Airworthiness Directives; Airbus Model A300 Series Airplanes
airworthiness · Rule · Final rule; request for comments.NUREG · Published 1998-10-16 · Effective 1998-11-02 · 63 FR 55522
Document
Document number
98-27480
Federal Register citation
63 FR 55522
Type
Rule
Action
Final rule; request for comments.NUREG
Category
airworthiness
Manufacturer
Airbus Model A300 Series
Publication date
1998-10-16
Effective date
1998-11-02
FAA docket
Docket No. 98-NM-288-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Airbus Model A300 series airplanes. This action requires incorporating into the FAA-approved maintenance program certain torque values for installing certain nuts and bolts of the engine attachment fittings; and follow-on actions, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to prevent cracking of the nuts and bolts of the engine attachment fittings due to overtorquing; such cracking could propagate and result in separation of the engine from the airplane.