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Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes

airworthiness · Rule · Final rule. · Published 2003-04-08 · Effective 2003-05-12 · 68 FR 16948

Document

Document number
03-8198
Federal Register citation
68 FR 16948
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pilatus
Publication date
2003-04-08
Effective date
2003-05-12
FAA docket
Docket No. 2003-CE-02-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC- 12/45 airplanes. This AD requires you to replace certain push switch caps on the electrical power management overhead panel with parts of improved design. 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 prevent the inability to operate the switch, which could result in failure to activate the related operational system. Such failure could adversely affect the operation and control of the airplane.

Source

Authoritative
Federal Register document
Machine
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