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
Vol. 2 11−10−28
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
AIR DATA SYSTEM INDICATIONS (CONT'D)
In AFCS vertical speed mode (VS), using the FCP/pitch wheel, two indications are displayed: a
reference bug on the VS scale, and a digital readout in the flight mode annunciation (FMA) field.
During FMS VNAV operations, the VS advisory pointer is a magenta open circle that indicates the
average VS required to climb or descend from the present position to the next climb (or descend)
altitude constraint. The FMS must be the active NAV source for the pointer to be displayed.
The vertical speed scale is also used to display TCAS resolution advisories (see Chapter 17,
Navigation Systems).
Vertical speed source data comes from the ADCs. Vertical acceleration from the onside IRS is
used to filter vertical speed in order to provide a smoother presentation to the pilot. The filtered
vertical speed is referred to as inertial vertical speed.
Vertical Speed Display
Figure 11−10−27
Air Data Flags
When ADC airspeed, altitude or vertical speed data is invalid, red air data flags are presented to
replace the affected system’s information. An invalid inertial vertical speed may also cause a VS
red flag to appear.
Negative Altitude Warning
A white vertically positioned NEG is displayed in the current altitude window to indicate negative
barometric altitudes.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−29
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
AIR DATA SYSTEM INDICATIONS (CONT'D)
Air Data Flags/RA Flag/Negative Altitude Indication
Figure 11−10−28
Air Data Reversionary Function
ADC Switch (Reversionary Panel)
When NORM is selected, the pilot and copilot electronic flight displays receive data from their
individual, onside air data computers (ADCs).
When 1 is selected, the pilot and copilot electronic flight displays receive data from ADC 1 only.
A yellow ADC 1 message is displayed on both L and R PFDs.
When 2 is selected, the pilot and copilot electronic flight displays receive data from ADC 2 only.
A yellow ADC 2 message is displayed on both L and R PFDs.
ADC Reversionary Annunciation
Figure 11−10−29
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−30
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ATTITUDE DISPLAY
Description
The attitude information provides pilot orientation to the aircraft’s axes of inclination with respect to
the horizon. The PFD’s pitch, roll and yaw indications are generated by the IRS computers.
Attitude information displayed on the PFD includes:
• Aircraft and wing symbols;
• Horizon line;
• Sky/ground display;
• Pitch tape and chevrons;
• Roll scale and pointer;
• Slip/skid indicator; and
• Unusual attitude display (PFD declutter).
Attitude Information Field
Aircraft and Wing Symbols
The aircraft symbol is an inverted black V-shape. It is a stationary representation of the aircraft,
and is represented by a black symbol with a white outline. Two small white rectangular wing
symbols are shown to the left and right of the aircraft symbol. The V-shaped aircraft symbol
appears when the flight director V-Bar (single cue) is selected.
The split T-shaped aircraft symbol appears when the flight director X-PTR (cross pointers split
cue) is selected.
Aircraft Symbols
Figure 11−10−30
Horizon Line
The horizon line is the ADI’s representation of the outside horizon. With zero degrees of pitch
and roll, the white horizon line touches the apex of the aircraft symbol, and passes through the
center of the aircraft wing symbol.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−31
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ATTITUDE DISPLAY (CONT'D)
Sky/Ground Display
Separated by the horizon line, this blue-and-brown image (wall to wall or coast to coast)
provides a visual representation of the actual position of the sky and ground with respect to the
aircraft.
Pitch Tape
The pitch tape is fixed on the attitude sphere and moves with the horizon line. The tape has
wide line markings every 10 degrees, medium line markings every 5 degrees and small line
markings every 2.5 degrees.
Roll Scale and Pointer
At the top of the blue raster is a roll scale and pointer. The scale range is ±60 degrees from a
wings level attitude.
The scale is marked as follows:
• Large tick marks at ±30 and ±60 degrees
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者605机组操作手册 CL605-FLIGHT_INSTRUMENTS(10)
