Document ID: chunk:federal_register_of_legislation:F2006B02660:body:0
Version: federal_register_of_legislation:F2006B02660
Segment Type: other
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Character Range: 0–839

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

 Boeing 727 Series Aeroplanes

AD/B727/138 Main Cargo Door 1/92

Applicability: Model 727 series as listed in the requirement document.

            Requirement: Action in accordance with the technical requirements of FAA AD 91-22-04 Amdt 39-8064.

Note: Boeing SB 727-52-0142 refers.

            Compliance: As specified in the requirement document with a revised effective date of 12 January 1992 for Australian Registered Aircraft.

            Background: This AD arises from reports of worn latch cams and worn pressure relief door hinge fittings, and a report of a main cargo door that opened in flight. The effective date required by the FAA is extended by approximately one month.