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Airworthiness Directives; Boeing Model 747 Series Airplanes

airworthiness · Rule · Final rule. · Published 1997-05-14 · Effective 1997-06-18 · 62 FR 26381

Document

Document number
97-12682
Federal Register citation
62 FR 26381
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747 Series
Publication date
1997-05-14
Effective date
1997-06-18
FAA docket
Docket No. 97-NM-12-AD

Abstract

This amendment revises an existing airworthiness directive (AD), applicable to certain Boeing Model 747 series airplanes, that currently requires repetitive inspections of the access doors to the midspar/spring beam fuse pins on all engine pylons to detect cracks on the external surface; repetitive inspections of each midspar/spring beam fuse pin to detect if it protrudes beyond its mating nut by a specified distance; and repair of any discrepancy found. The actions specified by that AD are intended to prevent migration of this fuse pin, which, if not detected and corrected in a timely manner, could result in failure of the engine pylon and consequent separation of the engine from the wing. This amendment increases the intervals between inspections of the access doors and each midspar/spring beam fuse pin, and consequently decreases the frequency of inspections. This amendment is prompted by new data provided by the manufacturer indicating that the reported migration of the fuse pin was apparently the result of an incorrectly installed nut.

Source

Authoritative
Federal Register document
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