AD/MU-2/31 - Cockpit Airconditioning Ducts - Inspection and Modification

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

Legislation au F2006B11361 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-2/31 Cockpit Airconditioning Ducts - Inspection

and Modification

Applicability: All models MU-2B-26A/-40 with S/Nos. 321SA, 348SA, 350SA to 457SA.


1/84

 

MU-2B-36A/-60 with S/Nos. 661SA, 697SA to 699SA, 1501SA to 1542SA, 1544SA to 1547SA.

 

Document: Mitsubishi SB No. 040/21-002.

 

Compliance: Prior to issue of the next maintenance release after 21 December 1983.

 

Background:  The manufacturer advises that it may be necessary to re-route and modify the airconditioning ducting located above the electrical overhead panel due to the possibility of electrical arcing or shorting occurring in that area.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.