Airworthiness Directives; Honeywell International Inc. TFE731-2 and -3 Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2005-03-14 · Effective 2005-04-18 · 70 FR 12404
Document
Document number
05-4686
Federal Register citation
70 FR 12404
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Honeywell International Inc. TFE731-2 and -3 Series Turbofan
Publication date
2005-03-14
Effective date
2005-04-18
FAA docket
Docket No. FAA-2004-18019
Abstract
The FAA is adopting a new airworthiness directive (AD) for Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 series turbofan engines with certain part number (P/N) low pressure turbine (LPT) stage 1 disks installed. This AD requires for TFE731-2 and -2C series engines, initial and repetitive measurements and calculations to determine acceptance, and adjustment or replacement if necessary, of the LPT stage 1 nozzle assembly. This AD also requires for TFE731-3, -3A, -3AR, -3B, -3BR, and -3R series engines, replacement of LPT stage 1 disks with serviceable disks. This AD also allows replacement of the LPT stage 1 disk with a disk having a part number not listed in the AD as optional terminating action to the repetitive actions. This AD results from a report of an uncontained failure of the LPT stage 1 disk installed in a TFE731-3-1H turbofan engine. We are issuing this AD to prevent additional uncontained failure of the LPT stage 1 disk, and possible damage to the airplane.