Document ID: chunk:federal_register_of_legislation:F2006B02862:body:0:p2
Version: federal_register_of_legislation:F2006B02862
Segment Type: other
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Character Range: 2952–3909

PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Compliance:   For Requirement 1 - Within six months after the effective date of this Directive.

            For Requirement 2 - Before further flight after the Requirement 1 test. For Requirement 3 - Before further flight after the Requirement 1 test. This Airworthiness Directive becomes effective on 6 September 2001.
            Background:  This Directive requires a test of the two electrical circuits that close the fuel shutoff valve on the wing spar, and repair, if necessary. This action is necessary to prevent inability to shut off the flow of fuel to an engine after an uncontained engine failure which could result in a fire spreading to other parts of the aeroplane.

 James Coyne
 Delegate of the Civil Aviation Safety Authority 20 July 2001

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