Document ID: chunk:federal_register_of_legislation:F2006B03072:body:0
Version: federal_register_of_legislation:F2006B03072
Segment Type: other
Provision Reference: 
Character Range: 0–1121

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

 Boeing 747 Series Aeroplanes

 AD/B747/17
 Amdt 2

       Inboard Engine Strut-To-Diagonal Brace Attach Fitting

 1/96

 Applicability: Model 747 series aircraft as listed in Boeing Service Bulletin (SB) 747-54-2062 Rev.
            7.

            Requirement: Inspect the inboard strut-to-diagonal brace fittings for cracking in accordance with FAA AD 95-20-05 Amdt 39-9383.

            Note: Boeing SB 747-54-2062 Rev. 7 refers.

            Compliance: As specified in the Requirement Document with a revised effective date of 4 January 1996.

            Background: A number of operators reported cracked fittings found in service. Amendment 1 reflected the revision status of SB 54-2062 which allowed terminating action including installation of a cover plate to seal a gap in the web. Amendment 2 is issued in response to reports of cracking and severing of the attach fittings. This amendment expands the applicability and requires an additional inspection.