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MANUAL
REFUEL
REFUEL
NO AFT
FUEL
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
12−10−19
REFUEL/DEFUEL PANEL (CONT'D)
GF1210_020
PRESELECT TOTAL
QTY DISPLAY
Displays the fuel
quantity target for
automatic refueling. Set
in 100 lb (50 KG)
increments.
LEFT/RIGHT/CTR/AFT/TOTAL
Displays the current fuel
quantity in each tank and the
total quantity of all tanks.
Quantities are displayed in 50 lb
(25 KG) increments.
INCR/DECR
Increases or decreases
the preselect quantity for
AUTO refueling.
MANUAL FUEL SOVs
Allows tanks to be
refueled or defueled
manually.
MASTER ON/OFF
Supplies power to the
components required for
fueling/defueling.
SHUT OFF TEST
When selected shuts off
all valves to verify their
operation. It also carries
out a test of the high
level sensors and
circuitry in each tank
during refueling.
AFT ON/OFF
Enables or disables the
automatic function of
refueling the aft tank.
START/STOP
(for AUTO mode only)
START − Starts
automatic refueling.
STOP − Stops
automatic refueling.
MODE SELECTOR
REFUEL − Enables
manual refueling.
AUTO REFUEL −
Enables automatic
refueling.
DEFUEL − Enables
manual defueling.
REFUEL/DEFUEL PANEL MASTER
ON
INCR
DECR
PRESEL
RIGHT
AFT
TOTAL
LEFT
CTR
30000
10000
8000
LB 30000
10000
2000
LB
MANUAL
LEFT CTR RIGHT AFT
OPEN
CLOSE
REFUEL
DEFUEL
AUTO REFUEL
START
REFUEL
AUTO
STOP
AFT
ON
OFF
SHUT
OFF
TEST
OFF
Normal Fuel Loading
The normal fuel loading is as follows:
· Wing tanks only if the required fuel load is equal to or less than the wing tank capacity.
· Wing tanks full and the remainder in the aft tank if the required fuel load is greater than the
wing tank capacity, but less than or equal to the combined capacity of the wing and aft
tanks.
FUEL
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
12−10−20
REFUEL/DEFUEL PANEL (CONT'D)
Normal Fuel Loading (Cont’d)
· Any fuel in excess of the combined capacity of the wing and aft tanks is placed in the centre
tank.
NOTE
The left and right wing tank quantities must be within 400 lbs
(181 KG) for normal fuel loading.
An additional switch position on the refuel/defuel panel allows auto refueling without adding fuel to
the aft tank.
REFUEL NO AFT
This switch position
inhibits refueling of the
aft tank.
IF INSTALLED
GF1210_021
AFT
ON
OFF
REFUEL
DEFUEL
AUTO
OFF
MANUAL
REFUEL
REFUEL
NO AFT
If the aft tank fueling is inhibited by the switch then the refuel sequence is as follows:
· Wing tanks only if the required fuel load is equal to or less than the wing tank capacity.
· Wing tanks full and the remainder in the centre tank if the required fuel load is greater than
the total wing capacity.
Gravity Refueling
The wing tanks may be refueled through over wing gravity fill adapters located on top of both left
and right wings. It is not possible to completely fill either wing tank by gravity fueling, since the fill
adapters are located outboard and below the maximum fuel level.
The centre tank may be refueled through a gravity fill adapter located on top of the right hand
wing.
Gravity fueling of the aft tank is not provided.
Pressure Refueling
Pressure refueling is accomplished through the single point refuel/defuel adapter, located in the
right hand wing root and is controlled by the refuel/defuel control panel. An optional duplicate
refuel/defuel control panel can be installed in the flight compartment.
NOTE
A “SHUTOFF
TEST” must be carried out prior to all refueling
operations.
If the test is successful a “SOV PASS” is displayed in the PRESEL window. If the test fails a “SOV
FAIL” is displayed in the PRESEL window. “SOV FAIL” will be displayed in the tank window for
the failed shutoff
valve, alternating display of the tank quantity.
Pressure refueling may be performed in either “AUTOMATIC” or “MANUAL” mode. The airplane
does not have a fuel jettison system.
FUEL
　
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