Citation Mustang airplane flight manual 1(63)

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1. PRESS CONT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY NORM
• IF MESSAGE DOES NOT CLEAR
2. Cabin altitude, differential pressure, and rate indications . . . . . . . . . . . . . . . . MONITOR
3. PRESS CONT Switch. . . . . . . . . . . . . . . . . . . STANDBY (if cabin pressure not stable)
NOTE
With PRESS CONT switch in STANDBY, the pressurization will be operating in a
pneumatic backup mode. Cabin altitude should remain stable if the aircraft altitude
does not change. If the aircraft descends, the cabin altitude will increase until the
cabin altitude reaches the 14,500 feet limiter. If the aircraft climbs, the cabin altitude
will decrease until the maximum differential pressure is reached.
 IF CABIN ALTITUDE INCREASING (RED CABIN ALTITUDE IS
DISPLAYED)
4. Consider emergency descent if required. Refer to Emergency Procedures,
EMERGENCY DESCENT.
PROCEDURE COMPLETED
 IF CABIN ALTITUDE DECREASING
4. Cabin Differential Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
Refer to Abnormal Procedures, OVERPRESSURIZATION if 8.5 PSI is exceeded.
PROCEDURE COMPLETED
 IF INDICATIONS ARE STABLE
4. Pressurization Instruments . . . . . . . . . . . . . . . . . . . . . . . CONTINUE TO MONITOR
5. Land as soon as practical.
BEFORE LANDING
6. CABIN DUMP Switch . . . . . . . . . . . DUMP (if Cabin Differential Pressure not zero)
PROCEDURE COMPLETED
3-72 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
ELECTRICAL
 AFT JBOX CB L-R (AFT J-BOX CIRCUIT BREAKER)
This message is displayed when a respective START CONTROL circuit breaker in the aft junction
box is tripped.
• ON GROUND
1. Correct prior to flight. Respective engine cannot be started.
PROCEDURE COMPLETED
• IN FLIGHT
1. Respective engine cannot be restarted in flight.
PROCEDURE COMPLETED
 AFT JBOX LMT L-R (AFT J-BOX LIMITER)
Indicates a current limiter is open in the aft junction box. The bus on the side with the failed current
limiter can still receive power from its on-side generator, but cannot receive power from the battery.
Neither the left or right busses can receive power from the opposite generator.
• ON GROUND
1. Correct prior to flight.
PROCEDURE COMPLETED
• IN FLIGHT
1. Be prepared for loss of FEED BUS and SHUNT BUS and the associated busses on the
affected side in the event of a generator failure.
PROCEDURE COMPLETED
510FM-07 AA 3-73
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 BATTERY O’TEMP - AMBER
(BATTERY OVER-TEMPERATURE)
Indicates that the battery temperature is between 63°C and 71°C (145°F - 160°F). If the message
turns red, it indicates the battery temperature is above 71°C (160°F).
1. BATTERY VOLTS/AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTE
2. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMER
3. BATTERY VOLTS/AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTE DECREASE
NOTE
If battery amps decrease, and battery voltage is 1 volt less than generator voltage
within 30 seconds to 2 minutes, monitor BATTERY O’TEMP message.
• IF BATTERY VOLTS / AMPS DECREASE
4. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
 IF BATTERY O’TEMP MESSAGE DOES NOT CLEAR OR
MESSAGE TURNS RED.
5. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAVE OFF
6. Land as soon as possible.
PROCEDURE COMPLETED
 IF BATTERY O’TEMP MESSAGE CLEARS
5. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATT
PROCEDURE COMPLETED
• IF NO VOLTS/AMPS DECREASE (BATTERY RELAY STUCK)
4. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATT
5. BATTERY DISCONNECT Switch . . . . . . . . . . . . . . LIFT GUARD AND DISCONNECT
CAUTION
• Prolonged operation with the Battery Disconnect Switch disconnected and
the Battery Switch ON will gradually deplete the battery through the Battery
Disconnect Relay.
• After landing, refer to the Airplane Maintenance Manual for proper
maintenance procedures, as damage to the battery may have occurred.
　
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