AD/BAe 146/42 - Wing Centre Section Top Skin

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

Legislation au F2006B03493 Not 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

 


British Aerospace BAe 146 Series Aeroplanes

 

AD/BAe 146/42 Wing Centre Section Top Skin 4/92

Applicability: All Series 146 aircraft pre mod HCM 00851C.

 

Requirement: Action in accordance with Mandatory BAe 146 Service Bulletin SB 57-41, dated 26 July 1991.

 

Compliance: Inspect before achieving 24 000 flights and then at intervals not exceeding 9 000 flights.

 

Background:  Recent results from the manufacturer’s airframe structural test program have indicated that cracking should be expected in both the LH and RH upper wing skin panels, beneath the upper centre line butt strap.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.