CTHRepealedLegislation
AD/MU-2/9 - Trim Aileron Bellcrank Bracket Bolt Holes - Inspection
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AD/MU-2/9 - Trim Aileron Bellcrank Bracket Bolt Holes - 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 Mitsubishi MU-2 Series Aeroplanes
AD/MU-2/9 Trim Aileron Bellcrank Bracket Bolt Holes - Inspection
Applicability: As detailed in the requirement document. Document: Mitsubishi SB No. 164.
Compliance: Within 50 hours time in service after 28 June 1974.
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