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Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Series Airplanes

airworthiness · Rule · Final rule. · Published 1999-03-05 · Effective 1999-04-09 · 64 FR 10555

Document

Document number
99-5041
Federal Register citation
64 FR 10555
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
British Aerospace Model BAC 1-11 200 and 400 Series
Publication date
1999-03-05
Effective date
1999-04-09
FAA docket
Docket No. 98-NM-27-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to all British Aerospace Model BAC 1-11 200 and 400 series airplanes, that currently requires repetitive visual inspections to detect cracks in the flight deck canopy area, and repair, if necessary; and repetitive detailed visual and eddy current inspections to detect cracks of the top sill members at station 82.5, and replacement of cracked parts with new parts, or repair of the top sill members. This amendment continues to require detailed visual and eddy current inspections to detect cracks of the top sill members at station 82.5. This amendment also adds a requirement for a one-time inspection to determine the type of fasteners installed in certain holes of the joint strap installation, and replacement of rivets with bolts, if necessary. This amendment is prompted by the issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to detect and correct cracking in the flight deck canopy area, which could result in reduced structural integrity of the flight deck frame and adjacent fuselage structure.

Source

Authoritative
Federal Register document
Machine
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