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庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-飞行仪表(11)

时间:2011-11-15 10:09来源:蓝天飞行翻译 作者:公务机
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The indicated airspeed tape has an airspeed range from 40 to 400 kt. The tape has a scale that is marked every 5 kt and numerically marked every 20 kt.
REFERENCE SPEEDS
The takeoff reference speeds are presented on the speed scale as a V1, VR, V2, and VT. Manually set V speed values show in cyan characters; optional FMS-calculated V speed characters show in magenta.
The FGP SPEED knob is used to select and set the airspeed reference bug to the desired speed on the airspeed tape. The speed bug is located beside the selected speed with a ± 5 knot deviation indication.
When the center of the SPEED knob is depressed, the speed reference toggles between Mach and speed.
LOW/OVERSPEED/FLAP SPEED CUES
A low speed cue indicates a calculated airspeed of 1.06 VS. It appears from the lower portion of the airspeed scale and is displayed as a solid red line that changes to an expanded alternating red and black band when the aircraft is within a few knots of activating the stickshaker. The top of this cue visually represents the speed at which the stick shaker will activate.
An overspeed cue is provided to indicate the maximum operating speed. It appears in the upper portion of the airspeed scale and is displayed as a solid redline that changes to an alternating red and black band when approaching overspeed.The over-speed cue reduces to the flap operating speed limit when the flaps are extended.
TREND VECTOR
The airspeed trend vector originates from the tail of the indicated airspeed arrow. The magenta trend vector moves verti-cally in response to the aircraft acceleration or deceleration indicating the speed predicted in the next 10 seconds.
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
11-01-11 AIR DATA SYSTEM (Cont)

ALTIMETER BAROMETER KNOB
The ALTM BARO knob is rotated to increase or decrease barometric pressure setting. The barometric setting is displayed on the PFD. The standard barometric pressure setting of 29.92 inches of mercury, or 1013 hPa, is selected when the center of the BARO knob is pressed.
AIR DATA REVERSION SWITCH
The AIR DATA switch is located on the reversion panel on the center pedestal. When NORM is selected, the pilot’s and copilot’s adaptive flight displays receive data from their respective air data computer (ADC).
When ‘1’ is selected, the pilot’s and copilot’s adaptive flight displays receive data from ADC 1 only. An amber ADC 1 message is displayed on both PFDs.
When ‘2’ is selected, the pilot’s and copilot’s adaptive flight displays receive data from ADC 2 only. An amber ADC 2 message is displayed on both PFDs.
AIR DATA COMPUTERS
Each ADC senses total pressure, static pressure, and total temperature. The pressure sensors are solid-state piezoresistive type, and transform the pressure to an analog electrical signal. The analog signal is then digitized and used for all ADC calculations. Data is then passed from the ADCs to the cockpit displays, IAPS, other aircraft systems.
 
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