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AD/MU-2/31 - Cockpit Airconditioning Ducts - Inspection and Modification
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AD/MU-2/31 - Cockpit Airconditioning Ducts - Inspection and Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Mitsubishi MU-2 Series Aeroplanes
and Modification
Applicability: All models MU-2B-26A/-40 with S/Nos. 321SA, 348SA, 350SA to 457SA.
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.