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importantRule

AD FAA-2015-3781

Airworthiness Directives; Agusta S.p.A. Helicopters

Summary

We are adopting a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109A, A109A II, A109C, A109E, A109K2, A109S, and AW109SP helicopters. This AD requires visually inspecting the tail rotor drive shaft assembly (drive shaft) for a crack. This AD was prompted by the discovery of three cracks on the drive shaft of a Model A109S helicopter. The actions of this AD are intended to detect a crack on the drive shaft to prevent failure of the driveshaft, failure of the tail rotor, and subsequent loss of helicopter control.

Directive Details

AD Number

FAA-2015-3781

Document Number

2016-21707

Type

Rule

Publication Date

September 15, 2016

Effective Date

October 20, 2016

Affected Manufacturer

Agusta S.p.A.

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2015-3781

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Agusta S.p.A. →

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