Beechcraft Baron G58 Pilot Operating Handbook page 234

Section 5
Performance
Enter the Accelerate-Go graph at 15°C, 5653 ft pressure alti-
tude, 4700 lbs, and 10 knots headwind component:
Total Distance Over 50-ft Obstacle . . . . . . . . . . . . . 9400 ft
Ground Roll Distance. . . . . . . . . . . . . . . . . . . . . . . . 3760 ft
Enter the graph for Take-Off Climb Gradient - One-Engine-
Inoperative at 15°C, 5653 ft pressure altitude, and 4700 lbs:
Climb Gradient . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.6%
A 2.6% climb gradient is 26 ft of vertical height per 1000 ft of
horizontal distance.
The Take-off Climb Gradient - One-Engine-
Inoperative graph assumes zero wind con-
ditions. Climbing into a headwind will result
in higher angles of climb, and hence, better
obstacle clearance capabilities.
Calculation of horizontal distance to clear an obstacle 90 ft
above the runway surface:
Horizontal distance used to climb from 50 ft to 90 ft =
(90-50) X (1000 ÷ 26) = 1539 ft
Total Distance = 9400 + 1539 = 10,939 ft
5-10
NOTE
Model G58
July, 2014