Engine Fire; On The Ground; In Flight - Beechcraft Baron G58 Pilot Operating Handbook

Model G58
f. Alt Load . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
g. Nonessential Electrical Equipment. . . . . . . . . OFF AS
h. Alternator . . . . . . . . . . . . . . . . . . . . . . . . . . . BUS TIE
(ties the side with the functional alternator to the inop-
erative side)
i. Alt Load . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
j. Nonessential Electrical Equipment. . . . . . . . . .ON AS
k. Cowl Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

ENGINE FIRE

ON THE GROUND

1. Mixture Controls . . . . . . . . . . . . . . . . . . . . . . CUT OFF
2. Starter (affected engine). . . . . CONTINUE TO CRANK
3. Fuel Selector Valves . . . . . . . . . . . . . . . . . . . . . . . .OFF
4. Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
5. Alternators. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
6. Batteries . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
7. Exit airplane and move to a safe distance.

IN FLIGHT

Shut down the affected engine according to the following pro-
cedure and land immediately. Follow the applicable one-
engine-inoperative procedures in this section.
1. Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . .OFF
2. Mixture Control . . . . . . . . . . . . . . . . . . . . . . . CUT OFF
3. Propeller . . . . . . . . . . . . . . . . . . . . . . . . . FEATHERED
4. Fuel Boost Pump . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
5. Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
6. Alternator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
April, 2008
(to reduce load on operative alternator)
(maintain load limits of operative alternator)
Emergency Procedures
REQUIRED
REQUIRED
Section 3
3-7