Document ID: chunk:federal_register_of_legislation:F2006B03104:body:0
Version: federal_register_of_legislation:F2006B03104
Segment Type: other
Provision Reference: 
Character Range: 0–1092

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

 Boeing 747 Series Aeroplanes

AD/B747/204 Number 1 Main Entry Door Cutout 7/99

 Applicability: Model 747 series aircraft, line numbers 1 through 685.

            Requirement: Perform eddy current inspection in accordance with the technical requirements of FAA AD 99-07-03 Amdt 39-11085.

            Note: Accomplishment of the repair or preventative modifications specified in ASB 747-53A2414, constitutes terminating action for the repetitive inspection requirements of this Directive for that repaired/modified edge frame web and doubler.

            Compliance: Initial and repetitive inspection as specified in the Requirement Document with a revised effective date of 15 July 1999.

            This Airworthiness Directive becomes effective on 15 July 1999.

            Background: The FAA received reports of fatigue cracks found in the edge frame web and doubler at the door stop number 1 of the number 1 main entry door cutout.