AD/BAe 146/70 - Skin Inspection at Frame 29 between Stringers 12 and 13

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

Legislation au F2006B03518 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 146/70  Skin Inspection at Frame 29 between Stringers 12 and 13


8/98

 

Applicability: All BAe 146 Series 100 and 200 aircraft, and Series 300 aircraft with constructors numbers listed in effectivity of SB 53-144.

 

Requirement: Inspect in accordance with British Aerospace Mandatory Service Bulletin 53-144, classified mandatory by UK CAA.

 

Compliance: As specified in the Requirement document.

 

This airworthiness directive becomes effective on 16 July 1998.

 

Background: Fatigue cracking of the skin in the vicinity of frame 29 between stingers 12 and 13 has been found on two aircraft during routine inspection.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.