AD/F28/24C - Cargo Doors - Door Lock Mechanism - Inspection and Modification

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

Legislation au F2006B09761 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/F28/24C  Cargo Doors - Door Lock NK Mechanism - Inspection and Modification

Applicability: All models with S/Nos. 11003 to 11993.

 

Requirement: 1. Inspect door locking mechanism as per Part 2 of SB F28/52-53 by aircraft S/No. as referenced in applicable SB.

 

2.    Modify door locking mechanism by fitting a reinforced safety catch and stop assembly, detailed in SB F28/52-51 on aircraft with S/nos. referenced in that service bulletin.

 

3.    Further modify door locking mechanism by fitting a revised switch operating mechanism as detailed in SB F28/52-49 on aircraft with S/No. referenced in that service bulletin.

 

4.    Further modify the cargo door locking mechanism by reinforcing the door locking handle access panel as detailed in SB F28/52-81 on aircraft with S/Nos. and cargo door configurations referenced in that SB. RLD AD A118/77 also refers.

 

Compliance: For Para. 1 - Before 1 September 1974.

 

For Para. 2 - Before 1 January 1975.

 

For Para. 3 - Before 1 January 1975.

 

For Para. 4 - Before 15 July 1978.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.