3-35
VELIS Electro
Pilot's Operating Handbook
POH
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SECTION
3
EMERGENCY PROCEDURES
APPROVED
distance from the elected landing site and when ready for a power-out ap-
proach, switch the motor o
ff
:
2
PWR CTRL circuit breaker
DISENGAGE
3
Emergency landing procedure (3.9.1)
PERFORM
NOTE:
In the case of engine communication failure, all parameters related
to the motor and power controller, including the parameters (RPM, kW) dis-
played on the Kanardia instrument installed in front of the left seat, are cov-
ered by a red cross (see Section 9-A1 for more details). The values displayed
represent the last valid output. Engine temperatures and other parameters
will not be available and can't be monitored. Be prepared to the possibility of
engine temperature rising, if communication was lost at high power settings.
Power derating and propeller overspeed protection will remain active.
3.5.18
ENGINE COOLANT PUMP FAILURE
Engine coolant pump failure causes engine temperatures to rise immediate-
ly as power is applied.
When the system detects a engine coolant pump failure, expect the follow-
ing caution message to appear:
EPSI570C message
Annunciator
ENGINE COOLANT PUMP
FAILURE
(amber)
React as follows:
1
Power lever
CUT OFF
2
Best glide speed (flaps 0)
70 KIAS
3
Engine (power controller and motor)
temperatures
CHECK
4
Land (emergency landing)
PREPARE TO LAND
NOTE
: Avoid unnecessary power application. Residual power before final
Summary of Contents for VELIS Electro
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