Document ID: chunk:federal_register_of_legislation:F2006B10938:body:0
Version: federal_register_of_legislation:F2006B10938
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 British Aerospace BAe 3100 (Jetstream) Series Aeroplanes

                              AD/JETSTREAM/68 Wings - Lower Surface at Landing Gear Bay

10/94

 Applicability: All Jetstream 3200 Aircraft.

            Requirement: Inspect, using high frequency eddy current, the wing lower surface skin at the outboard end of the main landing gear bay for fatigue cracking in accordance with British Aerospace SB 57-JA 930640 Revision 1 Appendix A.

            Compliance: Initial inspection before 10000 landings or within 600 landings from 15 September 1994 whichever occurs last. Repeat inspections at 10000 landing intervals.

            Note: CAA (UK) AD 004-09-03 refers.

 Background: Fatigue testing has shown a need to inspect the wing lower surface for cracking.