Airworthiness Directives; Boeing Model 757 Series Airplanes Equipped With Rolls Royce Engines
airworthiness · Rule · Final rule. · Published 1995-05-16 · Effective 1995-06-15 · 60 FR 25983
Document
Document number
95-11906
Federal Register citation
60 FR 25983
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 757 Series
Publication date
1995-05-16
Effective date
1995-06-15
FAA docket
Docket No. 94-NM-188-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 757 series airplanes, that currently requires inspections to detect fatigue-related cracking or breakage of the hydraulic tubing support brackets located on the upper spar web in the engine struts; further inspection to detect related damage of the upper spar web, the fuel lines, and the hydraulic lines, as necessary; and repair or replacement of cracked or damaged parts. That AD was prompted by reports of fatigue-related cracks in the hydraulic tubing support brackets located on the upper spar web in the engine struts. The actions specified by that AD are intended to prevent such fatigue-related cracking, which could result in fuel or hydraulic fluid leakage into the interior of the engine strut and cause a fire. This amendment requires installation of a previously optional terminating action.