Document ID: chunk:federal_register_of_legislation:F2006B11387:body:0
Version: federal_register_of_legislation:F2006B11387
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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-2/57 Acrylic Windshield and Side Windows 6/96

 Applicability: MU-2B -10, -15, - 20, -25, -26 S/N 008 to 347 (except 313 and 321), and -30, -35, -
            36, S/N 501 to 696 (except 652 and 661); equipped with windscreen, cockpit or cabin windows P/Nos:

            010A-31450-1 or -2 010A-31451-1 or -2

            010A-31874-1 or -2 010A-31870

            010A-31870-11 030A-32402

 Requirement: Inspect, and replace as necessary, in accordance with MHI MU-2 SB 224A.

            Note: JCAB AD TCD-4311-95 refers.

            Compliance: Within 100 hours time in service after 23 May 1996, thereafter at intervals not exceeding 100 hours time in service.

            Background: This Directive is issued to prevent possible in-flight failure of the acrylic transparencies due to undetected cracking.