AD/MU-2/10 Amdt 1 - Flap Control System Flexible Shafts - Inspection
1AD/MU-2/10 Amdt 1 - Flap Control System Flexible Shafts - 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-2/10
Amdt 1
Flap Control System Flexible Shafts - Inspection 12/84
Applicability: All models MU-2B aircraft referred to in the requirement document. Document: Mitsubishi MU-2 S.B. No. 162 Rev. A.
Compliance: At intervals not exceeding 100 hours time in service after 28 February 1975.
Background: This directive is amended to clarify the aircraft applicability and amend the revision status of the requirement document.