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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