Document ID: chunk:federal_register_of_legislation:F2006B11360:body:0
Version: federal_register_of_legislation:F2006B11360
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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-2/30  Engine Electrical Harness - Inspection and Replacement of P/No MS25471 Electrical Cable

 Applicability: MU-2B-10/-15/-20/-25/-26 S/Nos 005 to 347 (except S/Nos 313 and 321).

            MU-2B-30/-35/-36 S/Nos 501 to 696 (except S/Nos 652 and 661).

 Document: Mitsubishi Heavy Industries SB No. 191.

              1. Inspect engine electrical harness in accordance with SB No. 191.

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2.    Replace unacceptable electrical wiring Part No. MS 25471 in accordance with SB No. 191.

            Note: JCAB AD No. TCD 2113-82 refers.

                 Compliance: Part 1 - Within 100 hours time in service after 31 January 1984 and thereafter at intervals not exceeding 100 hours time in service if required.

            Part 2 - Within 300 hours time in service after 31 January 1984.

            Background: The conducting portion of the electrical cable has been found protruding through the insulation.