Fuel Vent Heat, Stall Warning Heat, Pitot Heat, Windshield Heat, And Ice Light; In Flight - Beechcraft Baron G58 Pilot Operating Handbook

Section 4
Normal Procedures
FUEL VENT HEAT, STALL WARNING HEAT, PITOT HEAT,
WINDSHIELD HEAT, AND ICE LIGHT
1. MFD Soft Keys . . . . . SELECT ENGINE AND SYSTEM
2. Switches . . . . . CYCLE ON AND OFF, ONE AT A TIME
3. L ALT and R ALT. . . MONITOR FOR LOAD INCREASE
Some systems only produce a slight
increase after a short time delay.

IN FLIGHT

Minimum airspeed for flight in icing condi-
tions is 130 KIAS. This applies to all phases
of flight except takeoff and landing. If air-
speed is decreasing due to ice accumula-
tion, and power or altitude changes fail to
curtail airspeed deceleration, alter flight to
exit icing conditions before speeds of less
than 130 KIAS are reached.
Flight in icing conditions may eventually
cause the cowling inlets to become partially
blocked, resulting in higher cylinder head
temperatures. If cowl flaps are required to
keep cylinder head temperatures below the
red line, the flight should be altered to leave
the icing conditions as soon as possible.
4-52
NOTE
Model G58
June, 2011