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ATTITUDE/HEADING
The attitude/heading reversion switch is a three-position rotary switch.
Position — 1.
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.
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
11-01-28 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.
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
11-01-29 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.
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