Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-0
Page EE - 20
Rev: 1
Date:JAN 18
Prepared by: LA
Checked by : CLS
(b) If the inoperative engine propeller has not been feathered even after
above measures had been taken then:
>
PCL of the inoperative engine
FEATHER
PM
AIRSPEED
min. V2, FLAPS 18
PF
AUT. BANK CONTROL switch
OFF
PM
At height of 400 ft(120m) above RWY
check TAKE OFF RATING
PM
INCREASE THE AIRSPEED
V2, FLAPS 0 + 3 kts
PF
WING FLAPS
RETRACT (FLAPS 0)
PM
TCL of operating engine
set continuous OEI rating
PM
AIRSPEED
V2 0 up to 1,500 ft (457 m)
above runway
PM
INOPERATIVE ENGINE
CHECK PARAMETERS
PM
(a) If the engine is fully stopped
The following items are valid for inoperative engine:
TCL
IDLE
PM
FUEL STOP COCK/ EMERGENCY
THROTTLE LEVER
SHUT
PM
GENERATOR DC + AC switches
OFF
PM
OFF
ENGINE STARTING, ELU, FUEL PUMP
CIRCUIT BREAKERS
4 PM
Summary of Contents for L410 UVP-E20
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