Electrothermal Heated Windshield Segment; Pitot Heat, Stall Warning Heat, And Fuel Vent Heat; After Landing; Simulating One-Engine Inoperative (Zero Thrust) - Beechcraft Baron G58 Pilot Operating Handbook

Section 4
Normal Procedures

ELECTROTHERMAL HEATED WINDSHIELD SEGMENT

Prior to Entering Icing Conditions:
• Windshield Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Continuous operation is permitted.
PITOT HEAT, STALL WARNING HEAT, AND FUEL VENT
HEAT
Switches should be ON prior to entering icing conditions.
Switches may be left ON during flight.

AFTER LANDING

• Fuel Vent, Stall Warning, Pitot, Propeller
and Windshield Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
SIMULATING ONE-ENGINE-INOPERATIVE
(ZERO THRUST)
Use the following power setting (only on one engine at a time)
to establish zero thrust. Use of this power setting avoids the
difficulties of restarting an engine and preserves the availability
of power to counter potential hazards.
The following procedure should be accomplished by alternat-
ing small reductions of propeller and then throttle, until the
desired setting has been reached.
1. Propeller Lever . . . . . RETARD TO FEATHER DETENT
2. Throttle . . . . . . .SET 12 in. Hg MANIFOLD PRESSURE
This setting will approximate Zero Thrust using
the recommended One-Engine-Inoperative
Climb speed.
4-54
NOTE
NOTE
Model G58
June, 2011