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Airworthiness Directives; Pratt & Whitney JT8D-200 Series Turbofan Engines

airworthiness · Rule · Final rule. · Published 2005-10-17 · Effective 2005-11-21 · 70 FR 60211

Document

Document number
05-20501
Federal Register citation
70 FR 60211
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pratt & Whitney JT8D-200 Series Turbofan
Publication date
2005-10-17
Effective date
2005-11-21
FAA docket
Docket No. 96-ANE-35-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD) that applies to Pratt & Whitney (PW) JT8D-200 series turbofan engines. That AD currently requires installing and periodically inspecting individual or sets of certain part number (P/N) temperature indicators on the No. 4 and 5 bearing compartment scavenge oil tube and performance of any necessary corrective action. This AD requires installing and periodically inspecting two temperature indicators on all PW JT8D-200 series turbofan engines, including those incorporating high pressure turbine (HPT) containment hardware. This AD results from five uncontained HPT shaft failures. We are issuing this AD to prevent oil fires and the resulting fracture of the HPT shaft which can result in uncontained release of engine fragments; engine fire; in-flight engine shutdown; and possible airplane damage.

Source

Authoritative
Federal Register document
Machine
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