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庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-语音和视觉警报 Aural and Visual Alerts(5)

时间:2011-11-02 15:06来源:蓝天飞行翻译 作者:公务机
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-Aural warning tones
-Voice alarms The other systems tests are as follows:
-PROBES — tests air data probes and sensors
-STALL RUD/LIM — tests the stall protection system
-ICE DET — tests the ice detection system
-FIRE DET — tests the fire detection and extinguishing (FIREX) system
-TAWS — tests the terrain avoidance warning system

Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
03-02-02 AURAL/VISUAL ALERTS ENGINE INDICATING AND CREW ALERTING SYSTEM (EICAS) (Cont)

CFO0302002_008

Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
03-02-03
AURAL/VISUAL ALERTS
ENGINE INDICATING AND CREW ALERTING SYSTEM (EICAS) (Cont)
MASTER WARNING/MASTER CAUTION SWITCHES
The master warning/master caution switches are located on the glareshield. When the DCUs generate a warning message, the master warning half of the two switches flash red. A triple chime accompanies the master warning lights. In addition, dedicated tones or voice messages may sound.
When the switch is pressed, the flashing light and the audio alerts are reset.
When the DCUs generate a caution message, the master caution half of the two switches flash amber. A single chime will accompany the master caution lights.
When the switch is pressed, the flashing light in the switches will reset.
WARNING
CAUTION
CFO0301002_001
AURAL WARNING DISABLE
Two AURAL WARNING disable switches located on the AURAL WARNING panel on the copilot aft cockpit bulkhead above the circuit breaker panel are used to disable and silence the aural warnings of a malfunctioning DCU. When DCU A is selected to OFF, DCU B provides the aural warning function. Selecting both DCU switches to OFF disables all EICAS aural warnings. These should only be used if problems with the aural warning system is encountered, or as directed by AFM procedure
AURAL  WARNING
DCU  A DCU  B

OFF
OFF
CFO0302002_005
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
03-02-04 ENGINE INDICATING AND CREW ALERTING SYSTEM (EICAS) (Cont) MFD CONTROL PANEL (MCP)

The MFD Control Panel is located on the center pedestal and the operation of each control is described below. Illustration is shown with the optional 3D map display switches (refer to Chapter 11-01-25 for further description).

L/R TOGGLE
The L/R toggle switch allows the flight crew to select control to the left or right MFDs.
CAS
Pressing the CAS switch once removes the caution, advisory, and status messages, and a white MSGS icon will display. Pressing the CAS switch a second time causes the messages to reappear.
When a new message is generated, it appears above the MSGS icon. Pressing the CAS switch hides the new message. Warning messages can not be paged out of view.
CKLST
Selecting the CKLST switch displays the electronic checklist on the right MFD.
 
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