Research projects - General aviation

Reference	Title	Status	Date
EASA.2007/2	Investigation of the technical feasibility and safety benefit of a light aeroplane operational Flight Data Monitoring (FDM) system	Final	December 2008
EASA/2008/3	Safety Aspects of Light Aircraft Spin Resistance Concept	Final	December 2009

Detailed description

Investigation of the technical feasibility and safety benefit of a light aeroplane operational Flight Data Monitoring (FDM) system
Reference:	EASA.2007/2
Description:	The object is to carry out a feasibility study, an initial prototype design and a flight trial of an integrated FDM system for single engine light aeroplanes that in addition provides a flight data storage and retrieval capability. It will assist accident investigation and also permit the pilot / maintenance personnel to access flight information and be notified of operational exceedances.
Status:	Final
Date:	December 2008
View File:	Final report EASA.2007/2

Safety Aspects of Light Aircraft Spin Resistance Concept
Reference:	EASA/2008/3
Description:	The primary objective of the project is to investigate safety criteria and relevant test methods which will form the fundamental basis for proposing a change to CS-23 Certification Specification. To demonstrate that the proposed criteria are satisfactory flight trials with an existing spin resistant aircraft or modified aircraft will be carried out.
Status:	Final
Date:	December 2009
View File:	Final report EASA.2008/3