(a)
For the main tanks, do these steps:
1) Remove the air mover from the overwing fill port
(Fig. 203). 2) Remove the ground from the air mover. 3) Remove the air mover adapter assembly from the overwing
fill port. 4) Install the cap on the overwing fill port. 5) Install the applicable main tank access doors
(AMM 28-11-01/401).
(b)
For the surge tanks, do these steps: 1) Remove the air mover from the adapter base (Fig. 203). 2) Remove the ground from the air mover. 3) Remove the tank adapter assembly from the opening of the
surge tank access door. 4) Install the surge tank access doors (AMM 28-11-03/401).
(c)
For the center fuel tanks, do these steps: 1) Remove the air mover from the adapter base (Fig. 203).
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MAINTENANCE MANUAL
2) Remove the ground from the air mover. 3) Remove the tank adapter assembly from the opening of the center tank access door. 4) Install the center tank access doors (AMM 28-11-02/401).
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(16)
FOR AIR BLOWER TYPE VENTILATION EQUIPMENT; Do these steps to remove the air blower equipment:
(a)
For the main tanks, do these steps: 1) Remove the ground from the airplane to the ventilation blower.
2) Install the applicable main tank access doors (AMM 28-11-01/401).
(b)
For the surge tank access doors, do these steps: 1) Remove the ground from the airplane to the ventilation
blower. 2) Install the surge tank access doors (AMM 28-11-03/401).
(c)
For the center tank, do these steps: 1) Remove the ground from the airplane to the ventilation
blower. 2) Install the center tank access doors (AMM 28-11-02/401).
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(17) Follow approved procedures to clean and return all respiratory equipment.
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WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO REMOVE THE DOOR LOCKS.
_______ DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(18) Remove the door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
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WARNING: DO THE ACTIVATION PROCEDURE FOR THE TRAILING EDGE FLAPS.
_______ ACCIDENTAL OPERATION OF THE TRAILING EDGE FLAPS COULD CAUSE INJURY TO PERSONS.
(19) Do the activation procedure for the trailing edge flaps (AMM 27-51-00/201).
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本文链接地址：757 AMM 飞机维护手册 燃油 CHAPTER 28 - FUEL 1(56)
