Obtaining The Best Single-Engine Climb Performance; Determining Inoperative Engine; Engine Failure During Ground Roll - Beechcraft Baron G58 Pilot Operating Handbook

Model G58
OBTAINING THE BEST SINGLE-ENGINE CLIMB
PERFORMANCE
To obtain best single-engine climb performance with one
engine inoperative, the airplane must be banked 3° to 5° into
the operative engine while maintaining a constant heading.

DETERMINING INOPERATIVE ENGINE

The following checks will help determine which engine is inop-
erative:
1. DEAD FOOT - DEAD ENGINE - The rudder pressure
required to maintain directional control will be on the side
of the operative engine.
2. THROTTLE - Partially retard the throttle for the engine
that is believed to be inoperative; there should be no
change in control pressures or in the sound of the engine
if the correct throttle has been selected. AT LOW ALTI-
TUDE AND AIRSPEED THIS CHECK MUST BE
ACCOMPLISHED WITH EXTREME CAUTION.
Do not attempt to determine the inoperative engine by means
of the tachometers or the manifold pressure displays. These
displays often indicate near normal readings.

ENGINE FAILURE DURING GROUND ROLL

1. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED
2. Braking . . . . . . . . . . . . . AS REQUIRED TO ACHIEVE
If emergency shutdown is warranted:
3. Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
4. Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
5. Alternators. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
6. Batteries . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
April, 2008
Emergency Procedures
STOPPING DISTANCE
Section 3
3-5