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Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146-RJ Airplanes

airworthiness · Rule · Final rule. · Published 2005-11-22 · Effective 2005-12-27 · 70 FR 70483

Document

Document number
05-22970
Federal Register citation
70 FR 70483
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146-RJ
Publication date
2005-11-22
Effective date
2005-12-27
FAA docket
Docket No. FAA-2005-20729

Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to all BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146-RJ airplanes. That AD currently requires revising the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate life limits for certain items and inspections to detect fatigue cracking in certain structures. This new AD requires revising the ALS of the Instructions for Continued Airworthiness to incorporate new and more restrictive life limits for certain items and new and more restrictive inspections to detect fatigue cracking in certain structures. This new AD results from issuance of a later revision to the airworthiness limitations of the BAe/Avro 146 Aircraft Maintenance Manual, which specifies new inspections and compliance times for inspection and replacement actions. We are issuing this AD 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
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