Airworthiness Directives; Boeing Model 767 Series Airplanes Powered by General Electric or Pratt & Whitney Engines
airworthiness · Rule · Final rule. · Published 2004-05-05 · Effective 2004-06-09 · 69 FR 24947
Document
Document number
04-9761
Federal Register citation
69 FR 24947
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 767 Series
Publication date
2004-05-05
Effective date
2004-06-09
FAA docket
Docket No. 2002-NM-275-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 767 series airplanes powered by General Electric or Pratt & Whitney engines, that currently requires repetitive inspections to detect discrepancies of the four aft-most fastener holes in the horizontal tangs of the midspar fitting of the strut, and corrective actions, if necessary. That AD also provides an optional terminating action for repetitive inspections. This amendment expands the area on which the inspections are required. The actions specified by this AD are intended to prevent fatigue cracking in the primary strut structure and reduced structural integrity of the strut, which could result in separation of the strut and engine. This action is intended to address the identified unsafe condition.