AD/MU-2/5 Amdt 3 - Wing Structural Fatigue Limitation
1AD/MU-2/5 Amdt 3 - Wing Structural Fatigue Limitation
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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-2/5
Amdt 3
Wing Structural Fatigue Limitation 4/79
Applicability: MU-2B-30 and MU-2B-36A aircraft.
Requirement: 1. Retire from service the outer wing front spar joint fitting.
Image unavailable in extracted text2. Retire the aircraft from service.
Compliance:
Note 1: The lives for the MU-2B-36A are conservative interim values and will be reviewed on receipt of further data from the manufacturer.
Note 2: Similar restrictions may be applied to other Models of the type should they enter the Australian Register.