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AD/L200/6 - Wing and Tailplane Structural Fatigue Life
1AD/L200/6 - Wing and Tailplane Structural Fatigue Life
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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 Morava L200 Series Aeroplanes
AD/L200/6 Wing and Tailplane Structural Fatigue Life 10/78
Applicability: All models.
Document: Omnipol IB No. L200/114. Compliance: Forthwith.