Pipistrel VELIS Electro, Pilot Operating Handbook

Page: 53 / 244

3-17
VELIS Electro
Pilot's Operating Handbook
POH - 128 - 00 - 40 - 001
PAGE REV. 0
PAGE
SECTION 3
EMERGENCY PROCEDURES
APPROVED
EPSI570C message Annunciator
POWER LEVER COMMUNICA-
TION FAILURE (amber)
EPSI570C message Annunciator
ENGINE COMMUNICATION
FAILURE (amber)
- If the take o ff run is not initiated yet:
1 PWR CTRL circuit breaker DISENGAGE
2 Power lever CUT OFF
3 Shutdown procedure (4.12) PERFORM
4 Parking procedure (4.13) PERFORM
- If take o ff run is initiated and there is enough runway to stop the aicraft or
power/speed is not su ffi cient for lift o ff and climb:
1 PWR CTRL circuit breaker DISENGAGE
2 Power lever CUT OFF
3 Come to a complete standstill PERFORM
4 Shutdown procedure PERFORM
5 Push the aircraft o ff the runway PERFORM
6 Parking procedure (4.13) PERFORM
- If there is not enough runway available to stop, and power/speed is suf-
ficient for lift o ff and climb: perform Engine / power lever communication
failure (in flight) procedures (3.5.17 / 3.5.21).
NOTE: In the case of an engine communication failure, all parameters related
to motor and power controller, including the parameters (RPM, kW) displayed
on Kanardia instrument installed in front of the left seat, are covered with a
red cross. The values displayed represent the last valid output.
CAUTION: Contact CAMO/CAO.