airworthiness · Rule · Final rule; request for comments. · Published 2014-06-17 · Effective 2014-07-02 · 79 FR 34403
Document
Document number
2014-13832
Federal Register citation
79 FR 34403
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Airbus
Publication date
2014-06-17
Effective date
2014-07-02
FAA docket
Docket No. FAA-2014-0340
Abstract
We are adopting a new airworthiness directive (AD) for certain Airbus Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300- 600 series airplanes); and Airbus Model A310 series airplanes. This AD requires inspections of the external area of the aft cargo door sill beam for cracking, and repair if necessary. This AD was prompted by reports of fatigue cracks on the cargo door sill beam, lock fitting, and torsion box plate. We are issuing this AD to detect and correct fatigue cracking of the cargo door sill beam, lock fitting, and torsion box plate, which could result in the loss of the door locking function and, subsequently, complete loss of the cargo door in flight with the risk of rapid decompression.