AD/B727/124 - Fuselage Crown Skin Circumferential Joint BS 1080

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Legislation au F2006B02646 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 727 Series Aeroplanes

 

AD/B727/124 Fuselage Crown Skin Circumferential

Joint BS 1080

Applicability: Model 727-100 and 727-100C aircraft listed in the Requirement document.


2/91

 

Requirement: Action in accordance with the technical requirements of FAA AD 90-21-10 Amdt 39-6761.

 

Note: Boeing SB 727-53-0109 Rev 1, Rev 2 and Rev 3 refer.

 

Compliance: As specified in the Requirement document with effective date 13 November 1990.

 

Background: Country of origin AD. To detect delamination, cracking, and/or corrosion that may lead to depressurisation.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.