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Airworthiness Directives; Raytheon Aircraft Company Beech Models 36, A36, A36TC, B36TC, 58, and 58A Airplanes

airworthiness · Rule · Final rule. · Published 2003-01-08 · Effective 2003-02-27 · 68 FR 997

Document

Document number
03-148
Federal Register citation
68 FR 997
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Raytheon
Publication date
2003-01-08
Effective date
2003-02-27
FAA docket
Docket No. 2002-CE-07-AD

Abstract

This amendment supersedes Airworthiness Directive (AD) 2000- 26-16, which applies to certain Raytheon Aircraft Company (Raytheon) Beech Models A36, B36TC, and 58 airplanes. AD 2000-26-16 requires you to inspect for missing rivets on the right hand side of the fuselage and, if necessary, install rivets. AD 2000-26-16 resulted from Raytheon identifying several instances of missing rivets on these airplanes. AD 2000-26-16 incorporated an incorrect listing of serial numbers for the affected model airplanes and omitted certain airplane models from the applicability section of AD 2000-26-16. This AD retains the actions required in AD 2000-26-16 and corrects the applicability section. The actions specified by this AD are intended to detect and correct missing rivets in the right hand fuselage panel assembly in the area above the right wing and below the cabin door threshold. These rivets must be present for the fuselage to carry the ultimate load and prevent critical structural failure with loss of airplane control.

Source

Authoritative
Federal Register document
Machine
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