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Airworthiness Directives; Raytheon Aircraft Company Beech Models 1900, 1900C (C-12J), and 1900D Airplanes

airworthiness · Rule · Final rule. · Published 2001-11-07 · Effective 2001-12-17 · 66 FR 56199

Document

Document number
01-27651
Federal Register citation
66 FR 56199
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Raytheon
Publication date
2001-11-07
Effective date
2001-12-17
FAA docket
Docket No. 2001-CE-04-AD

Abstract

This amendment supersedes Airworthiness Directive (AD) 95-02- 18, which applies to certain Raytheon Aircraft Company (Raytheon) Beech Models 1900, 1900C (C-12J), and 1900D airplanes. AD 95-02-18 requires you to repetitively inspect the engine truss assemblies for cracks, repair or replace any cracked engine truss assembly, and install reinforcement doublers. This AD requires engine truss assembly replacement, periodic inspections and replacements, and the eventual incorporation of a cowling support installation kit as terminating action. The repetitive inspections of AD 95-02-18 will be retained until mandatory engine truss assembly replacement. This AD is the result of continued reports of fatigue cracks found on engine trusses on airplanes in compliance with AD 95-02-18. The actions specified by this AD are intended to detect and correct cracked engine truss assemblies, which could result in failure of the engine truss assembly and consequent loss of airplane control.

Source

Authoritative
Federal Register document
Machine
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