Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 80

SECTION 5
PERFORMANCE
CESSNA
MODELT210M
normal climb using the data for 3800 pounds. The difference between the
values shown in the table for 4000 feet and 12,000 feet results in the
following:
Time
Fuel
Distance
13 Minutes
26 Pounds
25 Nautical Miles
The above values are for a standard temperature and are sufficiently
accurate for most flight planning purposes. However, a further correction
for the effect of temperature may be made as noted on the climb chart. The
approximate effect of a non-standard temperature is to increase the time,
fuel, and distance by 10% for each 8°C above standard temperature, due to
the lower rate of climb. In this case, assuming a temperature 16°C above
standard, the correction would be:
16°C
soc
x
10%
=
20% Increase
With this factor included, the fuel estimate would be calculated as follows :
Fuel to climb, standard temperature
Increase due to non-standard temperature
(26
X
20% )
Corrected fuel to climb
26
5
:IT
Pounds
Using a similar procedure for time and distance during a climb, the
following results are obtained:
Time to climb
Distance to climb
16 Minutes
30 Nautical Miles
~
The distances shown on the climb chart are for zero wind. A correction for '~
the effect of wind may be made as follows:
Distance with no wind 30
Decrease in distance due to wind
(16/60
x1Q
knot headwind)
_11
Corrected Distance to Climb 27 Nautical Miles
The resultant cruise distance is:
5-6
Total distance
Climb distance
Cruise distance
780
-27
753 Nautical Miles