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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
6. BATTERY AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTE DECREASE
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.
(Continued Next Page)
1. BATTERY VOLTS/AMPS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTE
2. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMER
3. BATTERY VOLTS/AMPS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTE DECREASE
3-32 AB 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
TAIL CONE BLEED LEAK
(RED TAIL CONE BLD LK CAS MESSAGE)
Indicates that the tail cone temperature sensor has detected a tail cone temperature over 82ºC
(180ºF) which may indicate a bleed air leak or fire in the tailcone.
1. L and R Engine ITT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTE
2. Throttle (engine with highest ITT) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
(If unable to determine a higher ITT, start procedure
by retarding the left engine to IDLE.)
• IF CAS MESSAGE EXTINGUISHES
(INDICATES POSSIBLE BLEED LEAK FROM IDLE ENGINE)
3. Throttle . . . . . . . . . . . . MAINTAIN REDUCED POWER to keep message extinguished
4. Land as soon as practical.
PROCEDURE COMPLETED
• IF MESSAGE DOES NOT CLEAR
3. Throttle (idle engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
4. Throttle (opposite engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
IF CAS MESSAGE CLEARS
(INDICATES POSSIBLE BLEED LEAK FROM IDLE ENGINE)
5. Throttle . . . . . . . . . MAINTAIN REDUCED POWER to keep message extinguished
6. Land as soon as practical.
PROCEDURE COMPLETED
IF CAS MESSAGE STILL DOES NOT CLEAR
(INDICATES POSSIBLE TAILCONE / BAGGAGE FIRE OR MAJOR
BLEED LEAK)
5. Use minimum symmetric power as required for descent and landing. Consider the
potential of baggage or tailcone fire and subsequent need for emergency evacuation
after landing.
6. Land as soon as possible.
PROCEDURE COMPLETED
510FM-07 AA 3-31
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
This Page Intentionally Left Blank
3-32.1 AC 510FM-05
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
BATTERY OVER-TEMPERATURE
(RED BATTERY O’TEMP CAS MESSAGE) (Continued)
IF BATTERY O’TEMP MESSAGE DOES NOT CLEAR OR
MESSAGE TURNS AMBER
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
510FM-07 AB 3-33
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
This Page Intentionally Left Blank
3-34 AB 510FM-05
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
BATTERY OVER-TEMPERATURE
(RED BATTERY O’TEMP CAS MESSAGE)
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.
510FM-07 AC 3-33.1
SECTION III - OPERATING PROCEDURES MODEL 510
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Citation Mustang airplane flight manual 1(40)
