Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-0
Page EE - 19
Rev: 1
Date:JAN 18
Prepared by: LA
Checked by : CLS
ENGINE FAILURE DURING TAKE-
OFF (AT SPEED ≤ V1) FLAPS 18°/ 0°
EC 5
Item
Action
CM
ABORT THE TAKE-OFF
ENGINE FAILURE DURING TAKE-OFF (AT SPEED > V1) FLAPS 18°
EC 5
Item
Action
CM
>
TCL of both engines
check TAKE OFF RATING
PM
>
FAILED ENGINE
DETERMINE
BOTH
After lift off:
>
LANDING GEAR
UP
PM
>
FAILED ENGINE PROPELLER
FEATHERING
CHECK
PM
(a) If the automatic feathering cycle has not been
accomplished:
>
MANUAL FEATHER. push-button of the
inoperative engine
PUSH
PM
>
ELU (LH + RH) circuit breakers
OFF
PM
Summary of Contents for L410 UVP-E20
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