Document ID: chunk:federal_register_of_legislation:F2006B03021:body:0
Version: federal_register_of_legislation:F2006B03021
Segment Type: other
Provision Reference: 
Character Range: 0–1033

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

 Boeing 747 Series Aeroplanes

 AD/B747/120
 Amdt 1

  Lower Lobe Cargo Doors and Main Deck Side Cargo Door

 8/93
 DM

            Applicability: Model 747 series; as listed in Boeing SB 747-52-2186, Revision 4, and Boeing ASB 747-52A2233.

            Requirement: Action in accordance with the technical requirements of FAA AD 93-10-01 Amendment 39-8580.

 Compliance: As specified in the requirement document.

            The compliance of the initial issue of this Directive remains unchanged. This Amendment is effective from 10 June 1993.

            Background: The FAA has received numerous reports of corroded or cracked fittings, cam latch bellcranks, and cam latches.

            Amendment 1 is issued in response to a final rule correction of FAA AD 93-06-03 which clarifies the compliance time for accomplishing optional repetitive inspections of the cam latches.