曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
fuel pump on the respective engine.
When the engine start terminates, the boost
pump is deenergized and the white FUEL
BOOST L-R message disappears from the
CAS window.
During normal operation, each engine is supplied
with fuel from the primary ejector pump
in the engine feed bay of each tank. The electric
boost pump (when energized automatically
or by pilot command) may augment the
operation of the ejector pump.
CITATION MUSTANG OPERATING MANUAL
510OM-00 5-9
Figure 5-12. ENGINE FIRE and BOTTLE
ARMED Lights
Fuel Transfer System Operation
Using the fuel transfer system, fuel is transferred
from the wing tank engine feed bay to
the opposite wing tank engine feed bay. The
arrow on the FUEL TRANSFER selector
points to the wing tank where transfer fuel is
directed.
Rotating the FUEL TRANSFER selector knob
from the OFF position to the R TANK position:
1. Energizes the left tank electric boost
pump. This displays the white FUEL
BOOST L message if the boost pump
switch is in the ON or NORM position. (If
the boost pump is set to OFF, there is no
flow and no FUEL BOOST L message.)
2. Energizes the fuel transfer valve open.
The white FUEL TRANSFER message
is displayed. The left tank boost pump
pressure supplies fuel from the left wing
tank engine feed bay through the open
transfer valve and into the right wing tank
engine feed bay.
Check that the FUEL BOOST L-R message indicates
only the correct boost pump is energized.
If both boost pumps are energized, fuel
transfer does not occur. To deenergize the
pump in the nonselected tank, cycle its L or
R FUEL BOOST switch to OFF, then ON,
then NORM, and leave in NORM position.
To verify fuel transfer, monitor the fuel quantity
white tape pointers or the digital indicators
(see Figure 5-9). Fuel normally transfers
to the selected tank at approximately 10 ppm
(600 pph). Maximum normal fuel imbalance
is 200 pounds. Maximum emergency fuel imbalance
is 600 pounds.
To terminate fuel transfer and return the system
to normal operation, rotate the fuel transfer
selector to OFF. The electric boost pump
deenergizes (if the FUEL BOOST switch is in
the NORM position), the white FUEL TRANSFER
message disappears, and the fuel transfer
valve spring-loads closed.
If electrical power fails during fuel transfer operation,
the fuel transfer solenoid valve returns
to the closed position, preventing fuel transfer.
EMERGENCY/ABNORMAL
For specific information on emergency/abnormal
procedures, refer to the appropriate abbreviated
checklists or the FAA-approved AFM.
CITATION MUSTANG OPERATING MANUAL
5-10 510OM-00
The information normally contained in this chapter is
not applicable to this particular airplane.
INTENTIONALLY LEFT BLANK
510OM-00 7-i
CHAPTER 7
POWERPLANT
CONTENTS
Page
INTRODUCTION ................................................................................................................... 7-1
GENERAL.............................................................................................................................. 7-1
DESCRIPTION ....................................................................................................................... 7-2
Turbofan Engine Basics ................................................................................................... 7-3
COMPONENTS ...................................................................................................................... 7-4
Engine Systems and Accessories ..................................................................................... 7-4
Engine Systems ................................................................................................................ 7-6
CONTROLS AND INDICATIONS ...................................................................................... 7-11
FADEC.......................................................................................................................... 7-11
FADEC Reset Switch..................................................................................................... 7-12
Throttles ......................................................................................................................... 7-12
L and R IGNITION Switches ........................................................................................ 7-13
ENGINE START Switches ............................................................................................ 7-13
Engine SYNC Switch .................................................................................................... 7-14
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Cessna塞斯纳公务机飞行手册(32)
