Airworthiness Directive · Amendment 39-10928 · Airbus Model A321-111, -112, and -131 Series Airplanes
Airbus Model A321-111, -112, and -131 Series Airplanes
Superseded. A later AD replaced this one: AD 2004-07-15. Comply with the one in force.
Model A321-111, -112, and -131 series airplanes; except those on which Airbus Modification 24977 has been accomplished during production, or on which the action described in Airbus Service Bulletin A320-57-1100, dated July 28, 1997 (Airbus Modification 26010) has been accomplished; certificated in any category.
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A321-111, -112, and -131 series airplanes. This action requires repetitive inspections to detect fatigue cracking in the area surrounding certain attachment holes of the forward pintle fittings of the main landing gear (MLG) and the actuating cylinder anchorage fittings on the inner rear spar; and repair, if necessary. This amendment also provides for optional terminating action for the repetitive inspections. 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 detect and correct fatigue cracking on the inner rear spar of the wings, which could result in reduced structural integrity of the airplane.
