3-56
PAGE
POH
-
128
-
00
-
40
-
001
PAGE REV. 0
PARTIAL POWER LOSS (at take o
ff
)
If it is not possible to stop the aircraft before the end of
the runway, lift o
ff
and:
Power available
ASSESS (at least 35 kW
for safe climb)
Airspeed
Vx (57 KIAS)
Climb over obstacles
PERFORM
Propulsion system
parameters (EPSI)
CHECK/MONITOR
Land
AS SOON AS PRACTICAL
PARTIAL POWER LOSS (in flight)
EPSI570C/annunciator
CHECK for Caution/
Warning messages
If conditions do not permit safe level flight:
Emergency landing
procedure (use partial
power as necessary)
PERFORM
If conditions permit safe level flight:
EPSI570C and
instruments
MONITOR
Land
AS SOON AS PRACTICAL
Summary of Contents for VELIS Electro
Page 9: ...SECTION 1...
Page 21: ...SECTION 2...
Page 36: ...This page is intentionally left blank...
Page 37: ...SECTION 3...
Page 40: ...This page is intentionally left blank...
Page 86: ...This page is intentionally left blank...
Page 108: ...This page is intentionally left blank...
Page 109: ...SECTION 4...
Page 126: ...This page is intentionally left blank...
Page 128: ...This page is intentionally left blank...
Page 140: ...This page is intentionally left blank...
Page 141: ...SECTION 5...
Page 167: ...SECTION 6...
Page 172: ...This page is intentionally left blank...
Page 173: ...SECTION 7...
Page 176: ...This page is intentionally left blank...
Page 209: ...SECTION 8...
Page 225: ...SECTION 9...
Page 227: ...APPENDIX 9 A1...