airworthiness · Rule · Final rule; request for comments. · Published 2009-06-11 · Effective 2009-06-26 · 74 FR 27684
Document
Document number
E9-11992
Federal Register citation
74 FR 27684
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2009-06-11
Effective date
2009-06-26
FAA docket
Docket No. FAA-2009-0082
Abstract
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Corporation (RRC) AE 2100D2, AE 2100D2A, AE 2100D3, and AE 2100J turboprop engines with certain propeller gearbox (PGB) shaft-and- carrier assemblies installed. These engines are U.S. type-certificated but as of the effective date of this AD are only installed on military airplanes. This AD requires monitoring a certain population of PGB shaft-and-carrier assemblies for vibration during flight, and borescope-inspecting the PGB shaft for cracks if vibration is experienced. This AD would also require removing the affected population of PGB shaft-and-carrier assemblies from service and installing serviceable PGB shaft-and-carrier assemblies. This AD results from a report of a crack found in the forward cone of a PGB shaft in an RRC AE 2100D3 turboprop engine that was removed from service due to high vibration. We are issuing this AD to prevent separation of the propeller from the airplane, which could result in injury, and damage to the airplane.