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3. Throttle (affected engine) . . . . . . . . . . . . . . . . . AS REQUIRED, normal operations
4. Engine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
5. Land as soon as practical.
PROCEDURE COMPLETED
• IF THE INDICATION RESPONDS AND PRESSURE GOES BELOW
170 PSI
PROCEDURE COMPLETED
510FM-07 AA 3-57
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
LOW OIL PRESSURE (AMBER POINTER AND DIGITS)
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE
• IF POINTER AND DIGITS RETURN TO GREEN
2. Throttle (affected engine) . . . . . . . . . . MAINTAIN REDUCED POWER AS REQUIRED
NOTE
• Oil pressure in the transient (amber) range is normal for a short period at ground
idle or in-flight following a power reduction from high thrust to idle.
• Operation at reduced oil pressure may result in increased oil temperature. If an oil
temperature limit is approached, a further reduction in power may be necessary.
• IF POINTER AND DIGITS TURN RED FOR MORE THAN 15 SECONDS
(ACCOMPANIED BY OIL PRESS LO L-R CAS MESSAGE)
2. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
3. Accomplish ENGINE FAILURE / PRECAUTIONARY SHUTDOWN.
4. Land as soon as practical. Refer to SINGLE-ENGINE APPROACH AND LANDING.
PROCEDURE COMPLETED
OIL TEMPERATURE HIGH
(>135°C, AMBER OIL TEMP INDICATION)
1. Throttle (affected engine) . . . . . . . REDUCE to maintain oil temperature at or below 135°C
• IF THE OIL TEMPERATURE DOES NOT DECREASE BELOW 135°C
OR OIL PRESSURE LIMIT IS REACHED
2. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
Refer to Abnormal Procedures, ENGINE FAILURE/PRECAUTIONARY SHUTDOWN.
NOTE
Engine damage may result from poor lubrication due to the high oil temperature and/
or low pressure.
PROCEDURE COMPLETED
• IF THE OIL TEMPERATURE DECREASES BELOW 135ºC AND ALL
OTHER ENGINE INDICATIONS ARE NORMAL
PROCEDURE COMPLETED
3-58 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
ENGINE INDICATION FAILURE (RED 'X' ON ENGINE DISPLAY)
1. FADEC RESET Switch . . . . . . . . . . . . . . . . . . . SELECT AFFECTED SIDE and RELEASE
2. ENGINE INTER 1 (L circuit breaker panel) and
ENGINE INTER 2 (R circuit breaker panel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
• IF ENGINE INDICATIONS REMAIN FAILED (RED ‘X’)
3. Use caution when adjusting engine thrust.
4. Land as soon as practical.
PROCEDURE COMPLETED
• IF NORMAL ENGINE INDICATIONS RETURN
PROCEDURE COMPLETED
ENG CTRL SYS L-R (ENGINE CONTROL SYSTEM FAULT)
Indicates that an input to the FADEC has failed, exceeded tolerances, or a FADEC channel is
inoperative. May also be accompanied by RED ‘X’ N1 and ITT. This message will display when
EMER power is selected due to loss of normal aircraft DC power to the FADEC.
1. FADEC RESET Switch . . . . . . . . . . . . . . . . . . . SELECT AFFECTED SIDE and RELEASE
• IF MESSAGE REMAINS DISPLAYED
2. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . MOVE LEVER SLOWLY DURING
ALL POWER CHANGES
CAUTION
The engine may be operating in a degraded mode. Depending on the exact
cause, some possible effects of this include:
• Degraded or lack of response to throttle movements including possible
surging or flameout.
• Possible inability to restart.
• Possible inability to achieve ground idle.
• Loss of automatic ITT limiting during ground or windmill starts.
• Loss of ITT indication.
3. Land as soon as practical.
PROCEDURE COMPLETED
• IF MESSAGE CLEARS
PROCEDURE COMPLETED
510FM-07 AA 3-59
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
F/W SHUTOFF L-R (FIREWALL SHUTOFF VALVES CLOSED)
Indicates that all electrical and fuel systems are shutoff to the indicated engine. Usually indicates
that the respective ENGINE FIRE switch has been activated. If this message posts when the
throttle is moved to CUTOFF, it indicates a malfunction of the normal shutdown system and the
respective side Firewall Shutoff Valve has been closed by the FADEC. Moving the respective
throttle out of CUTOFF will re-open the Firewall Shutoff Valve.
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Citation Mustang airplane flight manual 1(58)
