AD/B747/15 Amdt 1 - Trailing Edge Flap Track Fuse Bolt - Inspection and Replacement

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B03051 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 747 Series Aeroplanes

 

AD/B747/15

Amdt 1


Trailing Edge Flap Track Fuse Bolt - Inspection and Replacement


9/82

 

Applicability: All model 747 aeroplanes listed in Boeing SB 747-57-2206 R.1. Document:  Boeing SB 747-57-2206, Rev. 1.

Compliance: As detailed in the Requirement Document.

 

Background: Amdt. 1 introduces SB 747-57-2206, Rev. 1 which supersedes SB 747-57-2177.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.