Document ID: chunk:federal_register_of_legislation:F2006B07314:body:0
Version: federal_register_of_legislation:F2006B07314
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Character Range: 0–898

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Aerospatiale (Socata) TB20 (Trinidad) Series Aeroplanes

AD/TB20/11 Hydraulic Brake Line Clearance 11/87

            Applicability: All model TB20 and TB21 up to S/No 755 inclusive, except S/Nos 630, 631, 634, 636, 643, 648, 649, 656, 657, 658, 659, 661, 662, 663, 664, 750, 751, 752 and 753.

 Requirement: Action in accordance with Aerospatiale Socata SB No 33.

            Note: Bureau Veritas AD 87-118(A) refers.

            Compliance: Within 100 hours time in service or at the next scheduled inspection for maintenance release issue after 30 October 1987 whichever is the earlier.

            Background: The manufacturer has reported instances of the cockpit hydraulic brake lines being damaged by the aileron and rudder control rods.