AD/F50/23 - Elevator Control Rod Ends

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

Legislation au F2006B09849 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 F50 (F27 Mk 50) Series Aeroplanes

 

AD/F50/23 Elevator Control Rod Ends 10/89

Applicability: F27 Mark 050 aircraft with serial numbers 20103 through 20108, 20110 through

20147.

 

Requirement: Action in accordance with Fokker SB F50-27-006.

 

Note: RLD AD BLA89-56 refers.

 

Compliance: At the next scheduled 3000 hours inspection after 5 October 1989 or prior to 31 March 1990, whichever occurs first.

 

Background: Country of origin AD. Present rod ends have a semi-octagonal section, which may catch and retain foreign objects, leading to a potential jamming of elevator controls. Replacement rod ends required by this AD are less liable to jamming.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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.