircraft Models in Operation -
Installation of a placard on the main instrument panel;
and inclusion of the corresponding limitation in the
applicable AFM - Terminating action is
optional |
| (02/07/2007) FAA issued AD No
2007-12-14 on 11/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Boeing Model 727
series Airplanes - Forward Entry Door
Upper & Lower Hinge Cut-out Structure
Inspection/Modification |
| (02/07/2007) FAA issued AD No
2007-11-08 on 22/05/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Hawker Boeing Model
727 series Airplanes - FUEL TANK
SAFETY - Fuel Boost Pump Dry Bay, Electrical Wiring &
Sleeve Inspection/Repair/Operational Test |
| (18/06/2007) FAA issued AD No
2007-12-06 on 11/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Hawker Beechcraft
(formerly Raytheon Aircraft Company; Beech Aircraft
Corporation) Models C90A, B200, B200C, B300, and B300C
Airplanes - Flight Control System -
Inspection |
| (18/06/2007) FAA issued AD No
2007-11-17 on 01/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 Cessna Model 500,
501, 550, 551, S550, 560, 560XL and 750 Airplanes
- Engine/APU Fire Extinguishing
Bottles Wiring Modifications |
| (18/06/2007) FAA issued AD No
2007-12-15 on 14/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 General General
Electric Company (GE) CF34-10E Series Turbofan Engines
- Main Fuel Pump (MFP)
Replacement |
| (18/06/2007) FAA issued AD No
2007-12-09 on 05/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 General Electric
Company (GE) CF34-10E Series Turbofan Engines
- Combustor Case Life Limit
Reduction |
| (18/06/2007) FAA issued AD No
2007-12-02 on 05/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003 McDonnell Douglas
Model DC-8 series Airplanes - Fuel System in-line
Electrical Solenoid Valves along Wing Front Spar
- Bonding Jumpers Installation |
(18/06/2007) FAA issued AD No
2007-12-07 on 06/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
General
Electric Company (GE) CF6-80C2B Series Turbofan Engines
- ECU software version 8.2.Q1
Installation |
| (18/06/2007) ANAC
Brazil issued AD No. 2007-05-01 R1, effective 04 July
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer EMB-145( )
and EMB-135( ) Aircraft Models in Operation - Rework of
the aircraft structure on the forward fuselage LH and RH
sides |
(13/06/2007) FAA issued AD No
2007-11-18 on 31/05/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
General
Electric Company CF6-50C series Turbofan Engines -
Forward Fan Stator Case Rework and Fan Module Secondary
Containment Shield Installation NOTE: This has
resulted in the withdrawal (cancellation) of EASA AD
2004-0007, which addressed the same unsafe
condition. |
(13/06/2007) FAA issued AD No
2007-11-05 on 31/05/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
Sikorsky
Aircraft Corporation Model S- 76A, B and C series
Helicopters - One-time Ultrasonic Inspection of the Main
Rotor Shaft Assembly |
| (13/06/2007) ANAC
Brazil issued AD No. 2007-03-03, effective 10 April 2007,
which is considered accepted by EASA under provisions of
ED Decision 02/2003. Embraer EMB-120( ) Aircraft
Models in Operation - Replacement of the Stall Warning
Computers (SWC) |
(13/06/2007) FAA issued AD No
2007-11-16 on 30/05/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
McDonnell
Douglas Model MD-11 and MD-11F Airplanes
- FUEL TANK SAFETY
- Lower Auxiliary Fuel Tank and
Internal Fuel Pumps Bonding Modifications |
(13/06/2007) FAA issued AD No
2007-11-15 on 30/05/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
McDonnell
Douglas Model DC-10-30, DC-10-30F (KC-10A and KDC-10)
Airplanes; Model DC-10-40 and DC-10-40F Airplanes; and
Model MD-10-10F and MD-10-30F Airplanes
- FUEL TANK SAFETY
- Lower Auxiliary Fuel Tank and
Internal Fuel Pumps Bonding Modifications |
| (13/06/2007) ANAC
Brazil issued AD No. 2007-01-03, effective 22 January
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer EMB-135BJ
Aircraft Model in Operation - Replacement of the valance
panel lighting system wiring |
| (13/06/2007) ANAC
Brazil issued AD No. 2007-01-04, effective 29 January
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer EMB-135BJ
Aircraft Model in Operation - Replacement of the water
and waste system drain masts by new ones bearing a new
P/N |
| (13/06/2007) ANAC
Brazil issued AD No. 2006-03-02R1, effective 27 February
2007, to be considered accepted by EASA under provisions
of ED Decision 02/2003. Embraer ERJ-170( ) aircraft
models in operation - Inclusion of a temporary limitation
to the ANAC-approved Airplane Flight Manual (AFM) to
prohibit a throttle movement into the forward thrust
range immediately following a thrust reverser
application; and installation of new engine
Full-Authority Digital Engine-Control
(FADEC) software. |
(13/06/2007) FAA issued AD No
2007-06-09 on 15/03/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
Boeing Model
737-600, -700, -700C, and -800 Series Airplanes
- Fuselage Point
"D" Splice Fitting
Replacement/Inspection/Repair |
| (13/06/2007) Transport
Canada issued AD No. CF-2007-08 on 04/06/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bombardier Inc. (De Havilland
Canada) Models DHC-8-102, DHC-8-103, DHC-8-106,
DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, DHC-8-314 and
DHC-8-315 aircraft - Incorrect Installation of Elevator
Spring Tab Mechanism Bolts |
| (13/06/2007) Transport
Canada issued AD No. CF-2006-16R1 on 04/06/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bombardier Inc. Models CL-600-1A11,
CL-600-2A12 and CL-600-2B16 - Nose Landing Gear (NLG) and
Nose Gear Door Selector Valves |
| (13/06/2007) Transport
Canada issued AD No. CF-2006-17R1 on 30/05/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bombardier Inc. Model CL-600-2B19 -
AC Contactor Failure - Surface Sealing |
| (11/06/2007) The State
of Israel CAA issued AD No 29-07-01-11 on 28/05/2007, to
be considered accepted by EASA under provisions of ED
Decision 02/2003 Gulfstream Aerospace L.P. Models
GALAXY and G200 aircraft; Visual inspection of hydraulic
lines and attaching blocks for damage and wear.
Replacement of existing blocks made of Teflon to new
blocks made of Nylon 6/6. |
(07/06/2007) FAA issued
AD No 2007-10-12 on 23/05/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Boeing Model
737-200, -300, -400, -500, -600, -700, -800, and -900
Series Airplanes; Boeing Model 757-200 and - 300 Series
Airplanes; and McDonnell Douglas Model DC-10-10,
DC-10-10F, DC-10-30, DC-10-30F, DC-10-40, MD-10-30F,
MD-11, and MD-11F Airplanes; Equipped With Reinforced
Flight Deck Doors Installed in Accordance With
Supplemental Type Certificate (STC) ST01335LA, STC
ST01334LA, and STC ST01391LA, Respectively |
(07/06/2007) FAA issued
AD No 2007-11-13 on 25/05/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
McDonnell
Douglas Model 717-200 Airplanes |
(07/06/2007) FAA issued
AD No 2007-11-01 on 23/05/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Robinson
Helicopter Company Model R44 and R44 II Helicopters |
(07/06/2007) ANAC
Brazil issued 2007-05-02 Corrected, effective June 6,
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003.
This
corrected AD is applicable to all Embraer EMB-120 ()
aircraft models in operation Modification of the aircraft
maintenance plan |
(07/06/2007) FAA issued AD No
2007-11-20 on 05/06/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
General
Electric Company (GE) CF6-80 Series Turbofan Engines
- Fuel Shroud Retaining Rings
Replacement |
| (25/05/2007) FAA issued
AD No 2007-10-01 on 08/05/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003 Air
Tractor, Inc. Model AT-602 Airplanes |
(25/05/2007) FAA issued
AD No 2007-10-15 on 17/05/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Cessna
Aircraft Company Models 208 and 208B Airplanes |
(25/05/2007) FAA issued
AD No 2007-10-09 on 17/05/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Boeing Model
747-400 Series Airplanes |
| (25/05/2007) ANAC
Brazil issued AD No. 2007-03-04, effective April 10,
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer EMB-135BJ
aircraft model in operation Inspection and replacement,
if necessary, of cotton adhesive tapes |
(15/05/2007) FAA issued
AD No 2007-10-03 on 09/05/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Boeing Model
767-200 and -300 Series Airplanes |
(15/05/2007) FAA issued
AD No 2007-10-05 on 10/05/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
General Electric Company (GE) GE90 Series Turbofan
Engines |
(15/05/2007) FAA issued AD No
2007-10-04 on 01/05/2007, to be considered accepted by
EASA under provisions of ED Decision 02/2003
McDonnell
Douglas Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83
(MD-83), DC-9-87 (MD-87), and MD-88 Airplanes |
(15/05/2007) FAA issued
AD No 2007-08-02 on 12/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Hartzell
Propeller Inc. Model HC-E4A-3( )/ E10950( )
Propellers |
(08/05/2007) FAA issued
AD No 2007-06-52 on 30/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Boeing Model
737-800 Series Airplanes |
(08/05/2007) FAA issued
AD No 2007-09-04 on 30/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Boeing Model
777-200, 777-300, and 777- 300ER Series Airplanes |
| (08/05/2007) ANAC
Brazil issued AD No. 2005-09-02R2, effective May 10,
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Inspection and
modification of the rudder-II skin, hinge fittings and
control rods assembly; replacement of the rod end washers
in the rudder-II control rods (both rods, one end per
rod); and installation of springs and washers in the
rudder-II hinge fittings.This Airworthiness Directive is
applicable to all Embraer EMB-145( ) and EMB-135( )
aircraft models in operation. |
(05/05/2007) FAA issued
AD No 2007-08-04 on 12/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
McCauley
Propeller Systems Models 3A32C406/82NDB-X and
D3A32C409/82NDB-X Propellers |
(05/05/2007) FAA issued
AD No 2007-09-03 on 26/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Learjet
Model 45 Airplanes |
(04/05/2007) FAA issued AD No 2007-07-05R1 on 18/04/2007, to be considered accepted by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200, -200LR, -300, and -300ER series Airplanes - Air Supply and Cabin Pressure Controllers (ASCPCs) Software Installation |
|
| (24/04/2007) Transport
Canada issued AD No. CF-2007-03 on 27/03/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bell Helicopter Textron Canada
(BHTC), Models: 206L series and 407. Horizontal
Stabilizer - Manufacturing Flaws |
(24/04/2007) FAA issued
AD No 2007-05-51 on 20/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
MD
Helicopters Inc. (MDHI) Model MD600N Helicopters |
(24/04/2007) FAA issued
AD No 2007-08-08 on 20/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Raytheon
Aircraft Company (The Beech Aircraft Company and BEECH
previously held Type Certificate Nos. 3A15, 3A16, 5A3,
and A-777) Models 35-33, 35-A33, 35-B33, 35-C33, E33,
F33, G33, 35-C33A, E33A, F33A, E33C, F33C, 35, A35, B35,
C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35,
S35, V35, V35A, V35B, 36, A36, A45 (T-34A, B45), D45
(T-34B), 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B (T-
42A), 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC,
58, 95, B95, B95A, D95A, and E95 Airplanes |
(24/04/2007) FAA issued
AD No 2007-08-01 on 09/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
General
Electric Company CT7-5, -7, and -9 Series Turboprop
Engines |
(24/04/2007) FAA issued
AD No 2007-09-01 corrected on 20/04/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Cessna
Aircraft Company Models 182H, 182J, 182K, 182L, 182M,
182N, 182P, 182Q, and 182R Airplanes |
| (24/04/2007) Transport
Canada issued AD No. CF-2007-06 on 10/04/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bombardier Inc. Models DHC-8-101
(not EASA validated), -102, -103, -106, -201, -202, -301,
-311, -314 and -315; Corrosion Prevention and Control
Program (CPCP) |
| (24/04/2007) Transport
Canada issued AD No. CF-2007-05 on 10/04/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bombardier Inc. Models DHC-8-400
(not EASA validated), DHC-8-401 and DHC-8-402, Serial
Numbers 4001, 4003 through 4102. Translating Door
Over-Centering Spring Bracket Failure |
(24/04/2007) FAA issued
AD No 2007-07-02 on 28/09/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Boeing Model
737-300, -400, -500, -600, -700, -800 and -900 Series
Airplanes; and Model 757-200 and -300 Series
Airplanes |
(24/04/2007) Transport
Canada issued AD No. CF-2007-07 on 11/04/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bell Helicopter Textron Canada
(BHTC) Model 430 helicopter serial numbers 49001 through
49122.
Tail Rotor Pitch Change Mechanism |
(24/04/2007) Transport
Canada issued AD No. CF-2007-04 on 05/04/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bell Helicopter Textron Canada
(BHTC) Model 430 helicopter serial numbers 49001 through
49122.
Tail Rotor Pitch Change Mechanism |
(24/04/2007) FAA issued
AD No 2007-08-03 on 12/04/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Cessna
Aircraft Company Models 172R, 172S, 182T, T182T, 206H,
and T206H Airplanes |
(24/04/2007) FAA issued
AD No 2007-07-03 on 28/03/2007, to be considered accepted
by EASA under provisions of ED Decision
02/2003
Boeing Model
747 Airplanes |
| (24/04/2007) Transport
Canada issued AD No. CF-2006-23R1 on 12/03/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bell Helicopter Textron Canada
(BHTC) Model 206 A helicopters, serial numbers 004
through 660; and 672 through 715; and Model 206 B
helicopters, serial numbers 661 through 671 and 716
through 3216, having main rotor latch bolts, part numbers
206-010-169-001/-003 and 206-011-122-003. Main Rotor
Latch Bolts - Removal from Service |
(11/04/2007) Transport
Canada issued AD No. CF-1991-42R1 on 13/03/2007 to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Viking Air Ltd. (formerly Bombardier Inc.)DHC-2Mk.I, Mk.
II and Mk. III Aircraft - Front Spar Centre Web
Cracks
Note: The DHC-2 Mk I and II are Annex II
aircraft and therefore not EASA types. The DHC-2 Mk III
is an EASA type. |
(10/04/2007) FAA issued
AD No 2007-07-04 on 28/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-11 and -11F Airplanes |
(10/04/2007) FAA issued
AD No 2007-07-06 on 03/04/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Columbia Aircraft Manufacturing (Previously the Lancair
Company) Models LC40-550FG, LC41-550FG, and LC42-550FG
Airplanes |
| (10/04/2007) The State
of Israel CAA issued AD No 28-07-02-03 on 07/02/2007, to
be considered accepted by EASA under provisions of ED
Decision 02/2003 Gulfstream Aerospace L.P. Model
Gulfstream 200 Aircraft Serial Numbers 121 thru 154
certificated in any category - Right Fuel standby Pump
Connector (4Q1) Electrical Wiring, Inspection and
Repair |
(10/04/2007) FAA issued
AD No 2007-04-19R1 on 02/04/2007, to be considered
accepted by EASA under provisions of ED Decision
02/2003
Superior Air Parts, Inc. (SAP), Cast
Cylinder Assemblies Part Numbers Series: SA47000L,
SA47000S, SA52000, SA55000, SL32000W, SL32000WH,
SL32006W, SL36000TW, SL36000W, and SL36006W |
(22/03/2007) FAA issued
AD No 2007-06-07 on 15/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon Aircraft Company Models 58 and G58
Airplanes |
(22/03/2007) FAA issued
AD No 2007-03-03 on 31/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, - 300, -400, and -500
Series Airplanes |
(22/03/2007) FAA issued
AD No 2007-02-14 on 25/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, - 800, and -900 Series
Airplanes |
| (20/03/2007) ANAC
Brazil issued AD No. 2006-11-01R1, effective March 21,
2007, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Replacement of the
left hand (LH) and right hand (RH) engines low stage
bleed check valves by new ones |
(20/03/2007) FAA issued
AD No 2007-04-18 on 16/02/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Learjet Model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A,
24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 31,
31A, 35, 35A (C-21A), 36, 36A, 55, 55B, and 55C
Airplanes |
(20/03/2007) FAA issued
AD No 2007-04-17 on 16/02/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15,
DC-10-30, and DC-10-30F (KC-10A and KDC-10) Airplanes;
Model DC-10-40 and DC-10-40F Airplanes Equipped With
Pratt & Whitney JT9-20 or JT9-20J Engines; and Model
MD-10-10F and MD-10-30F Airplanes |
(20/03/2007) FAA issued
AD No 2007-05-17 on 08/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney JT9D Series Turbofan Engines |
(20/03/2007) FAA issued
AD No 2007-05-15 on 12/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Teledyne Continental Motors GTSIO-520 Series
Reciprocating Engines |
(20/03/2007) FAA issued
AD No 2007-05-04 on 05/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Mooney Airplane Company, Inc., (Mooney) Models M20M and
M20R Airplanes |
(20/03/2007) FAA issued
AD No 2007-05-06 on 05/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes |
| (20/03/2007) CAA New
Zealand issued Emergency AD No. AD No. DCA/750XL/12
(Effective March 12, 2007) to be considered accepted by
EASA under provisions of ED Decision 02/2003 Pacific
Aerospace 750XL aircraft [s/n 125, 126 and 127] Autopilot
- Disconnect |
| (19/03/2007) ANAC Brazil issued
Emergency AD 2007-03-02 -
Amdt.39-1177, effective 16 March 2007, to be considered
accepted by EASA under provisions of ED Decision
02/2003 Embraer ERJ-190( ) aircraft models; Visual
inspection of cargo doors; Rework of cargo doors surround
trim liner; and Inspection of fore and aft cargo doors
lateral locking mechanism. |
(10/03/2007) FAA issued
AD No 2007-05-16 on 07/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
General Electric Aircraft Engines (GE) CF34-3A1/-3B/-3B1
Turbofan Engines |
(10/03/2007) FAA issued
AD No 2007-05-10 on 07/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Cessna Aircraft Company Models 172R, 172S, 182S, 182T,
T182T, 206H, and T206H Airplanes |
(10/03/2007) FAA issued
AD No 2007-05-14 on 05/03/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
General Electric Company (GE) CF6-80C2 Turbofan
Engines |
(16/01/2007) FAA issued
AD No 2006-18-15 on 08/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Hartzell Propeller Inc. Model ( )HC-( )2Y( )-( ) series
Propellers - Hub
Inspection/Replacement. NOTE: This AD was reason
for EASA to cancel AD 2006-0092 whose aim was to correct
the same unsafe condition. |
(10/03/2007) FAA issued
AD No 2007-02-06 on 24/02/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney PW2000 Series Turbofan Engines |
| (10/03/2007) The State
of Israel CAA issued AD No 31-07-01-12 on 15/02/2007, to
be considered accepted by EASA under provisions of ED
Decision 02/2003 Gulfstream Aerospace LP models
GALAXY and G200 aircraft; Instrument Panel Wiring Harness
Inspection/Repair. |
| (10/03/2007) The State
of Israel CAA issued AD No 21-07-01-01 on 20/02/2007, to
be considered accepted by EASA under provisions of ED
Decision 02/2003 Gulfstream Aerospace LP models
GALAXY and G200 aircraft; Pressurization Safety Valves
P/N 103842-3 Replacement. |
ANAC Brazil issued AD 2006-09-04R1 -
Amdt 1170 , to be considered accepted by EASA under
provisions of ED Decision 02/2003
Correction Embraer ERJ-190( ) aircraft
models. Effective date 5 February 2007 |
(04/03/2007) FAA issued
AD No 2007-04-26 on 26/02/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney PW4077D, PW4084D, PW4090, and
PW4090-3 Turbofan Engines |
(04/03/2007) FAA issued
AD No 2007-04-16 on 16/02/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767 Airplanes |
(04/03/2007) FAA issued
AD No 2004-23-02 Correction on 16/02/2007, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Correction: Raytheon Aircraft
Company 65, 90, 99, 100, 200, and 1900 Series Airplanes,
and Models 70 and 300 Airplanes |
(04/03/2007) FAA issued
AD No 2007-04-06 on 14/02/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-8-62, DC-8- 63, DC-8-62F, and
DC-8-63F Airplanes |
| (21/02/2007) FAA issued
EAD No 2007-04-51 on 16/02/2007, to be considered
accepted by EASA under provisions of ED Decision
02/2003 General Electric Aircraft Engines (GE)
CF34-3A1/-3B/-3B1 turbofan engines installed on
Bombardier, Inc. CL-600-2B16 (CL-601-3R Variant),
CL-600-2B16 (CL-604 Variant), and CL-600- 2B19 (Regional
Jet Series 100 and 440) model airplanes. |
(06/02/2007) FAA issued
AD No 2007-03-07 on 01/02/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737 Airplanes |
(06/02/2007) FAA issued
AD No 2007-03-01 on 29/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes |
(06/02/2006) Transport
Canada issued AD No. CF-2007-01 on 19/01/2007, effective
on 05/03/2007, to be considered accepted by EASA under
provisions of ED Decision 02/2003
Bell Helicopter Textron Canada (BHTC) Model 206A, 206B,
206L, 206L-1, 206L-3 and 206L-4 helicopters, all serial
numbers, fitted with a CRES steel fitting, part number
(P/N) 407-030-750-103. Upper LH Tailboom Attachment Bolt
- Inspection/Replacement |
(06/02/2007) FAA issued
AD No 2007-02-18 on 29/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767-200 and -300 Series Airplanes |
(06/02/2007) FAA issued
AD No 2007-02-24 on 29/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
| CASA (Australia) issued
AD No AD/GA8-005, Amendment 1, effective on 15/03/2007,
to be considered accepted by EASA under provisions of ED
Decision 02/2003: Gipplands Aeronautics GA8
Aeroplanes - Horizontal Stabiliser
Inspection |
(31/01/2007) FAA issued
AD No 2007-02-23 on 26/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200, -300, and -300ER Series Airplanes -
Gimbal plates of the left and right outboard trailing
edge flaps |
(31/01/2007) FAA issued
AD No 2007-01-10 on 26/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
(31/01/2007) FAA issued
AD No 2007-01-09 on 25/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400,
747-400D, and 747SP Series Airplanes |
(23/01/2007) FAA issued
AD No 2006-26-09 on 04/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-200, -300, -400, and - 500 Series
Airplanes - Support bracket for the air conditioning
outlet extrusion |
| (23/01/2007) CTA Brazil
AD No.2007-01-01, effective January 29, 2007 to be
considered accepted by EASA under provisions of ED
Decision 02/2003 AEROMOT AMT-100,-200,-300
Replacement of the EVANS NPG+coolant liquid, application
of new red lines on the engine cylinder head temperature
gauge, replacement of the engine radiator cap, amendment
of the Airplane Flight Manual (AFM) |
| (23/01/2007) CTA Brazil
AD 2007-01-02 , effective January 15, 2007 to be
considered accepted by EASA under provisions of ED
Decision 02/2003 EMBRAER ERJ-170() Aircraft Models
Inspection of the fuel quantity probes harnesses and
correct reassembly |
(23/01/2007) FAA issued
AD No 2006-22-05 on 27/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Honeywell Primus II RNZ-850( ) and -851( ) series
Integrated Navigation Units -
Navigation Receiver Module (NRM)
Inspection/Modification. |
(22/01/2007) FAA issued
AD No 2007-01-02 on 10/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-11 and -11F Airplanes - Power
feeder cables of the integrated drive generator
(IDG) |
(16/01/2007) FAA issued
AD No 2007-15-01 on 12/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747- 100B SUD, 747-200B,
747-200C, 747-200F, 747-300, 747SR, and 747SP Series
Airplanes Equipped with General Electric CF6-45 or -50
Series Engines, or Equipped with Pratt & Whitney
JT9D-3 or -7 (Excluding -70) Series Engines |
| CAA New Zealand issued
AD No. AD No. DCA/R2000/37A (Revised Dec 21 2006) to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Alpha Aviation (Avions Pierre Robin;
APEX) HR 200 and R 2000 series -
"Wing Spars -
Inspection and Repair" |
(14/01/2007) FAA issued
AD No 2006-26-13 on 08/01/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 707-100 Long Body, -100B Long Body, -100B
Short Body, -E3F, -300, -300B, and -300C Series
Airplanes; Model 727-100 and -200 Series Airplanes; Model
737-200, - 200C, -300, -400, and -500 Series Airplanes;
Model 747-100B, 747-200B, 747-200C, 747-200F, 747-300,
747-400, 747-400D, 747SR, and 747SP Series Airplanes;
Model 757-200 and 757-200PF Series Airplanes; and Model
767- 200 and -300 Series Airplanes; Equipped With
Observer or Attendant Seats |
(11/01/2007) FAA issued
AD No 2006-26-06 on 27/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200 and -300 Series Airplanes Equipped
with Rolls-Royce Engines |
JCAB issued AD No
TCD-7030-2006 on 27/12/2006 to be considered accepted by
EASA under provisions of ED Decision 02/2003
Mitsubishi MU-2 - Centre-to-Outer Wing Attachment
Hardware & Parts - Inspection/Rework/Replacement |
(11/01/2007) FAA issued
AD No 2006-24-05 on 27/11/2007, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
| (04/01/2007) CTA Brazil
AD No.2006-09-03R1 , effective January 4, 2007 to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Embraer EMB-145( ) and EMB-135( )
aircraft Inspection/Replacement of the Engine Anti-icing
System Valves and Tubes |
| (04/01/2007) CTA Brazil
AD No. 2006-07-03R1, effective January 4, 2007 to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Embraer EMB-135BJ aircraft Rework,
modification and re-identification of the aft and forward
auxiliary fuel tanks |
(04/01/2007) FAA issued
AD No 2006-24-10 (Correction) on 04/12/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Air Tractor, Inc. Models AT-501, AT- 502, AT-502A,
AT-502B, and AT-503A Airplanes |
(04/01/2007) FAA issued
AD No 2006-23-09 (Correction) on 29/11/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Correction: Air Tractor, Inc. Model AT-602 Airplanes |
(26/12/2006) FAA issued
AD No 2006-25-12 on 19/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Rolls-Royce Corporation 501-D Series Turboprop Engines -
Removal from service of certain turbine rotor
components |
(26/12/2006) FAA issued
AD No 2006-25-13 on 14/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Rolls-Royce Corporation AE 2100D3 Turboprop Engines -
Compressor cone shaft assemblies |
(20/12/2006) FAA issued
AD No 2006-26-01 on 19/12/2006, to be considered accepted
by EASA under provisions of ED Decision
02/2003.
CFM International, S.A. CFM56-2, -3, -5, -5B, -5C, and
-7B series Engines - Fuel Filter
Identification/Replacement.
Note: The affected fuel filters are
not part of the original type design approval as awarded
to CFM International. They were manufactured under U.S.
parts manufacturer approvals (PMA), held by Western
Filter Corporation (Valencia, California, USA) and PTI
Technologies, Inc. (Oxnard, California, USA). For this
reason, ED Decision 02/2003 applies and the FAA AD is
applicable to aircraft registered in an EU member
state. |
(18/12/2006) FAA issued
AD No 2006-25-11 on 12/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Lockheed Model L-1011 Series Airplanes - C112 harness
clamp assembly |
(18/12/2006) FAA issued
AD No 2006-25-09 on 12/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-11F Airplanes - Auxiliary
power unit (APU) power feeder wires |
(18/12/2006) FAA issued
AD No 2006-25-08 on 11/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Columbia Aircraft Manufacturing Models LC41-550FG and
LC42-550FG Airplanes - Deice system |
(11/12/2006) FAA issued
AD No 2006-25-05 on 07/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 777 Airplanes - Fuselage skin under the
forward and aft wing-to-body fairings |
(11/12/2006) FAA issued
AD No 2006-25-02 on 07/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Gulfstream Model G-159 Airplanes |
| (07/12/2006) CTA Brazil
AD No. 2006-03-01_R1, effective December 15, 2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Amdt 1153 - Applicable to Embraer
EMB-145( ) and EMB-135( ) aircraft models Inspection on
the Fuel Quantity Indication System (FQIS) and DC Fuel
Pump Harnesses |
(07/12/2006) FAA issued
AD No 2006-25-01 on 04/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
International Aero Engines AG (IAE) V2522-A5, V2524-A5,
V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5
Turbofan Engines. Master magnetic chip detector
(MCD) |
(07/12/2006) FAA issued
AD No 2006-24-11 on 04/12/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon Aircraft Company Models 1900, 1900C, and 1900D
Airplanes Forward, vertical, and aft flanges |
(05/12/2006) FAA issued
AD No 2006-24-04 on 27/11/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767 Airplanes. High frequency eddy current
(HFEC) inspections |
(29/11/2006) FAA issued
AD No 2006-18-01 on 29/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
MD Helicopters, Inc. Model MD900 Helicopters |
| (29/11/2006) ANAC
Brazil issued AD No. 2006-11-02, effective November 16,
2006, which is considered accepted by EASA under
provisions of ED Decision 02/2003. Embraer ERJ-170
series - Auto Flight - Functional
check of the Flight Guidance Control System. |
 (27/11/2006) DNA
(Argentina) issued AD No RA 2006-06-01_R1 on 17/11/2006,
to be considered accepted by EASA under provisions of ED
Decision 02/2003
LAVIA S.A. (Piper; Chincul) PA-25 "Pawnee" series
aeroplanes - Horizontal Stabilizer Support Structure -
Inspection/Repair/Modification |
(27/11/2006) FAA issued
AD No 2006-24-01 on 21/11/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Cessna Model 750 Airplanes |
(27/11/2006) FAA issued
AD No 2006-23-14 on 16/11/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Air Tractor, Inc. Models AT-502, AT- 502A, AT-502B,
AT-602, AT-802, and AT-802A Airplanes |
(27/11/2006) FAA issued
AD No 2006-24-02 on 22/11/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747- 200B, 747-200C,
747-200F, 747SR, and 747SP Series Airplanes |
(27/11/2006) FAA issued
AD No 2006-22-01 on 27/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757-200, -200CB, and -300 Series
Airplanes. |
(27/11/2006) FAA issued
AD No 2006-23-15 on 16/11/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes. |
(20/11/2006) FAA issued
AD No 2006-15-11 on 25/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
CASA (Construcciones Aeronauticas, S.A.) Model C-212-CC
aeroplanes, if modified per STC ST02177AK, held by Flight
Alaska, Inc. - Note: At the time of publication, EASA
records indicate that Flight Alaska, Inc. STC ST02177AK
has not been approved or accepted by any EU Member
State. |
(14/11/2006) FAA issued
AD No 2006-22-08 on 27/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Air Tractor, Inc. Models AT-602, AT- 802, and AT-802A
Airplanes |
(09/11/2006) FAA issued
AD No 2006-23-05 on 07/11/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Cessna Model 750 Airplanes |
(09/11/2006) FAA issued
AD No 2006-22-15 on 06/11/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
(09/11/2006) FAA issued
AD No 2006-22-13 on 02/11/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney PW4074, PW4074D, PW4077, PW4077D,
PW4084D, PW4090, PW4090-3, and PW4098 Turbofan
Engines |
| (09/11/2006) ANAC Brazil issued AD No. 2006-10-03,
effective November 1, 2006, which is considered accepted
by EASA under provisions of ED Decision 02/2003. Embraer ERJ-190 series; Note: The AD
has been issued to owners but not as yet posted to our
Web page. |
(09/11/2006) ANAC Brazil issued AD No.
2006-10-02, effective November 1, 2006, which is
considered accepted by EASA under provisions of ED
Decision 02/2003. Embraer ERJ-170 series; Note: The AD has been issued to
owners but not as yet posted to our Web page. |
 (07/11/2006) FOCA
(Switzerland) issued AD HB-2006-444 on 14/11/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Pilatus - PC-12 - EXECUTIVE SEAT LEGS
- Identification, Replacement |
(07/11/2006) FAA issued
AD No 2006-18-17 on 08/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400, 747-400D, and 747-400F Series
Airplanes |
(07/11/2006) FAA issued
AD No 2006-16-11 on 09/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-700 and 737-800 Series Airplanes |
(07/11/2006) FAA issued
AD No 2006-18-08 on 06/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Goodyear Aviation Tires, Part Number 217K22-1, Installed
on Various Transport Category Airplanes, Including But
Not Limited to Bombardier Model BD-700-1A10 and
BD-700-1A11 Airplanes; and Gulfstream Model G-1159,
G-1159A, G-1159B, G-IV, GIV-X, GV, and GV-SP Series |
(07/11/2006) FAA issued
AD No 2006-15-01 on 17/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Twin Commander Aircraft Corporation Models 690, 690A, and
690B Airplanes |
(07/11/2006) FAA issued
AD No 2006-15-12 on 25/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
CASA (Construcciones Aeronauticas, S.A.) Model C-212-CC
aeroplanes, if modified per STC ST02129AK, held by
Evergreen Alaska, Inc. - Note: At the time of
publication, EASA records indicate that Evergreen Alaska,
Inc. STC ST02129AK has not been approved or accepted by
any EU Member State. |
CASA (Australia) issued
AD No AD/GAF-N22-069 on 26/10/2006, to be considered
accepted by EASA under provisions of ED Decision
02/2003
GAF N22 and N24 Series Aeroplanes |
(03/11/2006) FAA issued
AD No 2006-22-12 on 27/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Hartzell Propeller Inc. Model HC-B5MP- 3( )/M10282A( )+6
and HC-B5MP-3( )/M10876( )( )( )( ) Five-Bladed
Propellers |
(03/11/2006) FAA issued
AD No 2006-22-09 on 27/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
(02/11/2006) Transport
Canada issued AD No. CF-2006-22 on 26/10/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Fuel Manifold Leakage |
(02/11/2006) FAA issued
AD No 2006-21-06 on 25/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-10 Series Airplanes; DC-9-20
Series Airplanes; DC-9-30 Series |
(02/11/2006) FAA issued
AD No 2006-17-08 on 23/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney PW4077D, PW4084D, PW4090, and
PW4090-3 Turbofan Engines |
(02/11/2006) FAA issued
AD No 2006-21-05 on 18/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400, 777-200, and 777- 300 Series
Airplanes |
(28/10/2006) FAA issued
AD No 2006-08-08(Correction) on 12/05/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Air Tractor, Inc. Models AT-400; AT- 401, AT-401B,
AT-402, AT-402A, and AT-402B |
(28/10/2006) FAA issued
AD No 2006-16-06 on 18/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
General Electric Company (GE) CF6-80 Series Turbofan
Engines |
(28/10/2006) FAA issued
AD No 2006-16-09 on 09/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-90-30 Airplanes |
(28/10/2006) FAA issued
AD No 2006-10-04 on 12/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-200B, 747-200C, 747- 200F, 747-300,
747-400, and 747SP Series Airplanes |
(23/10/2006) FAA issued
AD No 2006-21-09 on 19/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200 Series Airplanes equipped with
General Electric GE90-94B Engines |
(20/10/2006) FAA issued
AD No 2006-14-07 on 17/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, and -200C Series
Airplanes |
(18/10/2006) CTA
Brazil AD No. 2006-02-03_R2, effective October 8, 2006,
to be considered accepted by EASA under provisions of
ED Decision 02/2003
Fuel Tank Electrical Bonding Clamps Replacement |
(18/10/2006) FAA issued
AD No 2006-21-03 on 13/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Cirrus Design Corporation Models SR20 and SR22
Airplanes |
(16/10/2006) FAA issued
AD No 2006-20-10 on 29/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Air Tractor, Inc. Models AT-802 and AT- 802A
Airplanes |
(16/10/2006) FAA issued
AD No 2006-19-03 on 12/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10 and DC-10-10F Airplanes;
Model DC-10-15 Airplanes; Model DC-10-30 and DC- 10-30F
(KC-10A and KDC-10) Airplanes; Model DC-10-40 and
DC-10-40F Airplanes; Model MD-10-10F and MD-10-30F
Airplanes; and Model MD-11 and MD-11F Airplanes |
(16/10/2006) FAA issued
AD No 2006-20-51 on 11/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200LR series airplanes powered by
General Electric (GE) Model GE90-110B engines, and Model
777-300ER series airplanes powered by GE Model GE90-115B
engines |
(16/10/2006) FAA issued
AD No 2006-20-11 on 04/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757-200, -200PF, and - 200CB Series
Airplanes |
(10/10/2006) FAA issued
AD No 2006-20-12 on 04/10/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model 717-200 Airplanes |
| (10/10/2006) Transport
Canada issued AD No. CF-2006-21R1 on 03/10/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Horizontal Stabilizer Trim -
Uncommanded Motion |
| (09/10/2006) Transport
Canada issued AD No. CF-2006-20R1 on 04/10/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003 Bombardier Inc. Model CL-600-2B19 -
Horizontal Stabilizer Trim Uncommanded Motion |
(05/10/2006) Transport
Canada issued AD No. CF-85-08_R4 on 28/09/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Stress Corrosion Cracking in the Wing Lift Strut Lower
Clevis Fitting |
(05/10/2006) FAA
issued AD No 2006-20-09 on 29/09/2006, to be considered
accepted by EASA under provisions of ED Decision
02/2003
Lycoming Engines (L)O-360, (L)IO-360, AEIO-360, O-540,
IO-540, AEIO-540, (L)TIO-540, IO-580, and IO-720 Series
Reciprocating Engines |
(05/10/2006) FAA issued
AD No 2006-10-17 on 18/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, - 800, and -900 Series
Airplanes |
(05/10/2006) FAA issued
AD No 2006-18-05 on 06/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-14, DC-9- 15, and DC-9-15F
Airplanes; Model DC-9-21 Airplanes; Model DC-9-30 Series
Airplanes; Model DC-9-41 Airplanes; and Model DC-9-51
Airplanes |
(05/10/2006) FAA issued
AD No 2006-20-07 on 28/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Rolls-Royce Corporation Models 250-C30, 250-C40, and
250-C47 Series Turboshaft Engines |
(05/10/2006) FAA issued
AD No 2006-20-02 on 28/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
(04/10/2006) FAA issued
AD No 2006-17-15 on 25/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10 and DC-10-10F Airplanes;
and Model MD-10-10F Airplanes |
CASA (Australia) issued
AD No AD/GA8/4 on 03/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Gippsland GA8 Airplanes - Seat Track
Stops Modification |
(27/09/2006) FAA issued
AD No 2006-18-11 on 12/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-200, -300, -400, and - 500 Series
Airplanes Equipped With an Auxiliary Fuel |
(27/09/2006) FAA issued
AD No 2006-14-08 on 17/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Mitsubishi MU-2B series Airplanes -
Flight Idle Blade Angle Settings |
JCAB issued AD No
TCD-6832-2006 on 10/04/2006; to be considered accepted by
EASA under provisions of ED Decision 02/2003
Fuji Heavy Industries, Ltd. Model FA-200 series
aeroplanes - Wing Spar Flange
- Inspection/Repair. |
(27/09/2006) FAA issued
AD No 2006-19-10 on 19/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Cirrus Design Corporation Models SR20 and SR22 |
(27/09/2006) FAA issued
AD No 2006-19-09 on 19/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon Aircraft Company Model B300 Airplanes |
(19/09/2006) FAA issued
AD No 2006-09-03 on 26/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 727, 727C, 727-100, and 727-100C Series
Airplanes |
(19/09/2006) FAA issued
AD No 2006-07-17 on 07/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 727, 727C, 727-100, 727- 100C, and 727-200
Series Airplanes |
CAA New Zealand issued
AD No. DCA/R2000/39, effective on 31 August 2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Alpha Aviation (Avions Pierre
Robin; APEX) HR200 and R2000 series -
"Fuel Shut-Off Mechanism
- Inspection and
Rework" |
CAA New Zealand issued
AD No. DCA/R2000/38, effective on 29 June 2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Alpha Aviation (Avions Pierre Robin; APEX) HR200 and
R2000 series -
"Cabin Compartment Barrier
- Inspection and
Modification" |
(11/09/2006) FAA issued
AD No 2006-18-16 on 08/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon Aircraft Company Model 390 Airplanes |
(11/09/2006) FAA issued
AD No 2006-18-13 on 08/09/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Gulfstream Model GV and GV-SP Series Airplanes |
CAA New Zealand issued
AD No. DCA/750XL/8 on 31 August 2006, to be considered
accepted by EASA under provisions of ED Decision
02/2003
Pacific Aerospace Corporation 750 XL - Fuselage Roof,
Station 180.85 - Inspection and
Repair" |
(11/09/2006) FAA issued
AD No 2006-18-02 on 30/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-10, -20, - 30, -40, and -50
Series Airplanes |
(11/09/2006) FAA issued
AD No 2006-16-15 on 18/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model MD-10-10F and MD-10-30F Airplanes
and Model MD-11 and MD-11F Airplanes |
(06/08/2006) Transport
Canada issued AD No. CF-2005-14R1 on 08/05/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Models DHC-8-400, DHC-8-401 and DHC-8-402
- Inspection of Fire Bottle Electrical Connectors |
(04/09/2006) FAA issued
AD No 2006-07-10 on 03/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 727 Airplanes |
(05/08/2006) Transport
Canada issued AD No. CF-2006-19 on 28/07/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Model CL-600-2B19 - Engine Exhaust Nozzle
In-Flight Loss |
(04/09/2006) FAA issued
AD No 2006-11-17 on 02/06/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Eurocopter (France) AS350 helicopters, if modified per
STC SH4747NM, held by Geneva Aviation, Inc.- Note: At the
time of publication, EASA records indicate that Geneva
Aviation, Inc. STC SH4747NM has not been approved or
accepted by any EU Member State. |
(04/09/2006) FAA issued
AD No 2006-17-07 on 30/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney JT8D-1, -1A, -1B, -7, - 7A, -7B, -9,
-9A, -11, -15, -15A, -17, -17A, -17R, -17AR, -209, -217,
- 217A, -217C, and -219 Turbofan Engines |
(01/09/2006)FAA issued
Emergency AD No 2006-18-51 on 31/08/2006 to be considered
accepted by EASA under provisions of ED decision
02/2003
Raytheon Aircraft Company (formerly Beech Aircraft
Corporation) Model 1900, 1900C and 1900D airplanes - Wing
Rear Spar Lower Caps Inspection/Repair |
(29/08/2006) FAA issued
AD No 2006-17-11 on 23/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767-400ER Series Airplanes and Model 777-200
and -300 Series Airplanes |
(29/08/2006) FAA issued
AD No 2006-16-04 on 03/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Rolls-Royce Corporation (Formerly Allison Engine Company,
Allison Gas Turbine Division, and Detroit Diesel Allison)
(RRC) 250-B and 250-C Series Turboshaft and Turboprop
Engines |
(29/08/2006) FAA issued
AD No 2006-12-26 on 21/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Correction: Boeing Model 777-200-300 and 300ER Series
Airplanes |
(29/08/2006) FAA issued
AD No 2006-15-13 on 26/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McCauley Propeller Systems Propeller Models
B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0 |
(28/08/2006) FAA issued
AD No 2006-15-08 on 20/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Honeywell International Inc. - TPE331 Series Turboprop
Engines |
(24/08/2006) FAA issued
AD No 2006-15-07 on 20/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Mitsubishi Heavy Industries, Ltd. MU-2B Series
Airplanes |
(24/08/2006) FAA issued
AD No 2006-17-01 on 18/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Mitsubishi Heavy Industries MU-2B Series Airplanes |
(24/08/2006) FAA issued
AD No 2006-17-04 on 18/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
The Cessna Aircraft Company Models 172R, 172S, 182T,
T182T, 206H, and T206H Airplanes |
(23/08/2006) FAA issued
AD No 2006-17-05 on 18/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Mitsubishi Heavy Industries MU-2B Series Airplanes |
(22/08/2006) FAA issued
AD No 2006-16-18 on 21/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Sandel Avionics Incorporated Model ST3400 Terrain
Awareness Warning System/Radio Magnetic Indicator (TAWS/
RMI) Units Approved Under Technical Standard Order(s)
C113, C151a, or C151b; Installed on Various Small and
Transport Category Airplanes |
(22/08/2006) FAA issued
AD No 2006-16-12 on 09/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-30,
DC-10-30F (KDC-10), DC-10-40, and DC-10-40F
Airplanes |
(22/08/2006) FAA issued
AD No 2006-16-03 on 03/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15,
DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, and
DC-10-40F Airplanes |
(21/08/2006) FAA issued
AD No 2006-15-05 on 20/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-200, -300, and -400 Series
Airplanes |
(21/08/2006) Transport
Canada issued AD No. CF-2006-18 on 15/08/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
All Bombardier Inc./Viking Air Ltd., models DHC-7-1, 100,
and 150 aircraft |
(21/08/2006) FAA issued
AD No 2006-11-14 on 31/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Sikorsky Aircraft Corporation Model S- 92A
Helicopters |
(21/08/2006) FAA issued
AD No 2006-12-11 on 12/06/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, - 800, and -900 Series
Airplanes |
(21/08/2006) FAA issued
AD No 2006-11-07 on 25/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon Model Hawker 800XP Airplanes |
(21/08/2006) FAA issued
AD No 2000-11-19 R1 on 12/06/2006, to be considered
accepted by EASA under provisions of ED Decision
02/2003
Revision: Boeing Model 767-200 and -300 Series
Airplanes |
(21/08/2006) FAA issued
AD No 2006-11-11 on 26/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes |
(21/08/2006) FAA issued
AD No 2006-11-06 on 25/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767-200 and -300 Series Airplanes |
(21/08/2006) FAA issued
AD No 2006-11-12 on 26/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767 Airplanes |
(21/08/2006) FAA issued
AD No 2006-12-10 on 12/06/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-400 Series Airplanes |
(21/08/2006) FAA issued
AD No 2006-12-03 on 07/06/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100B, 747-200B, 747- 200F, 747-300,
747-400, 747-400F, and 747SP Series Airplanes |
(21/08/2006) FAA issued
AD No 2006-12-06 on 07/06/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400, -500, -700, and -800 Series
Airplanes; Model 747-400 and -400F Series Airplanes;
Model 757-200 Series Airplanes; Model 767-300 Series
Airplanes; and Model 777-300 Series Airplanes Equipped
With Certain Driessen or Showa Galleys or Driessen
Closets |
(16/08/2006) FAA issued
AD No 2006-11-07 on 25/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon Model Hawker 800XP Airplanes |
(16/08/2006) FAA issued
AD No 2006-16-02 on 03/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82),
DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88
Airplanes |
(16/08/2006) FAA issued
AD No 2006-15-15 on 31/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-81 (MD- 81), DC-9-82
(MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88
Airplanes |
(16/08/2006) FAA issued
AD No 2006-16-01 on 31/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Hamilton Sundstrand Model 14RF-19 Propellers |
(16/08/2006) FAA issued
AD No 2006-15-16 on 31/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon (Beech) Model 400 and 400A Series Airplanes |
(16/08/2006) FAA issued
AD No 2006-15-18 on 31/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-300, -400, -500, -600, -700, -700C,
-800, and -900 Series Airplanes |
(14/08/2006) FAA issued
AD No 2006-16-05 on 31/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Pratt & Whitney PW4164, PW4168, and PW4168A Series
Turbofan Engines |
(14/08/2006) FAA issued
AD No 2006-16-10 on 09/08/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-200B, 747-200C, 747-200F, 747-300, and
747SR Series Airplanes |
(13/07/2006) FAA issued
AD No 2006-13-17 on 31/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757-200 Series Airplanes Modified by
Supplemental Type Certificate (STC) SA979NE |
(18/07/2006) FAA issued
AD No 2006-11-16 on 31/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Honeywell International Inc. T5311A, T5311B, T5313B,
T5317A, T5317A-1, and T5317B Series Turboshaft Engines
and Lycoming Former Military T53-L-11B, T53-L-11D,
T53-L-13B, T53-L-13B/D, and T53-L-703 Series Turboshaft
Engines |
(18/07/2006) FAA issued
AD No 2006-14-03 on 05/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Honeywell International Inc. TPE331 Series Turboprop, and
TSE331-3U Model Turboshaft Engines |
(17/07/2006) FAA issued
AD No 2006-13-13 (Correction) on 03/07/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Boeing Model 737 Airplanes |
(13/07/2006) FAA issued
AD No 2006-13-18 on 05/07/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-31, DC-9-32, DC-9-32F,
DC-9-33F, DC-9-34, and DC-9-34F Airplanes; and Model
DC-9-40 and DC-9-50 Series Airplanes |
(07/07/2006) CTA Brazil
AD No. 2004-12-03R1 corrected on 27/07/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
2004-12-03R1 - EMBRAER - Amendment 39-1145 |
(07/07/2006) CTA Brazil
AD No. 2005-08-04R1 on 27/07/2006, to be considered
accepted by EASA under provisions of ED Decision
02/2003
2005-08-04R1 - EMBRAER - Amendment 39-1144 |
(07/07/2006) CTA Brazil
AD No. 2006-06-03 on 07/07/2006, to be considered
accepted by EASA under provisions of ED Decision
02/2003
2006-06-03 - EMBRAER - Amendment 39-1143 |
(26/06/2006) FAA issued
AD No 2006-13-10 on 26/06/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Raytheon Aircraft Company 65, 90, 99, and 100 Series
Airplanes |
(26/06/2006) CTA Brazil
AD No. 2006-06-01 on 28/06/2006, to be considered
accepted by EASA under provisions of ED Decision
02/2003
EMBRAER - Amendment 39-1141 |
(26/06/2006) FAA issued
AD No 2006-12-19 on 13/06/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Hamilton Sundstrand Model 14RF-19 Propellers |
(26/06/2006) FAA issued
AD No 2006-11-13 on 26/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 777-200 and -300 Series Airplanes |
(14/06/2006) Transport
Canada issued AD No. CF-2006-05 on 31/03/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. DHC-8 Aircraft Models 400, 401 and 402,
serial numbers 4003, 4004, 4006, 4008 through 4064, 4072
and 4073. |
(14/06/2006) FAA issued
AD No 2006-12-08 on 12/06/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Goodrich Evacuation Systems Approved Under Technical
Standard Order (TSO) TSO-C69b and Installed on Airbus
Model A330-200 and -300 Series Airplanes, Model A340-200
and -300 Series Airplanes, and Model A340-541 and -642
Airplanes |
(14/06/2006) FAA issued
AD No 2006-10-14 on 17/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30,
DC-9-40, and DC-9-50 Series Airplanes; Model DC-9-81
(MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87
(MD-87) Airplanes; Model MD-88 Airplanes; Model MD-90-30
Airplanes; and Model 717-200 Airplanes |
(14/06/2006) FAA issued
AD No 2006-10-16 on 17/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
(12/06/2006) Transport
Canada issued AD No. CF-2006-09 on 08/05/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. DHC-8 Models 102, 103, 106, 201, 202,
301, 311, 314 and 315, Serial Numbers 003 through
579 |
(12/06/2006) Transport
Canada issued AD No. CF-2006-08 on 26/04/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Models DHC-8-400, DHC-8-401 and
DHC-8-402, Serial Numbers 4001, 4003 and subsequent. |
(12/06/2006) FAA issued
AD No 2006-10-14 on 17/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30,
DC-9-40, and DC-9-50 Series Airplanes; Model DC-9-81
(MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87
(MD-87) Airplanes; Model MD-88 Airplanes; Model MD-90-30
Airplanes; and Model 717-200 Airplanes |
(12/06/2006) FAA issued
AD No 2006-10-21 on 18/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Correction: Engine Components Incorporated (ECi)
Reciprocating Engine Connecting Rods |
(12/06/2006) FAA issued
AD No 2006-11-03 on 25/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Gulfstream Model GV and GV-SP Series Airplanes |
(12/06/2006) FAA issued
AD No 2006-10-21 on 18/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Engine Components Incorporated (ECi) Reciprocating Engine
Connecting Rods |
(01/06/2006) Transport
Canada issued AD No. CF-2006-06 on 04/04/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Model DHC-8-400, DHC-8-401 and DHC-8-402
Serial Numbers 4001 |
(01/06/2006) FAA issued
AD No 2006-05-20 on 22/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B,
747-200F, 747-300, 747-400, 747-400D, 747SP, 747SR,
767-200, 767-300, 777-200, 777-300, and 777-300ER Series
Airplanes |
(01/06/2006) FAA issued
AD No 2006-08-09 (Correction) on 12/05/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Correction: Air Tractor, Inc. Models AT-802 and AT- 802A
Airplanes |
(01/06/2006) FAA issued
AD No 2006-08-02 on 12/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-200C and -200F Series Airplanes |
(01/06/2006) FAA issued
AD No 2006-06-10 on 22/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B,
747-200C, 747-300, 747-400, 747-400D, and 747SR Series
Airplanes |
(01/06/2006) FAA issued
AD No 2006-06-11 on 22/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400,
and 747-400D Series Airplanes |
(01/06/2006) FAA issued
AD No 2006-10-02 on 08/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747 Airplanes |
(01/06/2006) FAA issued
AD No 2006-09-06 on 03/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B,
747-300, 747-400, 747-400D, and 747SR Series
Airplanes |
(01/06/2006) FAA issued
AD No 2006-09-01 on 19/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B,
747-200C, 747-200F, 747-300, 747SR, and 747SP Series
Airplanes |
(01/06/2006) Transport
Canada issued AD No. CF-2006-07 on 25/04/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Model CL-600-2B19, serial number 7003
thru 7990 and, 8000 and subsequent |
(01/06/2006) Transport
Canada issued AD No. CF-2006-04 on 28/04/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Bombardier Inc. Model CL-600-2B19, all serial
numbers |
(01/06/2006) FAA issued
AD No 2006-10-15 on 16/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Learjet Model 45 Airplanes |
(01/06/2006) FAA issued
AD No 2006-10-08 on 15/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767-200, -300, and -300F Series
Airplanes |
(31/05/2006) FAA issued
AD No 2006-09-09 on 03/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767 Airplanes |
(31/05/2006) FAA issued
AD No 2006-09-02 on 26/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757-200 and -200PF Series Airplanes Equipped
With Pratt & Whitney Engines |
(31/05/2006) FAA issued
AD No 2006-08-04 on 13/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767 Airplanes |
(31/05/2006) FAA issued
AD No 2006-07-21 on 11/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes Powered by Pratt & Whitney
Engines |
(31/05/2006) FAA issued
AD No 2006-07-23 on 11/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757 Airplanes |
(31/05/2006) FAA issued
AD No 2006-07-24 on 11/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 757-200 and -300 Series Airplanes |
(31/05/2006) FAA issued
AD No 2006-07-14 on 07/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 767-200, -300, and -300F Series
Airplanes |
(31/05/2006) FAA issued
AD No 2006-07-25 on 11/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-8-11, DC-8-12, DC-8-21,
DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43
Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model
DC-8-50, -60, -60F, -70, and -70F Series Airplanes; Model
DC-9-10, -20, -30, -40, and -50 Series Airplanes; Model
DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and
DC-9-87 (MD-87) Airplanes; and Model MD-88 Airplanes |
(31/05/2006) FAA issued
AD No 2006-07-11 on 31/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82),
DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD- 90-30
Airplanes |
(31/05/2006) FAA issued
AD No 2006-07-08 on 31/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30,
DC-9-40, and DC-9-50 Series Airplanes |
(31/05/2006) FAA issued
AD No 2006-06-06 on 19/05/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
The Cessna Aircraft Company Models 208 and 208B
Airplanes |
(31/05/2006) FAA issued
AD No 2006-03-08 on 07/02/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Aero Advantage ADV200 Series (Part Numbers ADV211CC and
ADV212CW) Vacuum Pumps |
(31/05/2006) FAA issued
AD No 2006-07-04 on 30/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-600, -700, -700C, - 800, and -900 Series
Airplanes |
(23/05/2006) FAA issued
AD No 2006-07-12 on 31/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 737-100, -200, -200C, -300, -400, and -500
Series Airplanes |
(23/05/2006) FAA issued
AD No 2006-04-13 on 13/04/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Gulfstream Model GIV-X and GV-SP Series Airplanes |
(20/04/2006) FOCA
(Switzerland) issued AD HB-2006-224 on 20/04/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
Model PC-9, PC-9/A, PC-9/B and PC-9/F airplanes
Manufacturers Serial Numbers (MSN) 101 thru MSN 247
inclusive and MSN 501 thru MSN 567 inclusive that do not
have the PILATUS PC-9 Service Bulletin No. 29-010
embodied. |
(18/04/2006) FAA issued
AD No AD 2006-05-08 on 09/03/2006, to be considered
accepted by EASA under provisions of ED Decision
02/2003
Boeing Model 777-200 series airplanes, certificated in
any category; as identified in Boeing Special Attention
Service Bulletin 777-28-0045, dated September 1,
2005.
 Link to PDF of AD on the FAA
website |
(18/04/2006) FOCA
(Switzerland) issued AD HB-2006-223 on 20/04/2006, to be
considered accepted by EASA under provisions of ED
Decision 02/2003
PILATUS AIRCRAFT LTD. All Model PC-12 and PC-12/45
airplanes, Manufacturer Serial Number (MSN) 101 through
MSN 617 inclusive. |
(31/03/2006) FAA issued
AD No 2006-05-09 on 09/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Certain Boeing Model 747-200C, -200F, -400, -400D and
-400F Series airplanes - inspection for cracks in
fuselage skin sections 41,42,46
 Link to AD on FAA
website |
(31/03/2006) FAA issued
AD No 2006-05-06 on 09/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Certain Boeing Model 747 airplanes -
inspection/modification of BS2598 bulkhead
structure
Link to AD on FAA
website |
(31/03/2006) FAA issued
AD No 2006-03-15 on 06/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Boeing Model 747SP, 747SR, 747-100, -100B, -100B SUD,
-200B, -200C, -200F and -300 Series airplanes -
modification of escape slide/raft pack assembly and cable
release sliders
Link to AD on FAA
website |
(31/03/2006) FAA issued
AD No 2006-06-03 on 16/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Certain Cessna Model 500, 501, 550, S550, 551, and 560
airplanes - Potential Fuel Vapour Ignition
|
(22/03/2006) FAA issued
AD No 2006-06-51 on 17/03/2006, to be considered accepted
by EASA under provisions of ED Decision 02/2003
Certain General Electric Company Aircraft Engines (GEAE)
CT7-8A turboshaft engines installed on Sikorsky S92
helicopters |
(16/03/2006) FAA issued
AD No 2006-05-02, to be considered accepted by EASA under
provisions of ED Decision 02/2003
Boeing Model 747-200F, 747-200C, 747- 400, 747-400D, and
747-400F Series Airplanes |
(16/03/2006) FAA issued
AD No 2006-04-04, to be considered accepted by EASA under
provisions of ED Decision 02/2003
Meggitt Model 602 Smoke Detectors Approved Under
Technical Standard Order (TSO) TSO-C1C and Installed on
Various Transport Category Airplanes, Including but Not
Limited to Aerospatiale Model ATR42 and ATR72 Airplanes;
Boeing Model 727 and 737 Airplanes; McDonnell Douglas
Model DC-10-10, DC-10-10F, DC-10-15, DC- 10-30 and
DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F,
MD-10- 10F, MD-10-30F, MD-11, and MD-11F Airplanes |
| (23/02/2006)CTA Brazil AD No.
2006-02-04 - EMBRAER - ERJ-170 - Integrated Drive
Generators |
(16/02/2006) FAA issued
AD No 2006-02-11, to be considered accepted by EASA under
provisions of ED Decision 02/2003
McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15,
DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40,
DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F
Airplanes |
| CTA Brazil issued AD
2006-02-02 - Amdt 1118 |
| (03/02/2006) FAA AD
2006-02-03 - Raytheon Model Hawker 800XP Airplanes -
Inspection of fuse on hydraulic over-temperature switch
on panel ZK |
| CTA Brazil issued AD
2006-01-03 - 'EMBRAER - Amendment 39-1114' is to be
considered accepted by EASA under provisions of ED
Decision 02/2003 |
(06/02/2006) FAA issued AD No 2006-02-51 on 02/02/2006, to be considered accepted by EASA under provisions of ED Decision 02/2003
Raytheon Aircraft Company Model 390 Airplanes – Hydraulic Tube Assembly & Clamp – Inspection/Replacement |
| CTA Brazil issued AD
No. 2005-11-01 to be considered accepted by EASA under
provisions of ED Decision 02/2003 |