Document ID: chunk:federal_register_of_legislation:F2009L03450:body:0:p2
Version: federal_register_of_legislation:F2009L03450
Segment Type: other
Provision Reference: 
Character Range: 4514–7293

OFF when either the CTR L FUEL PUMP or CTR R FUEL PUMP message displays if the centre tank is empty.  During cruise flight, both centre tank pump switches may be reselected ON whenever centre tank usable fuel is indicated.
   DE-FUELING AND FUEL TRANSFER
   When transferring fuel or de-fuelling centre or main wing tanks, the fuel pump low PRESS lights must be monitored and the respective fuel pump switches positioned to "OFF'' at the first indication of low pressure.  Prior to transferring fuel or de-fuelling, conduct a lamp test of the respective fuel pump low PRESS lights.
   Intentional dry running of a centre tank fuel pump (CTR L FUEL PUMP or CTR R FUEL PUMP message displayed on EICAS) is prohibited.
   Do not reset a tripped fuel pump or fuel pump control circuit breaker.
   Revision of the AFM may be accomplished by inserting a copy of this Directive into the AFM.
   Note 1:  When statements identical to those in Requirement 2 have been included in the general revisions of the AFM, the general revisions may be inserted into the AFM, and the copy of this Directive may be removed from the AFM.
      3. For Model 767-200, -300 and -300F aeroplanes that meet either of the conditions specified in sub-paragraphs a. or b. or c. below, install a placard in the flight deck adjacent to each pilot's primary flight display, to alert the flightcrew to follow the procedures required by AD/B767/167 Amdt 3.  The placard must include the following statement: "AD/B767/167 Amdt 3 fuel usage restrictions required.''
        a. The aeroplane is operated in a fleet of aeroplanes on which the actions specified in Requirement 1 of this Directive have been accomplished on at least one of the fleet's aeroplanes.
        b. Modified centre tank override and override/jettison fuel pumps (ie pumps that are not subject to the unsafe condition addressed by this Directive) have not been installed in accordance with either AD/B767/167 Initial Issue, Amdt1, Amdt 2 or Amdt 3.
        c. Requirement 1 of this Directive has not been accomplished.
   Note 2:  If the actions specified in Requirement 1 of this Directive have been accomplished on all aeroplanes operated within an operator's fleet, or if operation according to the fuel usage restrictions of AD/B767/167 Amdt 3 is maintained until automatic shutoff systems are installed on all aeroplanes in an operator's fleet:  No placard is necessary before removal of the wet shutoff restrictions of AD/B767/167 Amdt 3.

             Deactivation of the centre fuel tanks, in accordance with Boeing Alert Service Bulletin 767-28A0050, dated 18 December 1997; or Boeing SB 767-28A0050, Revision 1, dated 22 December 1999; terminates Requirement 1, 2 and 3 of this Directive, except as provided by Requirements 4 and 5 of