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AD FAA-2013-0354

Airworthiness Directives; Eurocopter France Helicopters

Summary

We are superseding Airworthiness Directive (AD) 2010- 21-01 for Eurocopter France (Eurocopter) Model AS350B, BA, B1, B2, B3, D, AS355E, F, F1, F2, and N helicopters. AD 2010-21-01 required an inspection to determine whether a cross-member is installed at station X 2165 and doublers at X 2325 and Y 269, and installing them if they are missing. This new AD retains the requirements of AD 2010-21-01 but clarifies the inspection procedures and limits the applicability to only those helicopters with collective-to-yaw control coupling. This AD is prompted by a crack discovered in the area of the center cross-member at station X 2325, at the attachment point of the yaw channel ball-type control sheath stop, of a Model AS355N helicopter fitted with the collective-to-yaw control coupling. The actions of this AD are intended to prevent reduced yaw control and subsequent loss of helicopter control.

Directive Details

AD Number

FAA-2013-0354

Document Number

2013-27637

Type

Rule

Publication Date

November 25, 2013

Effective Date

December 30, 2013

Affected Manufacturer

Eurocopter France

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2013-0354

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Eurocopter France →

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