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4. Airspeed
a. Climb/Cruise/Descent - - - - - - - - - - - - - - -120 MINIMUM non-icing
160 MINIMUM in icing conditions
b. Approach/Landing - - - - - - - - - - - - - - - - - - - - - - - - - - VAPP/VREF
for approach and landing (per flap setting)
PROCEDURE COMPLETED
3  LOSS OF NAVIGATION DATA (LATERAL DEVIATION BAR
NOT PRESENT AND/OR GLIDESLOPE INDEX CLEARS)
4  STALL WARN FAIL (STALL WARNING FAILURE)
5  INACCURATE STALL WARNING OR ON-SPEED INDICATION
510CLEAP-07 AA 69
V
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
Indicated by overspeed warning tone sounding when airspeed is below the limit speed.
1. AIRSPEED- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CROSSCHECK
with opposite PFD
2. AIRSPEED- - - - - - - - - - - - - - - - - - - - - - - - - - - REDUCE AS REQUIRED
• IF BOTH AIRSPEEDS INDICATE BELOW VMO/MMO AND TONE STILL
SOUNDS
3. WARN LIGHTS Circuit Breaker - - - - - - - - - - - - - - - - - - - - - - - - -PULL
(R circuit breaker panel)
WARNING
When the WARN LTS circuit breaker is pulled, the following items will be
inoperative:
• Stall Warning Horn
• Gear Warning Horn
• Overspeed Warning Horn
• Master Caution and Master Warning lights
4. Land as soon as practical.
PROCEDURE COMPLETED
• IF AIRSPEEDS DO NOT AGREE
3. Refer to IAS MISCOMP (Airspeed Miscompare) procedure; Tab T1.
PROCEDURE COMPLETED
Indicated by one or both flight directors commanding attitude contrary to intended flight
path.
1. AP/TRIM DISC Button - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - PRESS
2. Attitude - - - - - - - - - - - - - - - - - - - - - - - - - - -CROSSCHECK BOTH PFDs
with the Standby Attitude indicator
3. Flight Director Modes - - - - - - - - - - - - - - - - - RESELECT AS DESIRED
4. Autopilot- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ENGAGE AS DESIRED
(if flight director commands are appropriate)
PROCEDURE COMPLETED
1  INACCURATE OVERSPEED WARNING
2  INACCURATE FLIGHT DIRECTOR DISPLAY
70 AA 510CLEAP-07
W
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
This message is displayed on both PFDs and indicates that both pilot and copilot PFDs
are displaying data from the same Air Data Computer. Normally the pilot’s side
displays ADC 1 and the copilot’s side displays ADC 2. Refer to GARMIN G1000
Cockpit Reference Guide for additional information.
1. PFD SENSOR softkey- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -PRESS
on PFD displaying data from opposite side ADC
2. PFD ADC1/2 softkey - - - - - - - - - - - - - - - - - - - - - SELECT ON-SIDE ADC
(ADC1 for Pilot PFD, ADC2 for copilot PFD)
3. PFD Displays - - - - - - - - - - - - - - - - - - CONFIRM “BOTH ON ADC 1 or 2"
message clears on both PFDs
PROCEDURE COMPLETED
This message is displayed on both PFDs and indicates that both pilot and copilot PFDs
are displaying data from the same Attitude Heading Reference System. Normally the
pilot’s side displays AHRS 1 and the copilot’s side displays AHRS 2. Refer to GARMIN
G1000 Cockpit Reference Guide for additional information.
1. PFD SENSOR softkey- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -PRESS
on PFD displaying data from opposite side AHRS
2. PFD AHRS1/2 softkey - - - - - - - - - - - - - - - - - - - SELECT ON-SIDE AHRS
(AHRS1 for Pilot PFD, AHRS2 for copilot PFD)
3 PFD Displays - - - - - - - - - - - - - - - - - CONFIRM “BOTH ON AHRS 1 or 2"
message clears on both PFDs
PROCEDURE COMPLETED
This message is displayed on both PFDs and indicates that both pilot and copilot PFDs
are displaying data from the same GPS receiver. Normally the pilot’s side displays
GPS 1 and the copilot’s side displays GPS 2 and is not pilot selectable. This may be
caused by operation outside of WAAS satellite coverage in which case the nonselected
GPS is still available in the event the active GPS fails. Refer to GARMIN
G1000 Cockpit Reference Guide for additional information.
1. GPS Status - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
a. Select MFD AUX-GPS STATUS page.
b. Select GPS1 then GPS2 softkeys and verify sufficient
satellite reception.
PROCEDURE COMPLETED
3  BOTH ON ADC 1/2
4  BOTH ON AHRS 1/2
5  BOTH GPS 1/2
510CLEAP-07 AA 71
W
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
This message is displayed on both PFDs and indicates that both PFDs are displaying
data from the opposite side Air Data Computer. Normally the pilot’s side displays ADC
　
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