AD/B747/124 - H-11 Steel Bolts

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

Legislation au F2006B03025 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 747 Series Aeroplanes

 

AD/B747/124 H-11 Steel Bolts 7/94

Applicability: Model 747 series aircraft with line numbers 641 through 708, excluding Model 747- 400 series aircraft.

 

Requirement: Action in accordance with the technical requirements of FAA AD 94-07-06 Amendment 39-8864.

 

Note: Boeing SB 747-51-2048 refers.

 

Compliance: As specified in the Requirement Document.

 

Background: Reports were received of cracked and fractured H-11 steel bolts installed at certain locations of the airframe structure. The actions specified in this Directive are intended to prevent the failure of attachment bolts at critical locations.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.