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
All displays present AHRS 1 data.
Position — NORM
The displays present onside AHRS (pilot-1, copilot-2).
Position — 2.
All displays present AHRS 2 data.
AIR DATA
The air data reversion switch is a three-position rotary switch.
Position — 1.
All displays present ADC 1 data.
Position — NORM.
The displays present onside ADC data (pilot-1, copilot-2).
Position — 2.
All displays present ADC 2 data.
TUNE
The tune switch is a four-position rotary switch.
Position — COM 1 121.50
L-VHF com tuned to 121.50 MHz emergency frequency
Position — MFD ONLY
Tuning of the radios by the CDU is disabled, tuning enabled only by MFD.
Position — NORM
Tuning is normal.
Position — CDU ONLY
Tuning of the radios by the MFD is disabled. Tuning is enabled only by CDU.
FLIGHT INSTRUMENTS
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 11-01-29
STANDBY INSTRUMENT
DESCRIPTION
The self-contained standby indicator supplies the pilots with backup attitude, barometric altitude and airspeed indications.
The standby instrument receives information from the standby pitot static system.
COMPONENTS AND OPERATION
STANDBY INDICATOR
The indicator supplies the flight crew with displays of aircraft speed, attitude, slip/skid, and glideslope/localizer data as
long as 28 vdc power is available.
The localizer and glideslope data come from the VHF navigation receiver 1. The localizer and glideslope pointers and
scales are not in view until an ILS frequency is selected.
If the localizer data becomes invalid, a red LOC or GS flag is visible and the pointer, and scale are removed from sight.
ALIGNING FLAG
When the standby instrument is first energized, an ALIGNING flag is visible. From initial application of the 28vdc power,
the display requires a maximum of 90 seconds to stabilize, providing aircraft attitude is less than 5°. After aligning, the flag
is no longer visible.
STANDBY INSTRUMENT FUNCTIONS
The standby instrument is operated as follows:
- Gyro caging (CAGE)
- Baro-settings (STD)
- Dimming adjustment (BRT and DIM)
- A rotary knob (BARO) is provided to enter the barometric pressure correction.
CFO1101002_012
CAGE
STD
B
R
T
D
I
M
BARO
240
220
200
180
M. 47
1013.2 hPa
29.92 in
13000
128
40
20
00
9
1
10
10
20
ILS
12500
FLIGHT INSTRUMENTS
Volume 2 Flight Crew Operating Manual Sep 13/2004
11-01-30 CSP 100-6 REV 1
CLOCK/CHRONOMETER
DESCRIPTION
A digital electronic clock/chronometer is installed on the center of the instrument panel just below the standby instrument.
COMPONENTS AND OPERATION
FLIGHT TIME (FLT/RST)
Flight time (FLT) represents the time that the aircraft is “in air” as determined by the status of the in air/on ground discrete
input. The FLT starts counting from zero (00:00) when the on-ground/in-air input transitions from ground (on-ground) to
open (in-air). The FLT stops counting when the on-ground/in-air input transitions from open (in-air) to ground (on-ground).
The FLT resets to 00:00 by pressing the FLT RST switch for a period of 2 or more seconds.
CHRONOGRAPH (CHR)
The chronograph (CHR) begins counting upon depression of the CHR switch. The first switch actuation starts the CHR
from zero (00:00). Pressing the switch again stops the CHR timer. Pressing the switch a third time deletes the display and
resets the CHR timer.
GPS/MAN MODE
GPS
The chronometer uses external GPS time when the user has selected GPS mode. GPS mode is indicated by an illuminated
“GPS” indication on the LCD display.
MAN
The chronometer uses a highly accurate internal time base when the user has selected manual mode. Manual mode is indicated
by the absence of the “GPS” indication on the LCD display.
MODE
The mode push button provides two functions. Pressing the mode button will toggle between the UTC (zulu time),
LOC (local time) and date displays. By pressing and holding the mode button for more than two seconds, the chronometer
will enter the UTC, LOC and date mode.
02_014
ET
UTC
CHR
HH MM
DAY MONTH YR
MM SS
0 1 : 23
13 13 55
43 : 33
GPS/MAN
FLT
RST
CHR MODE
FLIGHT INSTRUMENTS
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 11-01-31
STANDBY COMPASS
DESCRIPTION
The standby compass supplies the flight crew with the magnetic heading data. This system is in constant operation and is
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Bombardier_Challenger_Global_00-Flight_Instruments(15)
