Beechcraft Duchess 76 - Page 117

BEECHCRAFT
Duchess 76
Section V
Performance
The estimated landing weight is determined by subtracting
the
fuel required for the flight from the ramp weight:
Assumed ramp weight
= 3916 Ibs
Estimated fuel from DEN to AMA
= 39.8 gal (239 Ibs)
Estimated landing weight
= 3916 - 239 = 3677 Ibs
Examples have been provided on the performance graphs.
The above conditions have been used throughout. Rate of
climb was determined for the initial cruise altitude conditions.
Enter the graph for Landing Distance
- Flaps Down (DN) at
25°C. 3965 feet pressure altitude. 3677 pounds and 9.5 kts
headwind component:
Ground Roll 1050 ft
Total Distance over 50-ft Obstacle 1970 ft
Approach Speed 76 kts
Enter
the graph for Climb - Balked Landing at 25°C, 3965
feet pressure altitude and 3677 pounds:
Rate-af-Climb
61 0 ftlmin
Climb Gradient... 8.0%
January 1978
5013