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Airworthiness Directives; Pratt & Whitney JT8D Series Turbofan Engines

airworthiness · Rule · Final rule. · Published 2000-10-30 · Effective 2000-12-04 · 65 FR 64597

Document

Document number
00-27507
Federal Register citation
65 FR 64597
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pratt & Whitney JT8D Series Turbofan
Publication date
2000-10-30
Effective date
2000-12-04
FAA docket
Docket No. 99-NE-29-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to Pratt & Whitney (PW) JT8D series turbofan engines, that requires inspections of main fuel pump control shafts for excessive spline wear. Additionally, as terminating action to the inspections, this action requires the replacement of the main fuel pump control shaft with parts of improved design, and reworking the main fuel pump impeller, impeller gear train plate assembly, and impeller cover assembly. This amendment is prompted by reports of failed main fuel pump control shafts caused by excessive spline wear. The actions specified by this AD are intended to prevent loss of engine throttle control, uncommanded acceleration, uncommanded deceleration or inflight shutdown, which could result in reduced airplane control during a critical phase of flight.

Source

Authoritative
Federal Register document
Machine
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