AD/B747/93 - Section 42 Fuselage Frame Web

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

Legislation au F2006B03271 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/B747/93 Section 42 Fuselage Frame Web 6/91

Applicability: Model 747 series with line numbers 001 through 045.

 

Requirement: Action in accordance with the technical requirements of FAA AD 91-06-03 Amdt 39- 6923.

 

Compliance: As specified in the Requirement Document with a revised effective date of 13 June 1991 for Australian registered aircraft.

 

Background: The FAA has received reports of multiple cracks in the Section 42 frames. This condition, if not corrected, could result in rapid depressurisation of the aircraft.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.