Document ID: chunk:federal_register_of_legislation:F2006L00122:body:0:p2
Version: federal_register_of_legislation:F2006L00122
Segment Type: other
Provision Reference: 
Character Range: 4827–7109

may be required."
                Later revisions of the above Service Bulletins, approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2005-23-17, are considered acceptable for compliance with the equivalent Requirements of this Directive.
                Actions accomplished before the effective date of this AD in accordance with Boeing Special Attention Service Bulletin 737-28- 1193, dated 24 April 2003, or Boeing Special Attention Service Bulletin 737-28-1200, dated 10 July 2003; as applicable; including Information Notices 737-28-1193 IN 01 and 737-28-1200 IN 01, both dated 11 September 2003, as applicable, are acceptable for compliance with the corresponding actions required by this Directive.
                Note 2:  FAA AD 2005-23-17 Amdt 39-14375 refers.
Compliance:     For Requirement 1.a. - Within 18 months after the effective date of this Directive.
                For Requirement 1.b. - Before further flight after the Requirement 1.a. inspection.
                For Requirements 2.a. and 2.b. - Within 18 months after the effective date of this Directive.
                For Requirement 2.c. - Before further flight after the Requirement 2.a. or 2.b. inspection.
                This Airworthiness Directive becomes effective on 16 February 2006.
Background:     The FAA has received reports of chafed wiring behind the P15 refuel panel together with arcing to the back of the P15 refuel panel and adjacent wing structure.
                This Directive requires, for certain aeroplanes, a one-time detailed inspection for interference between a clamp assembly and the wires behind the P15 refuel panel together with any necessary corrective actions.  The Directive also requires for certain other aeroplanes, a one-time detailed inspection for discrepancies of the wires behind the P15 refuel panel together with any necessary corrective and related investigative actions.  Actions required by the Directive are designed to detect and correct chafing of the wiring behind the P15 refuel panel, which could lead to arcing and fire with consequent aeroplane damage and injury to refuelling personnel.

Charles Lenarcic
Delegate of the Civil Aviation Safety Authority

16 December 2005