← FAA Federal Register actions

Airworthiness Directives; Pratt & Whitney JT8D Series Turbofan Engines

airworthiness · Rule · Final rule. · Published 1997-09-19 · Effective 1997-11-18 · 62 FR 49133

Document

Document number
97-24796
Federal Register citation
62 FR 49133
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pratt & Whitney JT8D Series Turbofan
Publication date
1997-09-19
Effective date
1997-11-18
FAA docket
Docket No. 96-ANE-32

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to Pratt & Whitney JT8D-1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -17, and -17R series turbofan engines, that requires initial and repetitive fluorescent penetrant and eddy current inspections of 4th stage low pressure turbine (LPT) hubs for cracks, and, if necessary, replacement with serviceable parts. This amendment is prompted by a report of an uncontained 4th stage LPT blade release. The actions specified by this AD are intended to prevent a 4th stage LPT blade release due to hub cracking, which can result in an uncontained engine failure and damage to the aircraft.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown