Document ID: chunk:federal_register_of_legislation:F2005L03578:body:0:p2
Version: federal_register_of_legislation:F2005L03578
Segment Type: other
Provision Reference: 
Character Range: 2968–4041

the fuel tank caused by steel-to-steel contact during dry fuel pump operation.

                This amendment provides terminating actions for AD/B767/55 for those pumps fitted with machined diffuser rings.

                Amendment 2 changed the original compliance period for paragraph (i) of the requirement document following issue of FAA letter approving an extension.  This followed a submission from Boeing to be given sufficient time to carry out tests etc. to investigate operator reports of intermittent fuel imbalance caused by modified replacement pumps.

                Amendment 1 provided terminating actions as detailed in the requirement document with reference to the relevant Australian Directive.

                The original issue of the Airworthiness Directive became effective on 17 April 2003.

                Amendment 1 of this Directive became effective 30 October 2003.

                Amendment 2 of this Directive became effective on 20 January 2005.

James Coyne
Delegate of the Civil Aviation Safety Authority

11 November 2005