28-21-00
 (PRE-SB 28-29)  ú ú 01 Page 503 ú Sep 28/00

H09481
A

757
MAINTENANCE MANUAL

FUEL MANAGEMENT OVERHEAD
CONTROL PANEL AND FUEL PANEL, P5
QUANTITY INDICATOR

SEE A
EEC/FUEL QUANTITY TEST SWITCH
SEE B
RIGHT SIDEQUADRANT CONTROL PANEL, P61
STAND, P10 FUEL CONTROL PANEL SEE C
FLIGHT COMPARTMENT
L FUEL
R
PUMPS

PUMPSXFEED
ON ON
w w
AFT w AFT
PRESS VALVE PRESS
a a a
FUELON ON
w  QTY
w
FWD w
FWD
PRESS

VALVE PRESS
a a
a  EEC/FUEL QUANTITY TEST SWITCH
C PUMPS
FUEL  B
PP
CONFIG a
RR
EE
ON ON
SS
L R
Sa Sa
w w
LCR
5.7 8.5 5.7
L FUEL CONTROL
FUEL QTY
1 5 1 9.9

RUN
1 X 1000
2
RICH
FUEL TEMP `C TOTAL QTY CUT OFF
FUEL MANAGEMENT CONTROL PANEL AND FUEL QUANTITY INDICATOR FUEL CONTROL PANEL
A C
THE UNITS ARE IN LBS OR KGS.
1
AIRPLANES WITH ROLLS ROYCE ENGINES
2
Flight Deck Controls and Indications
Figure 502A

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH FORWARD AND AFT FUEL ú

 28-21-00
 CROSSFEED VALVES (POST-SB 28-29 OR  ú
 PRR 54578)  ú 01 Page 504 ú Sep 28/00

B72647
A

757 MAINTENANCE MANUAL
 S 865-035
 (4)  
Make sure these circuit breakers on the APU external power panel, P34, are in the closed position:

 (a)  
34A9, FLNG VALVES

 (b)  
34A10, FUEL QTY

 (c)  
34A11, FLNG CONT

 S 865-036
 (5)  Make sure the five EICAS circuit breakers on the overhead circuit breaker panel, P11, are closed.
 S 865-001
 WARNING: DO THE DEACTIVATION PROCEDURE FOR THE LEADING EDGE SLATS.
_______ ACCIDENTAL SLAT OPERATION COULD CAUSE INJURY TO PERSONS.
 (6)  
Do the deactivation procedure for the leading edge slats
 (AMM 27-81-00/201).

 E.
Test of the Pressure Fueling System

 S 015-037
 (1)  
Open the fueling station door, 621GB, on the leading edge of the right wing (AMM 06-44-00/201).

 S 215-038

 (2)  
Make sure the internal lighting on the LOAD SELECT indicators comes on (View B, Fig. 501).

 S 215-039

 (3)  
Make sure the fueling panel lights come on.
　
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