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Airworthiness Directives; PILATUS Aircraft Ltd. Model PC-7 Airplanes

airworthiness · Rule · Final rule. · Published 2002-11-01 · Effective 2002-12-20 · 67 FR 66541

Document

Document number
02-27418
Federal Register citation
67 FR 66541
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
PILATUS
Publication date
2002-11-01
Effective date
2002-12-20
FAA docket
Docket No. 2002-CE-28-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain PILATUS Aircraft Ltd. (Pilatus) Model PC-7 airplanes. This AD requires you to repetitively inspect the main landing gear front attachment brackets for cracks, and, if cracks are found, install improved-design brackets. Installing the improved-design brackets terminates the required inspections. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to detect and correct cracks in the main landing gear front attachment brackets, which could result in failure of the brackets. Such failure could lead to the main landing gear leg detaching from the wing main spar.

Source

Authoritative
Federal Register document
Machine
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