AD/F28/51 - Main Landing Gear Bay Cracking

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

Legislation au F2006B09786 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

 


Fokker F28 Series Aeroplanes

 

AD/F28/51 Main Landing Gear Bay Cracking 2/86

Applicability: All model F28 with S/Nos 11003 to 11091, 11094 to 11135, 11991 and 11992. Requirement:               Action in accordance with Fokker SB F28/57-76.

Note: RLD AD 85-87 refers.

 

Compliance: Prior to 31 March 1986.

 

The manufacturer reports an instance of a crack in the area of Station 2635 and the rear spar.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.