Document ID: chunk:federal_register_of_legislation:F2006B11361:body:0
Version: federal_register_of_legislation:F2006B11361
Segment Type: other
Provision Reference: 
Character Range: 0–853

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.

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            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.