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PROCEDURE COMPLETED
• IF TEMPERATURE IS SATISFACTORY
PROCEDURE COMPLETED
3-66 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 CABIN ALT - AMBER (CABIN ALTITUDE)
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
NOTE
The red CABIN ALTITUDE message indicates cabin altitude is above 15,000 feet
when in the High Altitude Airfield mode or above 10,000 feet in the normal mode.
5. Emergency Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
(refer to Emergency Procedures, EMERGENCY DESCENT)
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
510FM-07 AA 3-67
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 COCKPIT FORWARD OR SIDE WINDSHIELD OR CABIN
WINDOW CRACKED OR SHATTERED
1. PRESS CONT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBY
2. Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESCEND as able
NOTE
• Descend to the lowest practical altitude consistent with fuel range requirements,
approximately 14,500 feet or lower is recommended.
• As the airplane descends, the cabin altitude will climb but will not exceed 14,500
feet.
• Either window ply is structurally capable of maintaining cabin pressure.
• Refer to Operating Limitations, CRACKED COCKPIT OR CABIN WINDOW.
• CABIN ALTITUDE CAS message will post when cabin altitude exceeds 10,000
feet.
3. Crew Oxygen Masks (if cabin 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.
7. Land as soon as practical.
PROCEDURE COMPLETED
• 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
3-68 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 DUCT O’HEAT L-R
(ENVIRONMENTAL SYSTEM AIR DUCT OVERHEAT)
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 (L circuit breaker panel) . . . . . . . . . . . . . . . . . CHECK
 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 (L circuit breaker panel) . . . . . . . . . . . . PULL
5. Control cockpit temperature with the left throttle.
PROCEDURE COMPLETED
O IF MESSAGE CLEARS AND COCKPIT TEMPERATURE IS
SATISFACTORY
PROCEDURE COMPLETED
• IF DUCT O’HEAT R IS DISPLAYED
1. CABIN TEMP Knob. . . . . . . . . . . . . . . . . . . . . . . . SELECT COOLER TEMPERATURE
2. CABIN TEMP Circuit Breaker (R circuit breaker panel) . . . . . . . . . . . . . . . . . . . CHECK
 IF MESSAGE REMAINS DISPLAYED OR CABIN CANNOT BE
CONTROLLED TO COMFORTABLE TEMPERATURE
3. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L
　
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本文鏈接地址：Citation Mustang airplane flight manual 1(61)