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AD/B727/51 - Right Hand Inboard Midflap Trailing Edge Upper Chord Support Angle - Reinforcement
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AD/B727/51 - Right Hand Inboard Midflap Trailing Edge Upper Chord Support Angle - Reinforcement
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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 Boeing 727 Series Aeroplanes
AD/B727/51 Right Hand Inboard Midflap Trailing Edge Upper
Chord Support Angle - Reinforcement
6/67
Applicability: All models. Document: Boeing SB No. 27-97. Compliance: Forthwith.