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Controls and Indications .................................................................................................. 5-6
Operation......................................................................................................................... 5-9
Emergency/Abnormal .................................................................................................... 5-10
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5-ii 510OM-00
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ILLUSTRATIONS
Figure Title Page
5-1 Fuel Tank System ..................................................................................................... 5-2
5-2 NACA Scoop Fuel Vent ........................................................................................... 5-3
5-3 Fuel Tank Filler ........................................................................................................ 5-4
5-4 Sump Drain Valves................................................................................................... 5-4
5-5 Fuel Tank Servicing ................................................................................................. 5-4
5-6 Grounding Point ....................................................................................................... 5-5
5-7 Primary Ejector Pump .............................................................................................. 5-5
5-8 Fuel Controls ............................................................................................................ 5-6
5-9 Fuel Display in MFD (EICAS Normal Mode) ........................................................ 5-7
5-10 Alternate Fuel Display (EICAS Reversionary Mode) ............................................. 5-7
5-11 CAS Messages.......................................................................................................... 5-8
5-12 ENGINE FIRE and BOTTLE ARMED Lights ....................................................... 5-9
TABLE
Table Title Page
5-1 Fuel System Capacity............................................................................................... 5-3
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GENERAL
The Citation Mustang fuel system includes two
integral wing fuel tanks, an automatic fuel distribution
system, and manual fuel transfer capability
(Figure 5-1). Each wing tank includes
an integral engine feed bay. A primary ejector
pump and an electrically powered boost pump
provide fuel to the respective engine. Switches
on the lower pilot tilt panel and CAS messages
on the multifunction display (MFD) control and
indicate fuel operation and transfer.
0
2
4 6
8
10
MAIN
FUEL
LBS X 100
CITATION MUSTANG OPERATING MANUAL
CHAPTER 5
FUEL SYSTEM
510OM-00 5-1
INTRODUCTION
This chapter presents information on the fuel system of the Citation Mustang. Integral
fuel tanks in the left and right wings provide fuel storage. The fuel distribution system
provides fuel to each engine from the corresponding wing tank. The fuel transfer system
allows fuel to be transferred from one tank to the other. Crew alerting system (CAS)
messages alert the pilot to fuel system emergency and abnormal situations.
Information in this chapter is provided for the airframe fuel system upstream of the highpressure
engine-driven fuel pump. For description and operation of the engine fuel system,
refer to Chapter 7—“Powerplant.”
CITATION MUSTANG OPERATING MANUAL
5-2 510OM-00
FUEL
LBS
PPH
°C
1500
1000
500
CAS
OIL PRESS LO L
CABIN ALT
T2 HTR FAIL R
W/S O’HEAT L
W/S A/I FAIL L
FUEL PRES LO R
ENG A/I COLD L
CABIN DOOR
AFT DOOR
P/S HTR L
F/W SHUTOFF R
FDR FAIL
SURFACE DE-ICE
SPD BRK EXTEND
300
700
1040 950
13
400
F/W SHUTOFF L-R
FUEL FLTR BP L-R
FUEL LVL LO L-R
FUEL PRES LO L-R
FUEL BOOST L-R
FUEL BOOST L-R
FUEL LO INOP
FUEL TRANSFER
MAIN SPAR
MAIN SPAR
FORWARD SPAR
FORWARD SPAR
REAR SPAR REAR SPAR
LP LP
TS
VENT SCOOP
OVERBOARD
VENT VALVE VENT LINE
SURGE
VENT LINE
FUEL
PROBE
FUEL
DRAIN
FUEL
FILLER
CAP
ELECTRIC
BOOST
PUMP
LEFT
SURGE
TANK
LEFT MAIN
FUEL TANK
SCAVENGE EJECTOR
PUMPS
TEMPERATURE
SENSOR
FLAPPER
VALVE
PRIMARY
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Cessna塞斯纳公务机飞行手册(27)
