Windshield Defogging - Beechcraft Baron G58 Pilot Operating Handbook

Serials th-2125 and after
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Section 4
Normal Procedures
Blower must be left on for a minimum of two
minutes after turning the heater off to
ensure heater does not over temp causing
the over-temperature switch to open.

WINDSHIELD DEFOGGING

To Achieve Maximum Windshield Defogging:
1. Heater Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
2. Heater Blower Switch . . . . . . . . . . . . . . . . . . . . . . . . ON
3. Cabin Heat Control . . . . . . . . . . . . . . . . . .PULL AFT TO
4. Pilot Air and Copilot Air Controls . . . . . . . . . . . . PUSH IN
5. Defrost Control . . . . . . . . . . . . . . . . . . . . . . . PULL OUT
If View Through Windshield Is Insufficient For Landing:
6. Pilot's Storm Window . . . . . . . . . . . . . . . . . . . . . . OPEN
ICE PROTECTION SYSTEMS
Airplanes are approved for flight in icing conditions only when
properly equipped and operated per the procedures herein and
the applicable Title 14 CFRs. No multiengine airplane is
approved for flight into severe icing conditions and none are
intended for indefinite flight in continuous icing conditions. The
pilot should exit icing conditions if the capacity of the ice pro-
tection system is exceeded or any of the required ice protec-
tion equipment fails in flight (also refer to the Kinds Of
Operations Equipment List in Section 2, LIMITATIONS).
4-50
NOTE
INCREASE TEMPERATURE
Model G58
June, 2011

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