Document ID: chunk:federal_register_of_legislation:F2006B03105:body:0
Version: federal_register_of_legislation:F2006B03105
Segment Type: other
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Character Range: 0–1069

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

 Boeing 747 Series Aeroplanes

 AD/B747/206 Upper Link Assembly on Number 2
                       and Number 3 Engine Struts

 7/99

            Applicability: Boeing 747 series aircraft, line positions 1 through 886; equipped with Pratt & Whitney JT9D-3 or -7, or General Electric CF6-45 or -50 engine struts.

            Requirement: Action in accordance with the technical requirements of FAA AD 99-08-01 Amdt 39- 11105.

            Note: Boeing Alert Service Bulletin 747-54A2187 refers.

            Compliance: Initial and repeat inspections 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 corrosion and cracks located at the four fasteners that attach to the aft end to the upper link assembly on the number 2 and number 3 engine struts.