AD/B737/48 - Rudder Trim

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

Legislation au F2006B02947 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 737 Series Aeroplanes

 

AD/B737/48 Rudder Trim 11/90

Applicability: All model 737-300 and 737-400 series.

 

Requirement: 1. Replace the rudder trim control knob with a smooth round fluted knob.

 

2. If the rudder trim control knob is located near the rear of the cockpit centre console, add a guard rail with a height of approximately 38 mm (1.5 inches) to the rear of the cockpit centre console if no rail is currently installed; or, if a rail is currently installed, raise the cockpit centre console rear rail to a height of approximately 38 mm (1.5 inches).

 

Note: FAA AD 90-14-02 Amdt 39-6644 and Boeing Service Bulletin 737-27-1165 refer.

 

Compliance: Prior to 30 November 1991.

 

Background:  This Directive is raised in response to reports of inadvertent rudder trim actuation. This condition could lead to a take-off with an improperly trimmed rudder, and may result in a rejected take-off.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.