Airworthiness Directives; Airbus Model A310 Series Airplanes
airworthiness · Rule · Final rule. · Published 1995-08-22 · Effective 1995-09-21 · 60 FR 43517
Document
Document number
95-19652
Federal Register citation
60 FR 43517
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A310 Series
Publication date
1995-08-22
Effective date
1995-09-21
FAA docket
Docket No. 93-NM-121-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A310 series airplanes, that requires inspections to detect loose self-locking nuts and damaged cotter pins on the actuating cylinder to drag strut attachment of the left- and right-hand main landing gear (MLG), and correction of discrepancies. This amendment also provides an optional terminating action for the repetitive inspections. This amendment is prompted by reports of loose nuts and sheared cotter pins found on in-service airplanes. The actions specified by this AD are intended to prevent an undampened free fall of the left- and right-hand MLG, which subsequently could lead to the inability to retract the MLG and damage to other airplane systems.