POWER lever - IDLE.
PROP lever - Low RPM.
CONDITION lever - FUEL CUTOFF.
If conditions permit, reduce power on
the operative engine to obtain a TGT
of 700°C or less to reduce the
possibility of exceeding TGT limit.
Reduce electrical load to minimum
consistent with flight conditions.
False fuel flow indications may be
observed with the starter engaged
and the CONDITION lever in FUEL
ENG START switch - START-IGNITION.
Check IGN ON annunciator illuminated.
CONDITION lever - LOW IDLE.
ENG START switch - OFF after TOT
CONDITION lever - HIGH IDLE.
PROP lever - As required.
POWER lever - As required.
Engine cleanup - Perform if engine restart
GENERATOR switch - RESET, then ON.
Engine AUTO IGNITION - As required.
PROP SYNC switch - As required.
CABIN AIR MODE SELECT switch - As
Electrical equipment - As required.
9-11. MAXIMUM GLIDE.
In the event of failure of both engines, maximum
gliding distance is obtained by feathering both propellers
to reduce propeller drag and by maintaining the
appropriate airspeed with the gear and flaps up. Figure
9-2 or 9-3 gives the approximate gliding distances in
relation to altitude. The procedure to follow in the event
of failure of both engines is as follows:
Gear - UP.
Flaps - UP.
restarting first and second failed
feathering second engine propeller.
PROP levers - FEATHERED.
Airspeed - As required (fig. 9-2 or 9-3).
9-12. SINGLE-ENGINE DESCENT/ARRIVAL.
Perform the following procedure prior to the final
descent for landing:
CABIN CONTROLLER - Set
ICE & RAIN switches - As required.
RECOG lights - On.
Set windshield anti-ice to NORMAL or
HIGH as required well before descent
into icing conditions or into warm
moist air to aid in defogging. Turn off
windshield anti-ice when descent is
completed to lower altitudes and
when heating is no longer required.
This will preclude possible wind
Windshield anti-ice - As required.
Radio altimeter - As required.
Altimeters - Set to current altimeter
ASE - As required.
Flare/chaff dispenser safety pin - Insert.
Arrival briefing - Complete.
inoperative, maintain airspeed at a
minimum of Vyse until landing is
assured. A go-around after laps are
fully extended may not be possible.
9-13. SINGLE-ENGINE BEFORE LANDING.
PROP lever - HIGH RPM.
Flaps - As required.
Gear - DN.
Landing lights - As required.