Airworthiness Directives; Boeing Model 757 Series Airplanes Powered by Pratt & Whitney Engines
airworthiness · Rule · Final rule. · Published 2000-10-06 · Effective 2000-11-13 · 65 FR 59703
Document
Document number
00-25433
Federal Register citation
65 FR 59703
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 757 Series
Publication date
2000-10-06
Effective date
2000-11-13
FAA docket
Docket No. 99-NM-308-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 757 series airplanes, that requires modification of the nacelle strut and wing structure. This amendment is prompted by reports indicating that the actual operational loads applied to the nacelle are higher than the analytical loads that were used during the initial design. Such an increase in loading can lead to fatigue cracking in primary strut structure prior to an airplane reaching its design service objective. The actions specified by this AD are intended to prevent fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut.