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Airworthiness Directives; Fokker Model F.28 Mark 0100 Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-11-02 · Effective 1998-12-07 · 63 FR 58625

Document

Document number
98-29002
Federal Register citation
63 FR 58625
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fokker Model F.28 Mark 0100 Series
Publication date
1998-11-02
Effective date
1998-12-07
FAA docket
Docket No. 98-NM-101-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Fokker Model F.28 Mark 0100 series airplanes, that requires a one-time visual inspection and a one-time eddy current and/or dye penetrant inspection of the nose landing gear (NLG) main fitting to detect cracking; and rework of the NLG main fitting, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent cracking of the NLG main fitting, which could lead to collapse of the NLG during takeoff and landing and possible injury to the flightcrew and passengers.

Source

Authoritative
Federal Register document
Machine
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