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.