曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

to the TO detent. Verify the FADEC
thrust mode EICAS indicator (top of the N1%
window) displays a cyan TO for each engine.
Verify all EICAS indications are normal
and N1% rpm is at the cyan command bug for
each engine. Release the brakes and maintain
full takeoff power until reaching safe altitude.
NOTE
Takeoff thrust is limited to 5 minutes
except during emergency
situations (i.e., one engine inoperative).
Refer to the AFM.
After Takeoff—Climb
During climb, select throttles to the CLB detent.
Verify that the FADEC thrust mode
indicator displays a cyan CLB for each engine,
which indicates the FADECs are automatically
setting maximum climb thrust on each engine.
Cruise
During cruise, select throttles to CRU detent,
or as desired. If using the CRU detent, FADEC
automatically sets maximum cruise thrust;
verify that the FADEC thrust mode indicator
displays a cyan CRU for each engine.
NOTE
The throttles should be reduced to the
CRU detent or below within 10 minutes
after reaching an intermediate or
final cruise altitude. The use of CLB
during normal operations beyond 10
minutes after reaching cruise altitude
will significantly decrease engine life
and increase operator costs.
Descent, Approach, and
Landing
During descent, approach, and landing, reduce
the throttles as necessary to manage descent/
approach profile and navigate as required.
On final approach or landing, if an all-engines
go-around is desired, push both throttles full
forward to select the TO detent and maintain
takeoff power until a safe altitude is reached
and the aircraft is “cleaned up” (speedbrakes,
flaps, and landing gear retracted). Reduce
throttles to the CLB detent.
CAUTION
CAUTION
SHUTDOWN
Prior to shutdown, allow the ITT to stabilize
at a minimum value for 2 minutes. When ready
to shut down, lift the side latch (triggers) and
pull each throttle into CUT OFF, individually.
Monitor the EICAS panel during
shutdown to verify that operation of each engine
has terminated and that the ITT has
decreased accordingly.
Check the oil level 10 minutes after shutdown.
Ensure that the cowl door is secured. When the
engine, inlet, and exhaust nozzle are cool, install
the four engine covers.
EMERGENCY/ABNORMAL
For specific information on emergency/abnormal
procedures, refer to the appropriate
abbreviated checklists or the FAA-approved
AFM.
CITATION MUSTANG OPERATING MANUAL
510OM-00 7-23
CITATION MUSTANG OPERATING MANUAL
7-24 510OM-00
INTENTIONALLY LEFT BLANK
CHAPTER 8
FIRE PROTECTION
CONTENTS
Page
INTRODUCTION ................................................................................................................... 8-1
GENERAL.............................................................................................................................. 8-1
DESCRIPTION ....................................................................................................................... 8-2
Engine Fire Detection System.......................................................................................... 8-2
Engine Fire-Extinguishing System .................................................................................. 8-2
Portable Fire Extinguisher ............................................................................................... 8-2
COMPONENTS ...................................................................................................................... 8-2
Fire Detection Loop ......................................................................................................... 8-2
Pressure Sensor ................................................................................................................ 8-2
Engine Fire Bottle Assembly ........................................................................................... 8-2
Fuel Shutoff Valve and Generator Disconnect................................................................. 8-4
Portable Fire Extinguisher ............................................................................................... 8-4
CONTROLS AND INDICATIONS ........................................................................................ 8-4
ENGINE FIRE Lights...................................................................................................... 8-4
MASTER WARNING Lights .......................................................................................... 8-4
White BOTTLE ARMED Lights..................................................................................... 8-4
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Cessna塞斯納公務機飛行手冊(45)