AD/B737/63 - Stabilizer Trim Jackscrew Actuator

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

Legislation au F2006B02963 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

 


Boeing 737 Series Aeroplanes

 

AD/B737/63 Stabilizer Trim Jackscrew Actuator 12/91

Applicability: Model 737-300, -400 and -500 series, as listed in Boeing SB 737-27-1161. Requirement:               Action in accordance with the Technical Requirements of FAA AD 91-20-04 Amdt

39-8038.

 

Note: Boeing SB 737-27-1161 refers.

 

Compliance: As specified in the requirement document with a revised effective date of 12 December 1991 for Australian registered aircraft.

 

Background: Reports have been received of worn auxiliary trim brakes that may allow slippage and movement of the horizontal stabilizer under certain conditions. The effective date required by the FAA is extended by one month.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.