Air Start - Beechcraft Baron G58 Pilot Operating Handbook

Model G58
Closed [BRACKETS] in this section denotes Warning, Caution
and Advisory alerts which appear on the PFD and MFD.

AIR START

The pilot should determine the reason for
engine failure before attempting an airstart.
1. Alternator (inoperative engine) . . . . . . . . . . . . . . . . .OFF
2. Fuel Selector Valve. . . . . . . . . . . . . . . . . . . . . . . . . . .ON
3. Throttle . . . . . . . . . . . . . . SET (approximately 1/4 travel)
4. Mixture Control:
• FULL RICH, below 5000 ft (1/2 travel above 5000 ft)
5. Fuel Boost Pump . . . . . . . . . . . . . . . . . . . . . . . . . . LOW
6. Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
7. Propellers:
With Unfeathering Accumulators:
a. Propeller Control . . . . . . . . . . . . . . . . FORWARD OF
b. Propeller Control . . . . . . . . . . . . BACK TO DETENT
c. Starter (if necessary) . . . . ENGAGE MOMENTARILY
d. If propeller does not unfeather or engine does not
turn, proceed to Without Unfeathering Accumulators
procedure.
Without Unfeathering Accumulators:
a. Propeller Control. . . . . . . . . . . . . . . . . FORWARD OF
April, 2008
Abnormal Procedures
(feel for detent; confirm visually)
FEATHERING DETENT
(until engine obtains 600 RPM)
(to avoid overspeeding)
(to accomplish unfeathering)
FEATHERING DETENT
Section 3A
3A-3