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Airworthiness Directives; Pratt & Whitney JT9D-3A, -7, -7A, -7F, -7H, -7AH, and -7J Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 2003-12-31 · Effective 2003-12-18 · 68 FR 75400

Document

Document number
03-32155
Federal Register citation
68 FR 75400
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2003-12-31
Effective date
2003-12-18
FAA docket
Docket No. 2003-NE-52-AD Amendment 39-13410

Abstract

The FAA is revising an existing airworthiness directive (AD) for Pratt & Whitney (PW) JT9D-3A, -7, -7A, -7F, -7H, -7AH, and -7J turbofan engines, with gearbox pressure tube, part number (P/N) 697896, and No. 4 bearing front pressure manifold, P/N 670663, installed. That AD currently requires a one-time visual inspection of the gearbox pressure tube and No. 4 bearing front pressure manifold and the attaching clamp assemblies for correct positioning and for wear and damage, and replacement if necessary. This ad requires the same actions. This AD results from the need to correct errors in depicted clamping to ensure that AD compliance can be achieved, and to relax the level of maintenance required, as an optional method, when inspecting the affected tubing for dents. We are issuing this AD to prevent engine fires caused by failed gearbox pressure tubes or failed No. 4 bearing front pressure manifolds.

Source

Authoritative
Federal Register document
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