Beechcraft Baron G58 Pilot Operating Handbook page 169

NORMAL PROCEDURES
TABLE OF CONTENTS (CONT'D)
SUBJECT
Ice Protection Systems. . . . . . . . . . . . . . . . . . . . . . . . . . 4-50
Before Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-51
Cabin Heater . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-51
Surface Deice System . . . . . . . . . . . . . . . . . . . . . . 4-51
Electrothermal Propeller Deice . . . . . . . . . . . . . . . . 4-51
Fuel Vent Heat, Stall Warning Heat, Pitot Heat,
Windshield Heat, and Ice Light . . . . . . . . . . . . . . 4-52
In Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-52
Surface Deice System . . . . . . . . . . . . . . . . . . . . . . 4-53
Electrothermal Propeller Deice . . . . . . . . . . . . . . . . 4-53
Electrothermal Heated Windshield Segment . . . . . 4-54
Pitot Heat, Stall Warning Heat,
and Fuel Vent Heat . . . . . . . . . . . . . . . . . . . . . . . 4-54
After Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-54
Simulating One-Engine Inoperative (Zero Thrust) . . . . . 4-54
Practice Demonstration of V
Engine Break-In Information. . . . . . . . . . . . . . . . . . . . . . 4-56
Noise Characteristics . . . . . . . . . . . . . . . . . . . . . . . . . 4-56
June, 2011
SECTION 4
. . . . . . . . . . . . . . . . . . 4-55
MCA
Model G58
PAGE
4-3