Airworthiness Directives; Honeywell International Inc. ALF502L Series and ALF502R Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2006-05-09 · Effective 2006-06-13 · 71 FR 26823
Document
Document number
06-4193
Federal Register citation
71 FR 26823
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Honeywell International Inc. ALF502L Series and ALF502R Series Turbofan
Publication date
2006-05-09
Effective date
2006-06-13
FAA docket
Docket No. 92-ANE-34-AD
Abstract
The FAA is superseding an existing airworthiness directive (AD) for Honeywell International Inc. ALF502L series and ALF502R series turbofan engines. That AD currently establishes stress rupture retirement life limits for certain third stage turbine discs used in conjunction with certain third stage turbine nozzles. This AD brings requirements forward and unchanged, from the previous AD for ALF502R series turbofan engines. Also, this AD establishes new reduced stress rupture retirement life limits for certain part numbers (P/Ns) of third stage turbine disc and shaft assemblies installed in ALF502L series turbofan engines. This AD also requires removing those same parts from service using a drawdown schedule. This AD results from a report of failure of a third stage turbine disc and shaft assembly, leading to turbine blade release and separation of the exhaust nozzle. We are issuing this AD to prevent total loss of engine power, in-flight engine shutdown, release of turbine blades, separation of the exhaust nozzle, and possible damage to the airplane.