Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 81

CESSNA
MODEL T210M
SECTION 5
PERFORMANCE
With an expected 10 knot headwind, the ground speed for cruise is
predicted to be:
177
-10
167 Knots
Therefore, the time required for the cruise portion of the trip is:
753 Nautical Miles_ 4 5 H
167 Knots - · ours
The fuel required for cruise is:
4.5 hours
x
91 PPH
=
410 Pounds
The total estimated fuel required is as follows:
Engine start, taxi, and takeoff
Climb
Cruise
Total fuel required
This will leave a fuel reserve of:
534
-457
??Pounds
16
31
410
457 Pounds
Once the flight is underway, ground speed checks will provide a more
accurate basis for estimating the time enroute and the corresponding fuel
required to complete the trip with ample reserve.
LANDING
A procedure similar to takeoff should be used for estimating the
landing distance at the destination airport. Figure 5-10' presents landing
distance information for the short field technique. The distances corres-
ponding to 3000 feet pressure altitude and a temperature of 30°C are as
follows:
Ground roll
Total distance to clear a 50-foot obstacle
900 Feet
1705 Feet
A correction for the effect of wind may be made based on Note 2 of the
landing chart using the same procedure as outlined for takeoff.
5-7