Document ID: chunk:federal_register_of_legislation:F2006B10445:body:0:p2
Version: federal_register_of_legislation:F2006B10445
Segment Type: other
Provision Reference: 
Character Range: 2883–4698

and ensure that a minimum clearance of 6mm (0.25-inch) exists between the wire bundle and the fuel cross-feed valve operating valve throughout its range of travel, in accordance with the applicable service bulletin.

b.         If any chafing is detected, repair the chafed wire, ensure that the wire bundle is routed correctly and ensure that a minimum clearance of 6mm (0.25-inch) exists between the wire bundle and the fuel cross-feed valve operating valve throughout its range of travel, in accordance with the applicable service bulletin.
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

            Note 2: FAA AD 2000-22-22 Amdt 39-11970 refers.

            Compliance: For Requirement 1 - Within 50 flight hours or 6 months after the effective date of this Directive, whichever occurs first.

            For Requirement 2 - Before further flight.

            This Airworthiness Directive becomes effective on 25 January 2001.

            Background:  This Directive requires inspection of the wire bundle to relay 'KT' on panel 'JA' for correct routing, adequate clearance from the fuel cross-feed valve operating lever, and the presence of chafing. The Directive also requires necessary action to correct any wiring anomaly.

            These actions are intended to detect and correct chafing of the wire bundle exiting panel 'JA' due to insufficient clearance from the fuel cross-feed valve operating lever. Chafing of the wire bundle could result in a fire in the area of the fuel system in a confined space.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 11 December 2000

 The above AD is notified in the Commonwealth of Australia Gazette on 20 December 2000.