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PROCEDURE COMPLETED
BOTH ON AHRS1/2
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
510FM-07 AA 3-107
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
BOTH ON GPS1/2
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 non-selected 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
XSIDE ADC
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 1 and the copilot’s
side displays ADC 2. Refer to GARMIN G1000 Cockpit Reference Guide for additional
information.
1. Either PFD SENSOR softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
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 displays on both PFDs
4. Repeat procedure on opposite PFD.
5. PFD Displays . . . . . . . . CONFIRM “BOTH ON ADC 1 or 2" message clears on both PFDs
PROCEDURE COMPLETED
XSIDE AHRS
This message is displayed on both PFDs and indicates that both PFDs are displaying data from
the opposite side 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. Either PFD SENSOR softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
2. PFD AHRS 1/2 softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT on-side AHRS
(AHRS1 for Pilot PFD, AHRS2 for copilot PFD)
3. PFD Displays . . . . . CONFIRM “BOTH ON AHRS 1 or 2" message displays on both PFDs
4. Repeat procedure on opposite PFD.
5. PFD Displays . . . . . . . CONFIRM “BOTH ON AHRS 1 or 2" message clears on both PFDs
PROCEDURE COMPLETED
3-108.1 AK 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
YAW DAMPER INOPERATIVE
NOTE
This condition may be accompanied by a red AFCS or YAW on the PFDs.
1. AFCS Circuit Breaker (L circuit breaker panel). . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
• IF STILL INOPERATIVE
2. ALTITUDE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FL300 MAXIMUM
NOTE
• Consider alternate destination due to increased fuel consumption at lower
altitudes.
• Autopilot will be inoperative.
• The airplane is no longer RVSM capable due to the inoperative autopilot.
PROCEDURE COMPLETED
510FM-07 AA 3-109/3-110
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
HYDRAULICS/BRAKES
LANDING GEAR WILL NOT EXTEND
1. LDG GEAR CONT Circuit Breaker (L circuit breaker panel). . . . . . . . . . . . . . . . . . . CHECK
2. LDG GEAR MONITOR Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . CHECK
3. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE UP then DOWN
• IF LANDING GEAR STILL DOES NOT INDICATE DOWN/LOCKED OR
HANDLE FAILS TO MOVE FROM THE UP POSITION
4. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOVE 150 KIAS
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本文鏈接地址：Citation Mustang airplane flight manual 1(77)
