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AD FAA-2009-0351

Airworthiness Directives; Sikorsky Aircraft Corporation Model S-92A Helicopters

Summary

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2009-07-53, which was sent previously to all known U.S. owners and operators of Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters by individual letters. This amendment is prompted by the failure of 2 main gearbox filter bowl assembly studs (studs) that were found broken during a fatal accident investigation in Canada. Prior to the accident, the manufacturer was investigating a July 2008 incident that also involved broken studs. In both cases, the broken studs resulted in rapid loss of oil. The failures have been tied to fretting and galling of the original titanium studs; therefore, this AD requires removing all titanium studs and replacing them with steel studs. The actions specified by this AD are intended to prevent failure of a stud, which could result in rapid loss of oil, failure of the main gearbox, and subsequent loss of control of the helicopter.

Directive Details

AD Number

FAA-2009-0351

Document Number

E9-9301

Type

Rule

Publication Date

April 27, 2009

Effective Date

April 27, 2009

Affected Manufacturer

Sikorsky Aircraft Corporation Model S-92A

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2009-0351

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Sikorsky Aircraft Corporation Model S-92A →

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