Eclipse 500 System Manual page 195

Section 8. Engines & Fire Protection
NOTE:
FADEC does not abort engine start for abnormal oil pressure
b. ITT Rise
5. N2- 20%
a. N1 Rise
NOTE:
FADEC will not abort for lack of N1 rotation until N2 reaches 45%
b. ITT continues to rise
6. N2- 30 to 35%
a. Electric Fuel Pump- OFF
b. Starter-OFF
c. Left and Right Forward Circuit Breakers/Contactors- CLOSE
d. Right Battery Bus Contactor-
e. Generator Contactor-
f. Bus Tie Contactor- OPEN
NOTE:
Bus Tie Contactor opens after 2nd engine start
7. N2- Ground Idle (Approx 47% N2)
a. ITT Stabilizes
b. ITT Redline returns to 795°C
If the aircraft systems do not automatically configure properly for engine start an ENG
START FAIL advisory message appears. Check the state of the BUS TIE contactor
switch and verify that it is in AUTO; once completed engine restart may be attempted.
Should engine parameters exceed limits during engine start on the ground, the
FADEC automatically aborts the start and an ENG START ABORT caution message
appears. If this message appears, determine the cause of the abort and if a
mechanical failure is suspected do not attempt to restart the engine.
IMPORTANT:
The FADEC does not automatically abort engine air starts. The pilot is
responsible for monitoring engine parameters.
8.6.2 Engine Shutdown
Engine shutdown is accomplished by turning the engine start switch to OFF.
NOTE:
The engine start switch must be pushed in to move it from ON/START to OFF to
prevent inadvertent shutdown of the engine.
8.6.3 Engine Dry Motoring
If an engine start is aborted, fuel can puddle in the engine combustion chambers.
This fuel can be pumped out (without adding more fuel and without ignition) by dry
motoring the engine using the line select keys labeled L DRY MTR and R DRY MTR
Version 2.0 April 2007
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