AD/JETSTREAM/68 - Wings - Lower Surface at Landing Gear Bay
1AD/JETSTREAM/68 - Wings - Lower Surface at Landing Gear Bay
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.