Beechcraft Bonanza V35B, Pilot Operating Handbook

Page: 39 / 52

Beechcraft V35B Bonanza
Pilot Operating Handbook
- 38 -
The estimated landing weight is determined by subtracting the fuel required for the trip from the ramp
weight:
Assumed ramp weight = 2660 lbs
Estimated fuel from DEN to AMA = (28.6 gal) (6Ibsjgal) = 171 lbs
Estimated landing weight = (2660 - 171) = 2489 lbs
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.
COMMENTS PERTINENT 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, Le., 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 lines. Always project to the reference
line first, and then follow the guide lines to the next known item.
3. Indicated airspeeds (IAS) were obtained by using the AIRSPEED CALIBRATION Graph.
4. The associated conditions define the specific conditions from which performance parameters have
been determined. They are not intended to be used as instructions.
5. The full amount of usable fuel is available for all approved flight conditions.