System Emergencies - Beechcraft Baron G58 Pilot Operating Handbook

SECTION 3 - EMERGENCY PROCEDURES
ONE-ENGINE-INOPERATIVE PROCEDURES
RIGHT ENGINE FAILURE
After securing and feathering the right engine: The "Air Condi-
tioning Compressor OFF" mode on the Automatic Climate
Control should be selected by pressing the compressor switch
button until the adjacent indicator light goes out.
1. Air Conditioning Compressor Mode . . . . . . . . . . . . OFF
This procedure ensures absolute maximum
power is available for single engine opera-
tion.
ENGINE FIRE
IN FLIGHT
1. Climate Control System . . . . . . . . . . . . . . . . . . . . . OFF

SYSTEM EMERGENCIES

ELECTRICAL SMOKE OR FIRE
1. Climate Control System . . . . . . . . . . . . . . . . . . . . . OFF
SUSPECTED REFRIGERANT LEAK IN CABIN
The "Air Conditioning Compressor OFF" mode on the Auto-
matic Climate Control should be selected by pressing the com-
pressor switch button until the adjacent indicator light goes out.
1. Air Conditioning Compressor Mode . . . . . . . . . . . . OFF
SECTION 3A - ABNORMAL PROCEDURES
No Change.
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NOTE
Issued: March, 2017
FAA Approved
P/N 58-590000-0091