airworthiness · Rule · Final rule. · Published 2015-03-02 · Effective 2015-04-06 · 80 FR 11096
Document
Document number
2015-02692
Federal Register citation
80 FR 11096
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2015-03-02
Effective date
2015-04-06
FAA docket
Docket No. FAA-2014-0139
Abstract
We are superseding Airworthiness Directive (AD) 2009-20-05 for certain Airbus Model A318, A319, A320, and A321 series airplanes. AD 2009-20-05 required one-time inspections for cracking, damage, correct installation, and correct adjustment of the main landing gear (MLG) door hinge and actuator fittings on the keel beam, and corrective actions if necessary. This new AD expands the applicability, reduces the compliance time, and requires repetitive inspections instead of the one-time inspection. This AD also requires revising the maintenance or inspection program. This AD was prompted by reports of cracks on fittings that had successfully passed certain required inspections. We are issuing this AD to detect and correct cracking on the MLG door hinge fitting and actuator fitting on the keel beam, which could lead to in-flight detachment of an MLG door, possibly resulting in injury to persons on the ground and/or damage to the airplane.