Document ID: chunk:federal_register_of_legislation:F2005L00581:body:0:p3
Version: federal_register_of_legislation:F2005L00581
Segment Type: other
Provision Reference: 
Character Range: 5541–8786

exposed, and evidence of arcing is not detected; accomplish either Requirement 2.a. or 2.b.

                   6. If, during the Requirement 1.a. inspection, any electrical arcing or exposed copper conductor is detected, carry out either of the following:

                     a. replace any section of the electrical conduit where the arcing occurred with a new section, in accordance with the ASB 737-28A1132 or Revision 1 or Revision 2, and accomplish Requirement 2.b.;

                   or

                     b. perform a detailed visual inspection to detect fuel leaks of the electrical conduit, in accordance with the ASB 737-28A1132 or Revision 1 or Revision 2.

                   7. If no fuel leak is detected during the Requirement 6.b. inspection, accomplish Requirement 2.b. and repeat the Requirement 6.b. inspection.

                   8. If any fuel leak is detected during the Requirement 6.b. inspection, replace any section of the electrical conduit where the leak is with a new section, in accordance with the ASB 737-28A1132 or Revision 1 or Revision 2.  Immediately following the replacement, accomplish Requirement 2.b.

                   9. If, during the Requirement 1.a. inspection, any presence or scent of fuel on the electrical wires is detected, locate the source of the leak and replace the damaged conduit with a new conduit in accordance with the ASB 737-28A1132 or Revision 1 or Revision 2.  Immediately following the replacement accomplish Requirement 2.a. or 2.b. unless, unless previously accomplished in accordance with Requirements 2, 5 or 6.

                   10. For aeroplanes on which Requirement 1.b. has been accomplished, carry out the following actions:

                     a. Operators must ensure that aeroplane fuelling crews are properly trained in accordance with the procedures specified in Boeing Telex M-7200-98-04486, dated 1 December 1998.  This one-time training must be accomplished prior to utilising the procedures specified in Requirement 10.c.
                     b. Prior to fuelling the aeroplane, perform a check to verify that the fuelling panel centre tank quantity indicator is operative.

                        i. If the fuelling panel centre tank quantity indicator is found to be inoperative following the Requirement 10.b. check, replace the fuelling panel centre tank quantity indicator with a serviceable part.

                     c. One of the two manual fuelling procedures for the centre fuel tank must be used for each fuelling occurrence, in accordance with Boeing Telex M-7200-98-04486, dated 1 December 1998.

                Where there are differences between Boeing ASB and this Directive, the Directive prevails.

                   11. Dispatch with the centre fuel tank float switch deactivated, in accordance with ASB 737-28A1132 or Revision 1 is allowed until replacement float switches and wiring are available for installation.  Where there are differences between the Master Minimum Equipment List (MMEL) and this Directive, this Directive prevails.

                   12. For aeroplanes having line numbers 1 to 3108 inclusive, on which the Requirement 6.b. inspection has been accomplished prior to the effective date