Document ID: chunk:federal_register_of_legislation:F2006B10553:body:0
Version: federal_register_of_legislation:F2006B10553
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 British Aerospace (Hawker Siddeley) HS 748 Series Aeroplanes

AD/HS 748/19 Supplementary Structural Inspection Document 6/95

 Applicability: All HS748 aircraft.

            Requirement: Incorporate into the Maintenance Schedule the requirements of the HS748 Supplementary Structural Inspection Document Revision 2 with the following exceptions and additions:

(i)            A high frequency eddy current inspection approved by the Authority shall be used in lieu of the visual method specified in item 57-40-1.

(ii)         When complying with the SSID operators shall ensure the full requirements of the following Service Bulletins (SB) are met:

                 SB 57/75, SB 57/55, SB 57/34, SB 55/19, SB 53/49.

(iii)       The inspection intervals and associated inspection procedures of SB 52-101 shall be observed when complying with item 52-30-1.

            Note: CAA(UK) AD 010-09-85 and British Aerospace Alert Service Bulletin 12/11 Revision 1 refer.

 Compliance: Effective 25 May 1995.

            Background: The Supplementary Structural Inspection Document has been produced as part of a programme to ensure the continuing airworthiness of high time HS748 aircraft.