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Airworthiness Directives; McDonnell Douglas Helicopter Systems Model MD-900 Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 1999-01-19 · Effective 1999-02-03 · 64 FR 2810

Document

Document number
99-683
Federal Register citation
64 FR 2810
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
McDonnell Douglas Helicopter Systems Model MD-900
Publication date
1999-01-19
Effective date
1999-02-03
FAA docket
Docket No. 98-SW-24-AD

Abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 98-12-30 which was sent previously to all known U.S. owners and operators of McDonnell Douglas Helicopter Systems (MDHS) Model MD-900 helicopters by individual letters. This AD requires inspecting the main rotor upper hub assembly (hub assembly) for cracks, and if a crack is found, replacing the hub assembly. The AD also requires verifying attachment nut torque values and a repetitive inspection at intervals not to exceed 150 hours time- in-service. This amendment is prompted by the discovery of cracks in 6 main rotor upper hub assemblies. This condition, if not corrected, could result in failure of the hub assembly, loss of drive to the main rotor, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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