Beechcraft Baron G58 - Balked Landing Climb Performance; Landing; Total Fuel Required

Performance
Section 5
Model G58
5-15
Total Fuel Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . 17.4 gph
Reserve Fuel (45 minutes) (17.4 gph). . . . . . . . . . . 13.1 gal
TOTAL FUEL REQUIRED
Total Fuel Required = Calculated Fuel Usage + Reserve Fuel
Total Fuel Required
= 52.0 + 13.1 = 65.1 gal
LANDING
The estimated landing weight is determined by subtracting the
fuel required for the trip from the ramp weight:
Assumed Ramp Weight. . . . . . . . . . . . . . . . . . . . . 5524 lbs
Estimated Fuel (52.0 gal at 6 lbs/gal) . . . . . . . . . . . 312 lbs
Estimated Landing Weight (5524 - 312) . . . . . . . . 5212 lbs
NOTE
For the Landing Distance example, a 5039
lbs weight and a 9.5 kts headwind compo-
nent were assumed.
Enter the LANDING DISTANCE graph at 25°C, 3965 ft pres-
sure altitude, 5039 lbs landing weight an 9.5 kts headwind
component:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1450 ft
Total Distance over 50 ft. Obstacle . . . . . . . . . . . . . .2500 ft
Approach Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 91 kts
BALKED LANDING CLIMB PERFORMANCE
NOTE
For the Balked Landing Climb performance
example, a weight of 5166 lbs was
assumed.
July, 2014
58-590000-67A11_sec05.fm Page 15 Tuesday, July 29, 2014 8:32 AM