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AD/JETSTREAM/66 - Wing - Main Spar Fuel Fitting Attachment Holes
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AD/JETSTREAM/66 - Wing - Main Spar Fuel Fitting Attachment Holes
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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
Applicability: Jetstream 3200 Series aircraft up to and including constructor’s number 950.
Requirement: Modify the fuel tank drainage hole at wing station 64.8 on the left and right hand sides in accordance with British Aerospace SB 57-JM 8175 revision 1.
Compliance: Prior to 6000 landings or before 15 March 1995 whichever is the later.
Background: Cracking of the wing main spar webs has been found at this location on the Jetstream 3200 series wing test specimen.