Two fuel quantity indicators, one for each
wing, are located on the center instrument
panel (Figure 5-4). They indicate fuel quan-
tity in pounds times one thousand. Seven trans-
mitter units in each wing are electrically
connected to each fuel quantity indicator.
A magnetic fuel quantity indicator is provided
for the ventral tank. The indicator is located be-
tween the two fuel quantity indicators and
shows FULL, crosshatch, and EMPT. The high-
and low-level float switches send signals to the
indicators when the tank is full and empty, re-
spectively. The indicator shows crosshatch
anytime the tank is anywhere between full and
empty and when electrical power is off. A
small residual amount of usable fuel will re-
main in the tank after the ventral tank quantity
indicator shows EMPT during the climb. The
AUX FUEL TRANSFER lever should be left
in the open position for 5 minutes after tran-
sition from climb to cruise to ensure that fuel
transfer is complete. The ventral tank low-
level float switch maintains a circuit to provide
low VMO speed warning at 280 KIAS until
ventral tank fuel has been transferred.
REFUELING
The airplane can be gravity refueled through
a filler cap in the outboard section of each
wing and in the left rear side of the ventral tank
(Figure 5-5). A rubber flapper valve is fitted
beneath each wing refuel cap to close the out-
let in the event of an improperly closed cap.
Pressure refueling and defueling are provided
by a single-point connection on the right side
of the airplane below the right engine. Pressure
refueling is controlled from a refueling con-
trol panel (Figure 5-6). The panel is located
adjacent to the vestibule right-hand bulkhead;
the panel illumination is controlled by the
door ENTRY LIGHT and vestibule ENTRY
LIGHT switches. Electrical power for fuel
valve positioning is available directly from
the PE bus bar or battery No. 1 through the re-
fueling control panel ON-OFF power switch.
An option is also available for an aft external
refueling panel.
Revision 1
5-6
FOR TRAINING PURPOSES ONLY
HAWKER 800 XP
PILOT TRAINING MANUAL
FlightSafety
international
Figure 5-4. Fuel Indicators
Summary of Contents for 800 XP
Page 4: ......
Page 6: ......
Page 10: ......
Page 104: ......
Page 124: ......
Page 126: ......
Page 156: ......
Page 158: ......
Page 160: ......
Page 170: ......
Page 172: ......
Page 174: ......
Page 184: ......
Page 186: ......
Page 198: ......
Page 200: ......
Page 202: ......
Page 222: ......
Page 264: ......
Page 266: ......
Page 268: ......
Page 276: ......
Page 278: ......
Page 280: ......
Page 290: ......
Page 292: ......
Page 310: ......
Page 312: ......
Page 314: ......
Page 328: ......
Page 338: ......
Page 340: ......
Page 342: ......
Page 352: ......
Page 354: ......
Page 356: ......
Page 378: ......
Page 412: ......
Page 414: ......
Page 416: ......
Page 474: ......
Page 476: ......
Page 478: ......
Page 486: ......
Page 500: ......
Page 502: ......
Page 504: ......