Summary
We are adopting a new airworthiness directive (AD) for the specified Eurocopter France (ECF) helicopters. This AD results from a mandatory continuing airworthiness information (MCAI) AD issued by the aviation authority of the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The superseding MCAI AD states that several engine flameouts have involved failure of the 41-tooth pinion in the engine accessory gearbox. Each affected helicopter had a starter-generator manufactured by one company. Investigation revealed the torque damping system of the starter-generator was inoperative due to incorrect adjustment that caused bending stresses on the 41-tooth pinion. Failure of the pinion causes the engine fuel pump to stop operating, resulting in an engine flameout. The EASA AD requires a new adjustment procedure to optimize the performance of the specified starter-generator damping assembly. This AD is intended to prevent failure of a pinion and a fuel pump, engine flameout, and subsequent loss of control of the helicopter.
Directive Details
AD Number
FAA-2010-1228
Document Number
2011-11795
Type
Rule
Publication Date
May 18, 2011
Effective Date
June 22, 2011
Affected Manufacturer
Eurocopter France Model AS350B, B1, B2, B3, BA, and EC130 B4
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2010-1228
Topics
Official Documents
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