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Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-6, PC- 6/A, PC-6/B, and PC-6/C Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-06-04 · Effective 1998-07-13 · 63 FR 30370

Document

Document number
98-14607
Federal Register citation
63 FR 30370
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pilatus
Publication date
1998-06-04
Effective date
1998-07-13
FAA docket
Docket No. 97-CE-09-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC-6, PC-6/A, PC-6/B, and PC-6/C series airplanes equipped with turbo-prop engines. This AD requires modifying the fuel system to improve the venting between the collector tank, the main wing tanks, and the engine. 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 engine fuel starvation during maximum climb and descent caused by poor fuel tank venting with low fuel levels, which could result in a loss of engine power during critical phases of flight.

Source

Authoritative
Federal Register document
Machine
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