Document ID: chunk:federal_register_of_legislation:F2008L00533:body:0:p1
Version: federal_register_of_legislation:F2008L00533
Segment Type: other
Provision Reference: 
Character Range: 0–3129

AIRWORTHINESS DIRECTIVE
On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/B737/303 Amdt 1 and issues the following AD under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Boeing 737 Series Aeroplanes
AD/B737/303 Amdt 2  Fuel Boost Pump Wiring  3/2008

Applicability:  Model 737-100, -200, -200C, -300, -400 and -500 series aeroplanes.
Requirement:       1. Carry out a detailed inspection for damage of the sleeve and electrical wire of the fuel boost pump in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin (ASB) 737-28A1263 Revision 2 dated 10 August 2007.
                   2. Install new, smaller-diameter sleeving on the fuel boost pump wiring, carry out any related investigative and corrective actions, as applicable, in accordance with ASB 737-28A1263, Revision 2.
                   3. Submit a report of the findings (both positive and negative) of any Requirement 1 inspection and send any damaged parts to the manufacturer, as described in ASB 737-28A1263, Revision 1.  The report must include the inspection results, a description of any discrepancies found, the aeroplane serial number together with the number of landings and flight hours on the aeroplane.
                Actions accomplished before 31 August 2007 (the effective date of Amendment 1 of this Directive) in accordance ASB 737-28A1263, dated 19 February 2007, or actions accomplished before 13 March 2008 (the effective date of this Amendment) in accordance with ASB 737-28A1263 Revision 1, are considered acceptable for compliance with the corresponding actions specified in this Directive.
                Later revisions of ASB 737-28A1263, approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2007-24-02, are considered acceptable for compliance with the equivalent Requirements of this Amendment.
                Note:  FAA AD 2007-24-02 Amdt 39-15268 refers.

Compliance:     For Requirement 1 -
                     a. Model 737-100, -200, -300, -400 and -500 series aeroplanes having line numbers 1 through 3072 inclusive - Within 120 days after the effective date of this Amendment, or within 5,000 hours time in service (TIS) after the last inspection or repair done in accordance with any version of ASB
                     737-28A1120 listed in Table 1, whichever occurs later and thereafter, at intervals not to exceed 15,000 hours TIS.
                     b. Model 737-100, -200, -300, -400 and -500 series aeroplanes having line numbers