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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
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 AHRS1 and the copilot’s side displays AHRS2. 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
1. AFCS Circuit Breaker - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
(L circuit breaker panel)
• IF STILL INOPERATIVE
2. ALTITUDE - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -FL300 Maximum
PROCEDURE COMPLETED
1  XSIDE ADC
2  XSIDE AHRS
3  YAW DAMPER INOPERATIVE
72.1 AK 510CLEAP-07
X
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
3. Directional Control - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MAINTAIN
with nosewheel steering
4. Landing Distance:
C A U T I O NCAUTION
• The antiskid system does not function during emergency braking.
Excessive pressure on the emergency brake handle can cause both wheel
brakes to lock, resulting in the blowout of both main tires.
• Repeated application and release of the emergency brake handle may
cause premature loss of pneumatic pressure.
• When clear of the runway, stop and shut down. Do not attempt to taxi in
close proximity to buildings or other aircraft using emergency brakes.
Maintenance action is required prior to subsequest flights.
• Avoid landing with a tailwind.
PROCEDURE COMPLETED
4  HYDRAULIC WHEEL BRAKE FAILURE
1. Brake Pedals - - - - - - - - - - - - - -REMOVE FEET FROM BRAKE PEDALS
2. EMERGENCY BRAKE Handle- - - - - - - - - - - - - - - - - - - - SMOOTH PULL
AS REQUIRED AND HOLD UNTIL STOPPED
STALL WARNING - NORMAL Multiply normal Flap LAND landing distance by 1.83.
STALL WARNING - HIGH Multiply normal Flap TO/APR landing distance by 1.96.
510CLEAP-07 AA 73
X
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
1. LDG GEAR CONT Circuit Breaker - - - - - - - - - - - - - - - - - - - - - - - CHECK
(L circuit breaker panel)
2. LDG GEAR MONITOR Circuit Breaker - - - - - - - - - - - - - - - - - - - - CHECK
(L circuit breaker panel)
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
5. LDG GEAR CONT Circuit Breaker - - - - - - - - - - - - - - - - - - - - - - -PULL
(L circuit breaker panel)
6. EMERGENCY GEAR RELEASE Cover - - - - - - - - - - - - - - - - REMOVE
7. EMERGENCY GEAR RELEASE T-Handle - - - - - - - - - - - - -PULL AND
ROTATE TO LOCK
8. EMERGENCY GEAR RELEASE Knob - - - - - - - - - - - -PULL TO BLOW
DOWN (for positive lock)
9. Landing Gear - - - - - - - - - - - - - - - - - - - CHECK DOWN AND LOCKED
(3 green lights)
C A U T I O NCAUTION
• Prior to using the emergency extension system, the landing gear handle
must be down and/or the gear control circuit breaker pulled to prevent
possible energizing of the gear hydraulic system to the retract position
• Once the emergency gear extension system has been used, do not attempt
to retract the gear.
 IF LANDING GEAR HANDLE REMAINS UP
10. Land as soon as practical.
C A U T I O NCAUTION
• WIth the gear handle up, antiskid touchdown protection is lost. Caution
should be used to ensure that the brakes are not applied while touching
down.
• Once the airplane is on the ground, power brakes will function normally.
PROCEDURE COMPLETED
 IF LANDING GEAR HANDLE IS DOWN
　
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本文鏈接地址：Citation Mustang checklist EMERGENCY/ABNORMAL PROCEDURES(38)