AD/PL 12/4 - Stub Wing Structure - Inspection
1AD/PL 12/4 - Stub Wing Structure - Inspection
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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 Transavia PL 12 Series Aeroplanes
AD/PL 12/4 Stub Wing Structure - Inspection 12/68
Applicability: All models.
Requirement: Inspect the stub wing leading edge tube for cracking in the vicinity of landing gear attachment.
Compliance: Within 100 hours time in service after 14 February 1969 and thereafter at intervals not exceeding 100 hours time in service.