Cruise Climb - Beechcraft Baron G58 Pilot Operating Handbook

Section 5
Model G58 Performance
The results are illustrated as follows:
FLIGHT TIME, BLOCK SPEED AND FUEL
REQUIREMENT

CRUISE CLIMB

Enter the TIME, FUEL AND DISTANCE TO CRUISE CLIMB
Graph at the takeoff temperature of 15°C and trace up to 5653
ft pressure altitude. Then trace right to 5500 lbs. and then
down to obtain the time, fuel, and distance to climb from S.L to
5653 ft. Repeat the process starting with the cruise tempera-
ture of -5°C, cruise altitude of 11,500 ft, and initial cruise
weight of 5500 lbs. to obtain the time, fuel and distance to
climb from S.L. to 11,500 ft. Subtract the former values from
the latter values to obtain the time, fuel and distance to climb
from 5653 ft to 11,500 ft.
5-11
July, 2014