Document ID: chunk:federal_register_of_legislation:F2011L01846:body:0:p2
Version: federal_register_of_legislation:F2011L01846
Segment Type: other
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Character Range: 2807–3528

the fuel pump, which could lead to localized overheating of parts inside the fuel pump, and which could produce an ignition source inside the fuel tank.

   This amendment deletes the original text of the AD and incorporates the original FAA AD by reference.  This was done to facilitate easier cross referencing to FAA AD 2011-18-03 Amdt 39-16785 which details the terminating actions for the requirements of this AD.

   The original issue of this AD became effective on 20 November 2008.

   Alternative methods of compliance for AD 2008-24-51 that are approved by the FAA are acceptable as a means of compliance against this AD.

Mike Higgins
Delegate of the Civil Aviation Safety Authority

5 September 2011