Airworthiness Directives; Boeing Model 767 Series Airplanes Powered by General Electric Engines
airworthiness · Rule · Final rule. · Published 2001-04-02 · Effective 2001-05-07 · 66 FR 17492
Document
Document number
01-7701
Federal Register citation
66 FR 17492
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 767 Series
Publication date
2001-04-02
Effective date
2001-05-07
FAA docket
Docket No. 99-NM-127-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 767 series airplanes powered by General Electric engines, 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 the 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 the primary strut structure and consequent reduced structural integrity of the strut.