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Airworthiness Directives; Raytheon Aircraft Company (Formerly Beech Aircraft Corporation) Models 58P and 58PA Airplanes

airworthiness · Rule · Final rule. · Published 1997-05-07 · Effective 1997-06-30 · 62 FR 24809

Document

Document number
97-11895
Federal Register citation
62 FR 24809
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Raytheon
Publication date
1997-05-07
Effective date
1997-06-30
FAA docket
Docket No. 95-CE-89-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to Raytheon Aircraft Company (formerly Beech Aircraft Corporation) Models 58P and 58PA airplanes. This action requires inspecting for cracks in the right-hand (RH) upper and lower longeron near the second RH cabin window, inspecting for missing rivets in the cabin structure (longeron) adjacent to and aft of the second RH cabin window, repairing any cracked structure or reinforcing the longeron if it is not cracked, and installing rivets, if missing. Reports of cracks in the upper and lower longeron and missing rivets that are supposed to secure the frame, splice, and longeron together prompted this action. The actions specified by this AD are intended to prevent structural cracking to the cabin caused by missing rivets, which if not corrected, could cause decompression injuries to passengers, structural failure of the fuselage, and loss of the airplane.

Source

Authoritative
Federal Register document
Machine
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