Document ID: chunk:federal_register_of_legislation:F2007L00698:body:0:p2
Version: federal_register_of_legislation:F2007L00698
Segment Type: other
Provision Reference: 
Character Range: 2849–5957

the Accomplishment Instructions of Boeing Alert Service Bulletin 767-28A0088 (for Model 767-200, -300, and -300F series aeroplanes) or Boeing Alert Service Bulletin 767- 28A0089 (for Model
                   767-400ER series aeroplanes), both dated 24 February 2005, as applicable.

             Optional Terminating Action--Records Review

             For any period when the part number (P/N) of a main tank fuel boost pump installed on any aeroplane, as conclusively determined from a review of aeroplane maintenance records, is P/N 5006003D, no further action is required by Requirement 1 of this AD for that pump only.

             Accomplishment of the replacement terminates the repetitive measurement detailed in Requirement 1 of this AD for that pump only.

             Note 3:  Boeing Alert Service Bulletins 767-28A0088 and 767- 28A0089 reference Hamilton Sundstrand Service Bulletin 5006003-28-3, dated 8 December 2004, as the appropriate source of service information for modifying the pump.

                3. Only main tank fuel boost pumps identified in paragraphs (a) and (b) below may be installed on any aeroplane.

                  (a) Any main tank fuel boost pump that has been inspected, and on which all applicable corrective actions have been performed, in accordance with Requirement 1 of this AD.

                  (b) Any main tank fuel boost pump having P/N 5006003D.

             Note 4:  FAA AD 2007-04-16 Amdt 39-14948 dated 5 February 2007 refers.
Compliance:     1. For aeroplanes having line numbers (L/Ns) 1 through 914 inclusive:

                Within 12 months after the effective date of this AD, thereafter at intervals not to exceed the applicable time specified in paragraphs (a) or (b) below, until the replacement required by Requirement 2 of this AD is accomplished.  All applicable corrective actions must be done before further flight.

                  (a) For aeroplanes that have accumulated more than 15,000 total flight hours as of the date the initial actions are done in accordance with Requirement 1 of this AD:  Repeat the measurement thereafter at intervals not to exceed 6,000 flight hours or 24 months, whichever comes first.

                  (b) For aeroplanes that have accumulated 15,000 total flight hours or fewer as of the date the initial actions are done in accordance with Requirement 1 of this AD:  Within 12 months after the date on which the aeroplane accumulates 15,000 total flight hours or within 24 months after performing the initial inspection required by Requirement 1 of this AD, whichever occurs later. Repeat the measurement thereafter at intervals not to exceed 6,000 flight hours or 24 months, whichever comes first.

                For aeroplanes having L/Ns 915 and on:

                For aeroplanes that have accumulated more than 15,000 total flight hours as of the effective date of this AD, do the actions within 12 months after the effective date of this AD.  All applicable corrective actions must be done before further flight.

                For aeroplanes that have accumulated