Commonwealth legislation

AD/MU-2/67 - Fuselage Frame

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legislative instrument

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This Airworthiness Directive requires operators of Mitsubishi MU-2B-30, -35 and -36 aeroplanes (serial numbers 501–696, except 652 and 661) to inspect fuselage frames at STA 4610, 4850 and 5605 in accordance with Mitsubishi Heavy Industries Service Bulletin 209B. It responds to field reports of cracking around splice screw holes. Owners/operators must carry out the first inspection within 200 hours time in service after 12 August 1999 and then at intervals not exceeding 2,000 hours; they bear the inspection cost and arrange maintenance to comply.

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AD/MU-2/67 - Fuselage Frame

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Mitsubishi MU-2 Series Aeroplanes

AD/MU-2/67 Fuselage Frame 8/99

Applicability: Model MU-2B-30, -35, and -36 aircraft, with serial numbers 501 through 696; except 652 and 661.

Requirement: Inspect the fuselage frame in accordance with Mitsubishi Heavy Industries Service Bulletin 209B.

Note: JCAB AD TCD-5030-99 refers.

Compliance: Within 200 hours time in service after 12 August 1999; thereafter at intervals not to exceed 2,000 hours time in service.

This Airworthiness Directive becomes effective on 12 August 1999.

Background: The manufacturer received field reports of cracking around the splice screw holes of the fuselage frame at STA 4610. This Directive requires an inspection of the fuselage frames at STA 4610, 4850, and 5605.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.