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AD FAA-2011-1113

Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters

Summary

We are adopting a new airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This AD was prompted by the discovery of tail rotor blade assemblies (blades) manufactured with mislocated aluminum wire mesh, leaving portions of the graphite torque tube (spar) region unprotected from a lightning strike. The actions are intended to detect mislocated blade wire mesh and to prevent spar delamination, loss of the blade tip cap during a lightning strike, blade imbalance, loss of a blade, and subsequent loss of control of the helicopter.

Directive Details

AD Number

FAA-2011-1113

Document Number

2012-8052

Type

Rule

Publication Date

April 10, 2012

Effective Date

May 15, 2012

Affected Manufacturer

Sikorsky Aircraft Corporation

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2011-1113

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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