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Airworthiness Directives; Boeing Model 727 Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 1997-03-03 · Effective 1997-03-18 · 62 FR 9359

Document

Document number
97-4947
Federal Register citation
62 FR 9359
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Boeing Model 727 Series
Publication date
1997-03-03
Effective date
1997-03-18
FAA docket
Docket No. 97-NM-32-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to all Boeing Model 727 series airplanes. This action requires repetitive pre-modification inspections to detect cracks in the forward support fitting of the number 1 and number 3 engines; and repair, if necessary. This AD also provides for an optional high frequency eddy current (HFEC) inspection, and, if possible, modification of the fastener holes; and various follow-on actions. Accomplishment of these optional actions would constitute terminating action for the repetitive pre-modification inspections. This amendment is prompted by reports indicating that fatigue cracks were found in the forward support fitting of the number 1 and number 3 engines. The actions specified in this AD are intended to detect and correct such fatigue cracking, which could result in failure of the support fitting and consequent separation of the engine from the airplane.

Source

Authoritative
Federal Register document
Machine
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