Document ID: chunk:federal_register_of_legislation:F2006B02864:body:0:p2
Version: federal_register_of_legislation:F2006B02864
Segment Type: other
Provision Reference: 
Character Range: 2846–3538

within 3 years from the effective date of this Directive.

           This Airworthiness Directive becomes effective on 6 September 2001.

           Background:  This Directive is issued to prevent failure of the motor operated hydraulic shutoff valves, which could result in leakage of hydraulic fluid to the engine fire zone, reduced ability to retract the landing gear, loss of backup electric power or other combination of failures, and consequent reduced controllability of the aeroplane.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 27 July 2001

 The above AD is notified in the Commonwealth of Australia Gazette on 15 August 2001.