Beechcraft Baron 58 - Page 135

BEECHCRAFT Baron 58
Serial TH 773 and After
Pressure Altitude at AMA:
29.92 ~ 29.56 =.36 in. Hg
Section V
Performance
The pressure altitude at AMA is 360 feet above the field
elevation.
3605 + 360 = 3965 ft
NOTE
For
flight planning, the difference between
cruise altitude and cruise pressure altitude has
been ignored.
Maximum Allowable Take-off Weight = 5400 Ibs
Ramp
Weight = 5400 + 24 = 5424 Ibs
NOTE
Fuel for start, taxi and
take-off is normally 24
pounds.
Enter the Take-Off
Weight graph at 5650 feet pressure
altitude and 15°C.
The take-off weight to achieve a positive rate-of-c1imb at
lift-off for one engine inoperative is:
Take-off
Weight = 4850 pounds
Enter the Take-Off Distance graph at 15°C, 5650 feet pres-
sure altitude,
5400 pounds, and 9.5 knots headwind
component.
Ground Roll 1900 ft
Total Distance over 50 ft Obstacle 3090 ft
Lift-off Speed . . . . . . . . . . . . . . . . . . . . . . .. 86 kts
50 foot Speed 94 kts
October 1 976
5-5