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AD FAA-2012-0018

Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes

Summary

We are adopting a new airworthiness directive (AD) for Pilatus Aircraft Ltd. Models PC-6, PC-6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC- 6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2- H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as loose elevator and rudder hinge bolts caused by incorrect torquing and locking of the bolts, which could lead to in-flight failure of the elevator or rudder attachment. We are issuing this AD to require actions to address the unsafe condition on these products.

Directive Details

AD Number

FAA-2012-0018

Document Number

2012-6999

Type

Rule

Publication Date

March 30, 2012

Effective Date

May 4, 2012

Affected Manufacturer

Pilatus Aircraft Ltd.

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2012-0018

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Pilatus Aircraft Ltd. →

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