Document ID: chunk:federal_register_of_legislation:F2006B03042:body:0
Version: federal_register_of_legislation:F2006B03042
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Character Range: 0–1332

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 747 Series Aeroplanes

                        AD/B747/141 Pylon - Inboard and Outboard Strut Forward Lower Spar

5/95

            Applicability: B747 L/N 001 - 510 powered by JT9D-3 or -7 series engines, excluding JT9D-70 engines.

            Requirement: Perform a detailed visual inspection of the Inboard and Outboard Strut Forward Lower Spar Chords, Stiffeners and Web to detect cracks and loose fasteners. Inspect in accordance with Boeing Service Bulletin 747-54-2160.

            Note: FAA AD 94-17-17 refers.

            Compliance: Initially inspect before 2 February 1996 or before exceeding 6000 landings, whichever is the later.

            Aircraft that have accumulated between 6000 and 15000 landings shall be inspected before 2 October 1995.

            Aircraft which have accumulated more than 15000 landings shall be inspected before 2 July 1995.

            Reinspect at intervals not to exceed 2000 landings or 8000 hours time in service, whichever occurs first.

            Background: There have been five reports of cracks in the subject web. In addition it is suspected that a web crack may have contributed to a recent engine separation.