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庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-自动飞行控制系统(18)

时间:2011-11-02 15:11来源:蓝天飞行翻译 作者:公务机
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31.  Pitch command cross-pointer  Magenta  Vertical flight guidance command (not present if the com-mand is invalid) 
32.  Roll command cross-pointer  Magenta  Lateral flight guidance command (not present if the com-mand is invalid) 
33.  Cross-line over the annuncia-tion symbol(s)  Red  A required data source is invalid, for the active lateral outer loop (the line is drawn through the active lateral mode annunciation) 
A required data source is invalid, for the active vertical outer loop (the line is drawn through the active vertical mode annunciation) 

Volume 2 Flight Crew Operating Manual Sep 14/2005 CSP 100-6 REV 4
04-01-26 EICAS MESSAGES


The autoflight control system messages are shown on the EICAS. In the table below, the AFCS messages, inhibits and aural warnings are listed. A brief explanation of each message is provided.
MESSAGE  INHIBITS  MEANING  AURAL WARNING 
CONFIG AILERON TRIM CONFIG AUTOPILOT CONFIG FLAPS CONFIG RUDDER TRIM CONFIG SPOILERS CONFIG STAB TRIM  TO  The aircraft is on the ground and the takeoff parameters (autopilot, flaps, spoilers, and trims in any axis) are not properly config-ured for takeoff. Illumination of the respec-tive red CAS will be accompanied by the takeoff “CONFIGURATION“ voice warning  YES 
AFCS MESSAGES FAIL  Monitoring and indication of the autopilot modes may be unreliable 
AP HOLDING LWD AP HOLDING RWD AP HOLDING NOSE DOWN AP HOLDING NOSE UP  TO  The autopilot is holding control force in the direction indicated 
AP STAB TRIM FAIL  TO  The autopilot is unable to make a trim cor-rection to the horizontal stabilizer 
FD MODE CHANGE  An indirect mode change has occurred within the flight director. An example of an indirect mode change would be NAV or APPR mode changing to ROLL with a navi-gation source or frequency change 
YAW DAMPER FAIL  TO/LAND  The yaw damper has failed 
FD 1 FAIL FD 2 FAIL  TO/LAND  The respective flight director has failed accompanied by an FD flag on the PFD 

May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP 100-6
04-01-27 EICAS MESSAGES

The autoflight control system messages are shown on the EICAS. In the table below, the AFCS messages, inhibits and aural warnings are listed. A brief explanation of each message is provided.
MESSAGE  INHIBITS  MEANING  AURAL WARNING 
CONFIG AILERON TRIM CONFIG AUTOPILOT CONFIG FLAPS CONFIG RUDDER TRIM CONFIG SPOILERS CONFIG STAB TRIM  TO  The aircraft is on the ground and the takeoff parameters (autopilot, flaps, spoilers, and trims in any axis) are not properly config-ured for takeoff. Illumination of the respec-tive red CAS will be accompanied by the takeoff “CONFIGURATION“ voice warning  YES 
AFCS MESSAGES FAIL  Monitoring and indication of the autopilot modes may be unreliable 
 
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