Commonwealth legislation

AD/MU-2/9 - Trim Aileron Bellcrank Bracket Bolt Holes - Inspection

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

1/10 complexity

This Airworthiness Directive (AD) is a safety order requiring owners and operators of Mitsubishi MU-2 aircraft to inspect specific bolt holes in the trim aileron bellcrank bracket.

What you must do:

Inspect the trim aileron bellcrank bracket bolt holes following the procedures in Mitsubishi Service Bulletin No. 164 (an external technical document incorporated into this law)
Complete this inspection within 50 hours of flight time after 28 June 1974

Who it affects: Anyone operating Mitsubishi MU-2 series aeroplanes in Australia.

Why it matters: This directive addresses potential structural or mechanical issues with critical flight control components. The bellcrank bracket is part of the aircraft's control system, and defects in these bolt holes could affect the pilot's ability to control the aircraft safely.

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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

View image in the official source 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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Source text

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