Document ID: chunk:federal_register_of_legislation:F2006B03203:body:0
Version: federal_register_of_legislation:F2006B03203
Segment Type: other
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Character Range: 0–798

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

 Boeing 747 Series Aeroplanes

AD/B747/31 Aileron Control System - Modification 6/83

            Applicability: All model 747 with S/Nos. referenced in Boeing SB. 27-2065, SB 27-2095, SB 27- 2161 and SB 51-2032 as applicable.

 Document: Boeing SBs 747-27-2065, 747-27-2095, 747-27-2161, 747-51-2032.

            Note: FAA AD 82-02-10 refers.

            Compliance: Unless previously accomplished, within 3000 hours time in service after 30 June 1983.

            Background: Numerous occurrences of binding in the aileron control system are attributed to the accumulation of ice on the aileron control system in the wing gear wheel well area.