AD/PL 12/4 - Stub Wing Structure - Inspection

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

Transavia PL 12 Series Aeroplanes

AD/PL 12/4 Stub Wing Structure - Inspection 12/68

All models.

Inspect the stub wing leading edge tube for cracking in the vicinity of landing gear attachment.

Within 100 hours time in service after 14 February 1969 and thereafter at intervals not exceeding 100 hours time in service.