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1. AIR COND Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VERIFY ON
(if required)
2. COCKPIT and
CABIN TEMP Knob - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VERIFY
appropriate setting is selected
3. COCKPIT and
CABIN FAN Knob - - - - - - - - - - - VERIFY LO, MED, or FLOOD (not OFF)
4. COCKPIT TEMP or
CABIN TEMP circuit breakers- - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
• IF COCKPIT TOO HOT OR DUCT O’HEAT L MESSAGE IS DISPLAYED
5. AIR SOURCE SELECT Knob- - - - - - - - - - - - - - - - - - - - - - - - - - - - - -R
 IF COCKPIT STILL TOO HOT OR MESSAGE IS STILL DISPLAYED
6. COCKPIT TEMP circuit breaker - - - - - - - - - - - - - - - - - - - - - -PULL
(L circuit breaker panel)
7. Control cockpit temperature with the left throttle.
PROCEDURE COMPLETED
 IF COCKPIT TEMPERATURE IS SATISFACTORY AND MESSAGE
IS CLEARED
PROCEDURE COMPLETED
• IF CABIN TOO HOT OR DUCT O’HEAT R MESSAGE IS DISPLAYED
5. AIR SOURCE SELECT Knob- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - L
 IF CABIN STILL TOO HOT OR MESSAGE IS STILL DISPLAYED
6. CABIN TEMP circuit breaker - - - - - - - - - - - - - - - - - - - - - - - -PULL
(R circuit breaker panel)
7. Control cabin temperature with the right throttle.
PROCEDURE COMPLETED
• IF CABIN TEMPERATURE IS SATISFACTORY AND MESSAGE IS
CLEARED
PROCEDURE COMPLETED
• IF COCKPIT TOO COLD
5. AIR SOURCE SELECT Knob- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - L
• IF CABIN TOO COLD
5. AIR SOURCE SELECT Knob- - - - - - - - - - - - - - - - - - - - - - - - - - - - - -R
PROCEDURE COMPLETED
• IF TEMPERATURE IS SATISFACTORY
PROCEDURE COMPLETED
1  AUTOMATIC TEMPERATURE CONTROL INOPERATIVE
36 AA 510CLEAP-07
G
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
This message is displayed when the pressurization system is operating in High
Altitude Airfield mode and the cabin altitude exceeds 10,000 feet for more than 30
minutes.
1. Oxygen Masks - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DON AND NORM
2. L and R MIC Switches - - - - - - - - - - - - - - - - - - - - - - - - - - OXYGEN MASK
3. Cabin altitude - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -NOTE
• IF CABIN ALTITUDE IS CLIMBING OR IF MESSAGE TURNS RED
5. Emergency Descent - - - - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED
(Refer to EMERGENCY DESCENT; Tab F3)
6. OXYGEN CONTROL VALVE Knob - - - - - - -DROP MASK (as required)
(make sure passengers are receiving oxygen)
7. Transponder - - - - - - - - - - - - - - - - - EMERGENCY CODE (as required)
PROCEDURE COMPLETED
• IF CABIN ALTITUDE IS STEADY
PROCEDURE COMPLETED
1. PRESS CONT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - STANDBY
2. Altitude - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -DESCEND AS ABLE
3. Crew Oxygen Masks (if altitude > 10,000 feet) - - - - - - - - -DON and NORM
4. L and R MIC Switches - - - - - - - - - - - - - - - - - - - - - - - - - - OXYGEN MASK
5. OXYGEN CONTROL VALVE - - - - - - - - - - - - - - DROP MASK (if required)
6. Refer to Abnormal Procedures, USE OF SUPPLEMENTAL OXYGEN;
Tab I1.
7. Land as soon as practical.
• IF EITHER FORWARD WINDSHIELD CRACKED/SHATTERED
8. L and/or R WINDSHIELD ANTI-ICE Switches - - - - - - - - - - - - - -OFF
9. Remain clear of or exit icing environment.
PROCEDURE COMPLETED
• IF CABIN WINDOW CRACKED/SHATTERED
PROCEDURE COMPLETED
2  CABIN ALT – AMBER (CABIN ALTITUDE)
3  COCKPIT FORWARD OR SIDE WINDSHIELD OR CABIN
WINDOW CRACKED OR SHATTERED
510CLEAP-07 AA 37
G
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
This message is displayed when the duct temperature exceeds 149°C (300°F).
• IF DUCT O’HEAT L IS DISPLAYED
1. COCKPIT TEMP Knob - - - - - - - - - - - - - - - - - - - - - SELECT COOLER
TEMPERATURE
2. COCKPIT TEMP circuit breaker - - - - - - - - - - - - - - - - - - - - - - - CHECK
(L circuit breaker panel)
 IF MESSAGE REMAINS DISPLAYED OR COCKPIT CANNOT BE
CONTROLLED TO COMFORTABLE TEMPERATURE
3. AIR SOURCE SELECT Knob - - - - - - - - - - - - - - - - - - - - - - - - - - -R
O IF MESSAGE IS STILL DISPLAYED OR COCKPIT STILL TOO
HOT
4. COCKPIT TEMP circuit breaker - - - - - - - - - - - - - - - - - - -PULL
(L circuit breaker panel)
5. Control cockpit temperature with the left throttle.
PROCEDURE COMPLETED
O IF MESSAGE CLEARS AND COCKPIT TEMPERATURE IS
　
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