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

airworthiness · Rule · Direct final rule; confirmation of effective date. · Published 1998-04-22 · Effective 1998-05-29 · 63 FR 19798

Document

Document number
98-10596
Federal Register citation
63 FR 19798
Type
Rule
Action
Direct final rule; confirmation of effective date.
Category
airworthiness
Manufacturer
Pilatus
Publication date
1998-04-22
Effective date
1998-05-29
FAA docket
Docket No. 97-CE-98-AD

Abstract

This action confirms the effective date of Airworthiness Directive (AD) 98-05-06, which applies to Pilatus Aircraft Ltd. (Pilatus) Model PC-12 airplanes. AD 98-05-06 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
Machine
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