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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.
6. BATTERY AMPS - - - - - - - - - - - - - - - - - - - - - - - - - NOTE DECREASE
 IF BATTERY O’TEMP MESSAGE DOES NOT CLEAR OR MESSAGE
TURNS RED
7. Land as soon as possible.
PROCEDURE COMPLETED
 IF BATTERY O’TEMP MESSAGE CLEARS
7. BATTERY DISCONNECT Switch - - - - - - - - - - - - - CLOSE GUARD
8 Land as soon as practical.
PROCEDURE COMPLETED
1  BATTERY O’TEMP - AMBER (BATTERY
OVERTEMPERATURE)
1. BATTERY VOLTS/AMPS- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - NOTE
2. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - EMER
3. BATTERY VOLTS/AMPS- - - - - - - - - - - - - - - - - - - - - - NOTE DECREASE
510CLEAP-07 AB 47
K
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
Indicates that the NiCad battery temperature sensor has failed.
• IN FLIGHT
 IF BATTERY CURRENT AND/OR VOLTAGE ABNORMAL
1. BATTERY DISCONNECT Switch - - - - - - - - - - - - - - - LIFT GUARD
AND DISCONNECT
2. Land as soon as practical.
C A U T I O NCAUTION
Prolonged operation with the battery disconnect switch disconnected and the
battery switch ON will gradually deplete the battery through the battery
disconnect relay.
PROCEDURE COMPLETED
 IF BATTERY CURRENT AND VOLTAGE ARE NORMAL
1. Battery voltage and current - - - - - - - - - - - - - - - - - - - - - MONITOR
2. Land as soon as practical.
C A U T I O NCAUTION
• Monitor the battery voltage and current for abnormal indications such as
lower than normal voltage or unusually high battery current. If any
abnormal indications are noted, the battery should be disconnected.
• Avoid starter assisted inflight starts with the battery temperature monitoring
system inoperative.
PROCEDURE COMPLETED
• ON GROUND
1. Correct prior to engine start.
PROCEDURE COMPLETED
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
1  BATT TEMP FAIL
2  AFT JBOX CB L-R (AFT J-BOX CIRCUIT BREAKER)
48 AB 510CLEAP-07
L
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
This message is normally associated with the optional NiCad battery installation;
however, the wiring to support the temperature sensor is installed regardless of
which battery is installed. If this message is displayed with the standard Sealed Lead
Acid battery installed, no immediate action is required and the sensor wiring should
be inspected and repaired as soon as practical.
1  BATTERY O’TEMP - AMBER (BATTERY
OVERTEMPERATURE)
510CLEAP-07 AC 47.1
K
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
This message is normally associated with the optional NiCad battery installation;
however, the wiring to support the temperature sensor is installed regardless of
which battery is installed. If this message is displayed with the standard sealed lead
acid battery installed, no immediate action is required and the sensor wiring should
be inspected and repaired as soon as practical.
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
1  BATT TEMP FAIL
2  AFT JBOX CB L-R (AFT J-BOX CIRCUIT BREAKER)
48.1 AC 510CLEAP-07
L
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
Indicates a current limiter is open in the aft junction box. The electrical 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
　
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本文鏈接地址：Citation Mustang checklist EMERGENCY/ABNORMAL PROCEDURES(26)