Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes
airworthiness · Rule · Final rule. · Published 2008-04-14 · Effective 2008-05-19 · 73 FR 19975
Document
Document number
E8-7182
Federal Register citation
73 FR 19975
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2008-04-14
Effective date
2008-05-19
FAA docket
Docket No. FAA-2008-0014
Abstract
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A318, A319, A320, and A321 airplanes. That AD currently requires repetitive inspections for cracking in the forward lug of the support rib 5 fitting of both main landing gear (MLG), and repair if necessary. The existing AD also provides optional terminating actions for certain airplanes, as well as other optional methods for complying with the inspection requirements of the existing AD. This new AD continues to require repetitive inspections for cracking in the forward lug of the support rib 5 fitting of the left and right MLG at new repetitive intervals in accordance with new service information, and repair or replacement of any cracked MLG fitting if necessary. This new AD also requires modification of the rib bushings of the left and right MLG, which would end the repetitive inspections. This AD results from cracks found in the forward lug of the MLG support rib 5 fitting. We are issuing this AD to prevent cracking in the forward lug of the MLG, which could result in failure of the lug and consequent collapse of the MLG during takeoff or landing.