AD/MU-2/54 - Tip Tank Wiring Conduit

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B11384 In force Legislative Instrument

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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-2/54 Tip Tank Wiring Conduit 2/94

Applicability: MU-2B-10, -15, -20, -25 and -26 S/N 008 through 347 (except S/N 313 and 321) and

MU/2B/-30, -35 and -36 S/N 501 through 696 (except S/N 652 and 661).

 

Requirement: Unless previously carried out action in accordance with Mitsubishi MU-2 Service Bulletin No 221.

 

Note: JCAB TCD-3901-93 refers.

 

Compliance: Within 100 hours time in service from 28 February 1994.

 

Background: The manufacturer has advised that due to corrosion in the conduit which carries the navigation light and fuel low level switch wiring which could allow fuel to leak into the wiring conduit.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.