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Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-12 Airplanes

airworthiness · Rule · Direct final rule; request for comments. · Published 1998-03-03 · Effective 1998-05-29 · 63 FR 10299

Document

Document number
98-5201
Federal Register citation
63 FR 10299
Type
Rule
Action
Direct final rule; request for comments.
Category
airworthiness
Manufacturer
Pilatus
Publication date
1998-03-03
Effective date
1998-05-29
FAA docket
Docket No. 97-CE-98-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Model PC-12 airplanes. This AD requires inspecting the elevator for incorrect rivet lengths and installing new rivets if incorrect rivet lengths are found. This AD also requires inspecting the elevator to assure that an excessive gap (more than .004 inches or .1 millimeters (mm)) does not exist in the rivet shanks, and installing a shim between the rib and skin to fill any excessive gap. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified in this AD are intended to prevent fatigue damage to the elevator, which could result in structural failure and eventual loss of control of the airplane.

Source

Authoritative
Federal Register document
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