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Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

airworthiness · Rule · Final rule. · Published 2001-01-03 · Effective 2001-02-07 · 66 FR 264

Document

Document number
01-30
Federal Register citation
66 FR 264
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
British Aerospace (Jetstream) Model 4101
Publication date
2001-01-03
Effective date
2001-02-07
FAA docket
Docket No. 99-NM-250-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all British Aerospace (Jetstream) Model 4101 airplanes, that requires revising the Airworthiness Limitations Section of the Instructions for Continued Airworthiness to incorporate life limits for certain items and inspections to detect fatigue cracking in certain structures. This amendment is prompted by issuance of a revision to the airworthiness limitations of the British Aerospace J41 Aircraft Maintenance Manual. The actions specified by this AD are intended to ensure that fatigue cracking of certain structural elements is detected and corrected; such fatigue cracking could adversely affect the structural integrity of these airplanes.

Source

Authoritative
Federal Register document
Machine
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