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AD FAA-2009-1090

Airworthiness Directives; Eurocopter France Model AS355E, AS355F, AS355F1, AS355F2, and AS355N Helicopters

Summary

We are adopting a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters. This AD results from a mandatory continuing airworthiness information (MCAI) AD issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI AD states that a metallurgical non-conformity was discovered on a flange of the forward shaft section of the tail rotor drive shaft (drive shaft). The MCAI AD also states that stress analysis has shown that this non-conformity can significantly reduce the strength of the drive shaft and thereby its service life. The AD actions are intended to remove non-conforming drive shafts from service and prevent failure of the drive shaft and subsequent loss of control of the helicopter.

Directive Details

AD Number

FAA-2009-1090

Document Number

2010-5328

Type

Rule

Publication Date

March 16, 2010

Effective Date

April 20, 2010

Affected Manufacturer

Eurocopter France Model AS355E, AS355F, AS355F1, AS355F2, and AS355N

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2009-1090

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for Eurocopter France Model AS355E, AS355F, AS355F1, AS355F2, and AS355N →

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