Document ID: chunk:federal_register_of_legislation:F2006B11380:body:0
Version: federal_register_of_legislation:F2006B11380
Segment Type: other
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Character Range: 0–727

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 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.

            2. 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.