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Airworthiness Directives; British Aerospace Model HS 748 Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2005-11-21 · Effective 2005-12-06 · 70 FR 70038

Document

Document number
05-22790
Federal Register citation
70 FR 70038
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
British Aerospace Model HS 748
Publication date
2005-11-21
Effective date
2005-12-06
FAA docket
Docket No. FAA-2005-23006

Abstract

The FAA is adopting a new airworthiness directive (AD) for all British Aerospace Model HS 748 airplanes. This AD requires repetitive inspections for fatigue cracking, corrosion, and other related discrepancies of the rear pressure bulkhead and associated areas, and the fin attachment fittings, particularly the fin link beam; and related investigative and corrective actions. This AD results from a structural integrity audit of the airplane that showed the importance of inspecting for fatigue cracking and corrosion of these areas. We are issuing this AD to detect and correct cracking, corrosion, and other related discrepancies of the rear pressure bulkhead and associated areas, and the fin attachment fittings, particularly the fin link beam, which could result in damage to the airplane structure or injury to airplane occupants.

Source

Authoritative
Federal Register document
Machine
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