AD/F27/106 - Elevator: Inboard Trim Tab Hinge Bracket and Control Bracket - Inspection

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

Legislation au F2006B09675 Not 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 F27 Series Aeroplanes

 

AD/F27/106 Elevator: Inboard Trim Tab Hinge Bracket

and Control Bracket - Inspection

Applicability: As detailed in requirement document. Document:  Fokker SB F27/55-56.

Compliance: Before 1st July 1982.


4/82

 

Background: Manufacturers reports of severe damage to the elevator and elevator trim tab after excessive vibration in flight. The probable cause was determined to be installation stresses during incorporation of SB F27/55-31.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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.