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Airworthiness Directives; Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan Engines

airworthiness · Rule · Final rule. · Published 2007-11-28 · Effective 2008-01-02 · 72 FR 67242

Document

Document number
E7-22810
Federal Register citation
72 FR 67242
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan
Publication date
2007-11-28
Effective date
2008-01-02
FAA docket
Docket No. FAA-2007-26966

Abstract

The FAA is superseding an existing airworthiness directive (AD) for Rolls-Royce Corporation (RRC) AE 3007A and AE 3007C series turbofan engines. That AD currently prohibits any flight following a ground engine start where the engine oil temperature is below 32 [deg]F (0 [deg]C), unless certain preflight operational procedures are followed. This AD also requires those actions and would also require a terminating action. This AD results from design improvements to components in the accessory gearbox air turbine starter mounting pad. We are issuing this AD to prevent an in-flight engine shutdown due to loss of engine oil from the engine accessory gearbox starter pad shaft seal drain and possible loss of the airplane.

Source

Authoritative
Federal Register document
Machine
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