S 866-033
(7) Remove the electrical power if it is not needed for another task (AMM 24-22-00/201).
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28-22-00
ALL ú ú 04 Page 615 ú Jun 10/97
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F57839
Fuel Pump Inspection Data Sheet - Installed Pump
Figure 602 (Sheet 1)
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747 FUEL PUMP INSPECTION DATA SHEET - INSTALLED PUMP
A
747-400
MAINTENANCE MANUAL
Fuel Pump Inspection Data Sheet - Installed Pump
Figure 602 (Sheet 2)
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F92832 G58496
Fuel Pump Inspection Data Sheet - Replacement Pump (If Necessary)
Figure 603 (Sheet 1)
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747 FUEL PUMP INSPECTION DATA SHEET - REPLACEMENT PUMP
IF NECESSARY
A
747-400
MAINTENANCE MANUAL
A
747-400
MAINTENANCE MANUAL
Fuel Pump Inspection Data Sheet - Replacement Pump (If Necessary)
Figure 603 (Sheet 2)
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G58515
A
747-400
MAINTENANCE MANUAL
ADDITIONAL DATA HERE
PARTNUMBER______ SERIALNUMBER______ COMMENTS:
Fuel Pump Inspection Data Sheet
Figure 604
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F57892
A
747-400 MAINTENANCE MANUAL
ENGINE FUEL SHUTOFF (SPAR) VALVE ACTUATOR - REMOVAL/INSTALLATION
________________________________________________________________
1. General_______
A. This procedure has two tasks:
(1)
A task to remove the actuator for the engine spar valve.
(2)
A task to install the actuator for the engine spar valve.
B.
The engine fuel shutoff valve actuator will be referred to as the spar valve actuator in this procedure.
C.
Each main fuel tank contains one spar valve. The spar valve actuators are found on the front spar outside of the applicable main tank.
D.
AIRPLANES WITH PW OR RR ENGINES; The No. 1 and 4 spar valves are installed rotated 180 degrees compared to the No. 2 and 3 spar valves. The actuator, adapter shaft and valve body are all rotated in this 180 degree orientation. The TOP position marker on the adapter plate for the No. 1 and 4 engine spar valves must be on the bottom of the adapter plate.
TASK 28-22-01-004-001
2. Engine Spar Valve Actuator Removal (Fig. 401)__________________________________
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