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4 LOSS OF RADIO TUNING FUNCTIONS
5 TRANSPONDER FAILURE
510CLEAP-07 AA 67
U
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
This indicates a loss of valid air data system information to the respective system. If
either primary altitude indication is affected, the airplane is no longer RVSM capable.
• IF BOTH SIDES
1. Airspeed and Attitude - - - - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR
using standby instruments
2. Land as soon as practical.
PROCEDURE COMPLETED
• IF ONE SIDE ONLY
1. Affected PFD SENSOR softkey - - - - - - - - - - - - - - - - - - - - - - - PRESS
2. Affected PFD
ADC1/2 softkey - - - - - - - - - - - - - - - - -SELECT OPPOSITE SIDE ADC
3. PFD ADI Displays- - - - - - - - - - - - - -CONFIRM “BOTH ON ADC1 or 2"
is displayed on both PFDs
PROCEDURE COMPLETED
This message indicates a loss of pitch, roll, and/or heading information from AHRS.
Refer to GARMIN G1000 Cockpit Reference Guide for additional information.
Interference from GPS repeaters operating inside nearby hangars can cause an
intermittent loss of attitude and heading displays while the aircraft is on the ground.
This is usually accompanied by a BOTH ON GPS1/2 message. Moving the aircraft
more than 100 yards away from the source of the interference should alleviate the
condition.
• IF BOTH SIDES
1. Attitude - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR
using standby attitude gyro
2. COCKPIT FAN Knob- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
3. AIR SOURCE SELECT Knob- - - - - - - - - - - - - - - - -L, BOTH, R or OFF
(Any position other than FRESH AIR)
4. L/R WINDSHIELD ANTI-ICE Switches - - - - - - - - - - - - - - - - - - - - -OFF
5. Heading- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR
using magnetic compass
6. Land as soon as practical.
PROCEDURE COMPLETED
• IF ONE SIDE ONLY
1. Standby Attitude Gyro - - - - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR
2. Affected PFD SENSOR softkey - - - - - - - - - - - - - - - - - - - - - - - PRESS
3. Affected PFD
AHRS1/2 softkey - - - - - - - - - - - - - - SELECT OPPOSITE SIDE AHRS
4. PFD ADI Displays- - - - - - - - - - - - CONFIRM “BOTH ON AHRS1 or 2"
is displayed on both PFDs
5. Flight Director- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TRANSFER
(XFR button) to functional side
PROCEDURE COMPLETED
1 FAILED AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED
(RED “X” ON PFD AIRSPEED, ALTITUDE, AND/OR VERTICAL
SPEED INDICATORS)
2 FAILED ATTITUDE AND/OR HEADING (ATTITUDE FAIL
AND/OR RED “X” OVER HEADING DISPLAY ON PFD)
68 AA 510CLEAP-07
V
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
This indicates a loss of data from the selected NAV source. Refer to GARMIN G1000
Cockpit Reference Guide for additional information.
1. Opposite NAV Source- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -SELECT
2. PFD HSI Display - - - - - - - - - - - - - - - -CONFIRM OPPOSITE “LOC1/LOC2”
or “VOR1/VOR2” is displayed on both PFDs
PROCEDURE COMPLETED
This message is displayed when the stall warning and/or low speed awareness
functions are inoperative.
1. STALL WARN circuit breaker - - - - - - - - - - - - - - - - - - - - - - - - - - - -RESET
(R circuit breaker panel) • IF MESSAGE DOES NOT CLEAR
2. Refer to INACCURATE STALL WARNING OR ON-SPEED INDICATION;
Tab V5.
WARNING
The following systems will be inoperative:
• Stall warning horn with automatic autopilot disconnect
• Low speed awareness range on airspeed indicator
• On-speed circle
PROCEDURE COMPLETED
• IF MESSAGE CLEARS
PROCEDURE COMPLETED
Indicated by stall warning horn sounding at an inappropriate time or on-speed
indication that does not agree with expected speeds.
1. Airspeed - - - - - - - - - - - - - - - - - - - - -CROSSCHECK with other indicators
Refer to IAS MISCOMP (Airspeed Miscompare) procedure; Tab T1, if
required.
2. Aircraft Weight - - - - - - - - - - - - - - - - - - - - - - - - - - - - -VERIFY CORRECT
• IF AIRSPEED AND GROSS WEIGHT ARE CORRECT
3. STALL WARN circuit breaker- - - - - - - - - - - - - - - - - - - - - - - - - - - PULL
(R circuit breaker panel)
WARNING
The following systems will be inoperative:
• Stall warning horn with automatic autopilot disconnect
• Low speed awareness range on airspeed indicator
• On-speed circle
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Citation Mustang checklist EMERGENCY/ABNORMAL PROCEDURES(35)
