Summary
We are adopting a new airworthiness directive (AD) for certain Airbus Model A300 B4-601, B4-603, B4-605R, F4-605R, and C4-605R Variant F airplanes. This AD was prompted by reports of cracking found in the pylon box, which was due to the stresses resulting from the pressure applied by the thrust reverser cowl bumpers. This AD requires repetitive high frequency eddy current (HFEC) inspections for cracking; and replacement of all fittings if necessary, which terminates the repetitive HFEC inspections for the modified side only. We are issuing this AD to detect and correct cracks of the pylon rib 5, which could result in reduced structural integrity of the airplane.
Directive Details
AD Number
FAA-2014-0230
Document Number
2015-00997
Type
Rule
Publication Date
January 29, 2015
Effective Date
March 5, 2015
Affected Manufacturer
Airbus
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2014-0230
Topics
Official Documents
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