AD/F28/76 - Landing Gear Locking Mechanism

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

Legislation au F2006B09810 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Fokker F28 Series Aeroplanes

 

AD/F28/76 Landing Gear Locking Mechanism 3/95

Applicability: All F28 aircraft serial number 11003 through 11241, 11991 and 11992. Requirement:  Unless previously carried out action in accordance with Fokker SB F28/32-153.

Note: RLD BLA AD 94-163 (A) refers.

 

Compliance: By 1 November 1995.

 

Background: The manufacturer has advised that a Fokker 100 experienced a main undercarriage collapse during landing. Subsequent investigation confirmed that no undercarriage component had failed but extreme inward side-load conditions during the landing caused the lock toggle link to be pulled out of the overcentre position resulting in a main gear collapse.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.