Document ID: chunk:federal_register_of_legislation:F2006B07207:body:0:p2
Version: federal_register_of_legislation:F2006B07207
Segment Type: other
Provision Reference: 
Character Range: 3048–4107

for the Requirement 1 P/N 2-1203-3 brake initial inspection, and the Requirement 2 modification.

            This Airworthiness Directive becomes effective on 28 December 2000.

            Background:  Wheel brake system malfunctions have occurred on several of the affected aircraft where regular brake system maintenance had been performed. The actions specified by this Directive are intended to prevent wheel brake system malfunctions that could result in a fire in the brake area.

            Amendment 1 is issued in response to a new FAA AD which incorporates inspection and replacement requirements for additional landing gear brake assemblies. The FAA AD specifies wear and maximum clearance limits which take precedence over those specified in the service information.

            The original issue of this Airworthiness Directive became effective on 6 March 1992.

 David Alan Villiers
 Delegate of the Civil Aviation Safety Authority 8 November 2000

 The above AD is notified in the Commonwealth of Australia Gazette on 22 November 2000.