Beechcraft Baron 58 - COMMENTS Perttnent to the USE of PERFORMANCE GRAPHS

BEECHCRAFT Baron 58
Serial TH 773 and After
SectionV
Performance
Enter the graph for Landing Distance - Flaps 30 degrees at
25°C,
3965 feet pressure altitude, 5039 pounds and 9.5
kts
headwind component:
Ground Roll 1450 ft
Total Distance over 50
ft Obstacle 2500 ft
Approach Speed 91 kts
Enter
the graph for Climb-Balked Landing at 25°C, 3965
feet pressure altitude and 5039 pounds:
Rate-of-Climb
640 ft/min
Climb Gradient 6.5%
COMMENTS PERTtNENT TO THE USE OF
PERFORMANCE GRAPHS
1. The example, in addition to presenting an answer for a
particular set of conditions, also presents the order in
which the graphs should normally
be used, i.e., if the
first item in the example is OAT, then enter the graph at
the known OAT.
2. The reference lines indicate where to begin following
guide tines. Always project to the reference line first,
then follow the guide lines to the next known item.
3. Indicated airspeeds (lAS) were obtained by using the
Airspeed Calibration-Normal System.
4. The associated conditions define the specific conditions
from which performance parameters have been
deter-
mined. They are not intended to be used as instructions;
however, performance values determined from charts
I
can only be achieved if specific conditions exist.
5. The full amount of usable fuel is available for all ap-
proved flight conditions.
September, 1979
5-13