Document ID: chunk:federal_register_of_legislation:F2006B07540:body:0:p2
Version: federal_register_of_legislation:F2006B07540
Segment Type: other
Provision Reference: 
Character Range: 2802–4014

of this Directive.
              Replacement of faulty fittings found during the inspection detailed in Requirement 1 prior to further flight.

2.        Before further flight immediately following the Requirement 1 inspection.

3.        Within 25 hours TIS from the effective date of this Directive.

4.        Within 25 hours TIS from the effective date of this Directive.

5.        Within 25 hours TIS from the effective date of this Directive.

6.        From the effective date of this Directive.

7.        From the effective date of this Directive.

           This Airworthiness Directive becomes effective on 10 July 2003.

           Background: There have been failures of the fuel line nipple located between the gascolator and the elbow on the carburettor. Incorrect installation of the fuel line nipple, the elbow and removal of the bracing that supports the gascola tor lead to failure of the fuel line nipple and the elbow. Failure of the fuel line nipple or elbow can lead to fuel leakage causing engine stoppage or fire.

 Jim Coyne
 Delegate of the Civil Aviation Safety Authority 26 May 2003

 The above AD is notified in the Commonwealth of Australia Gazette on 18 June 2003.