|
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
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.35
Oct 05/06
Altitude Capture Sequence
Figure 04.10.29
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.36
Oct 05/06
Altitude Alert System
The altitude alert system provides aural and visual indications of preselected altitude capture and tracking. It also provides aural and visual indications of altitude deviations from the preselected altitude (ALTS).
The altitude alerting system processes data from the air data computers (ADCs), and is independent of the flight director or autopilot modes. Altitude alert annunciations are based on the baro-corrected altitude of the coupled side altimeter.
Capture Alert
At 1,000 feet prior to the preselected altitude, the preselected digital readout and bug flash, and an aural tone (C-chord) sounds.
Deviation Alert
If the aircraft deviates by more than 200 and/or 1,000 feet from the preselected altitude, the altitude bugs and digital readout flash yellow, and an aural tone (C-chord) is heard.
Altitude alerts can be canceled by pushing the PUSH CANCEL inset of the ALT knob, or by selecting a new preselect altitude.
Altitude alerts are inhibited if the glideslope (GS) or FMS glide path (VGP) is captured.
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.37
Oct 05/06
Altitude Alert Annunciations Figure 04.10.30
Altitude Hold Mode
Altitude hold mode (ALT) generates commands to maintain the pressure altitude at the time of selection. Altitude hold mode commands are based on the baro-corrected altitude of the coupled side barometric altimeter. When active, a green ALT annunciation appears in the active vertical field of the flight mode annunciator.
Altitude hold mode is activated by pushing the ALT button on the FCP, or by changing the preselected altitude while in altitude select track mode (ALTS active).
AUTOMATIC FLIGHT CONTROL SYSTEM Description Vol. 2 04.10.38
Oct 05/06
Altitude hold mode is inhibited whenever glideslope (GS) mode is active.
NOTE
If the ALT button on the FCP is pushed during a climb or descent, it is possible for the aircraft to temporarily overshoot the desired altitude while the FCCs compensate for the aircraft’s vertical speed at the moment of ALT mode selection.
The pilot may adjust the altitude reference by pushing the FD SYNC button and manually flying to the desired altitude. The FD will generate commands to maintain the new altitude reference upon release of the FD SYNC button.
Altitude hold mode may be cleared by:
.
Pushing the ALT button;
.
Selecting another vertical mode; or
.
Capturing an armed vertical mode.
Altitude Hold Mode Figure 04.10.31
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址：庞巴迪挑战者605公务机机组操作手册 CL605-AUTOMATIC_FLIGHT_CONTROL_SYSTEM(17)
| 
