MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
ABNORMAL PROCEDURES
The following Abnormal Procedures are listed by system rather than with respect to a particular CAS
or GARMIN message. They may be accompanied by one or more CAS or GARMIN messages and
possible aural warnings. Procedures for specific CAS and GARMIN messages are listed separately
and grouped by color.
ENGINE / FUEL
ENGINE FAILURE / PRECAUTIONARY SHUTDOWN
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
CAUTION
• If possible, the engine should remain at idle for a minimum of two minutes
prior to shutdown to allow the engine inter-turbine temperatures to stabilize
and avoid turbine blade rub.
• If the engine windmills for more than 15 minutes without a positive
indication of oil pressure, a notation is required in the engine logbook and
the engine must be inspected in accordance with the Pratt and Whitney
Engine Maintenance Manual.
• If the engine windmills for more than 15 minutes with the firewall shutoff
closed or the boost pump turned off, the engine fuel pump must be
inspected in accordance with the Pratt and Whitney Engine Maintenance
Manual.
2. GEN Switch (affected side). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. IGNITION Switch (affected side). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
4. Electrical Load . . . . . . . REDUCE as required, (300A maximum FL300 / 280A > FL300)
5. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
• IF ENGINE FIRE HAS OCCURRED
(FIRE EXTINGUISHED, SECURE ENGINE)
6. Verify ENGINE FIRE switch (affected side) is pushed (appropriate F/W SHUTOFF L-R
CAS message displayed).
7. Land as soon as practical. Refer to Abnormal Procedures, SINGLE-ENGINE
APPROACH AND LANDING.
PROCEDURE COMPLETED
(Continued Next Page)
510FM-07 AA 3-49
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
ENGINE FAILURE / PRECAUTIONARY SHUTDOWN (Continued)
• PRECAUTIONARY ENGINE SHUTDOWN (NO ENGINE FIRE)
6. Verify ENGINE FIRE switch is not depressed and firewall shutoff is open (no F/W
SHUTOFF CAS message).
7. FUEL BOOST Switch (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
8. Land as soon as practical. Refer to Abnormal Procedures, SINGLE-ENGINE
APPROACH AND LANDING.
PROCEDURE COMPLETED
INFLIGHT RESTART - ONE ENGINE
1. Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Below 20,000 FEET
Refer to Figure 3-1 for Engine Airstart Envelope
CAUTION
Do not attempt to restart an engine if it is possible that ice has formed in the
engine or engine inlet. Significant damage to the engine can occur.
2. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
NOTE
• Affected throttle must be placed in CUTOFF to reset FADEC start logic.
• The engine may be started at any time after shutdown. However, to reduce the
potential of turbine blade rub, initiate routine starts within 1 minute of engine
shutdown, or wait at least 10 minutes after shutdown.
• In order to maintain ITT below the start limit, an engine ITT 100C is
recommended prior to start initiation.
3. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
4. ENGINE ANTI-ICE (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
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