Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 4

PERFORMANCE-
SPECIFICATIONS
CESSNA
MODELT210M
PERFORMANCE - ·SPECIFICATIONS
SPEED:
Maximum at 17,000 Ft
Cruise, 80% Power at 20,000 Ft
Cruise, 80% Power at 10,000 Ft
CRUISE: Recommended lean mixture with fuel allowance for
engine start, taxi, takeoff, climb and 45 minutes
reserve at 45% power.
80% Power at 20,000 Ft
534 Pounds Usable Fuel
80% Power at 10,000 Ft
534 Pounds Usable Fuel
Maximum Range at 20,000 Ft
534 Pounds Usable Fuel
Maximum Range at 10,000 Ft
534 Pounds Usable Fuel
RATE OF CLIMB AT SEA LEVEL
SERVICE CEILING
TAKEOFF PERFORMANCE:
Ground Roll . . . . . .
Total Distance Over 50-Ft Obstacle
LANDING PERFORMANCE:
Ground Roll . . . . . . . . . . .
Total Distance Over 50-Ft Obstacle
ST ALL SPEED (CAS):
Flaps Up, Power Off
Flaps Down, Power Off
MAXIMUM WEIGHT:
Ramp . . . . . . . .
Takeoff and Landing .
STANDARD EMPTY WEIGHT:
Turbo Centurion . . . .
Turbo Centurion II . . .
MAXIMUM USEFUL LOAD:
Turbo Centurion . . . .
Turbo Centurion II . . .
BAGGAGE ALLOWANCE: Maximum With 4 People
WING LOADING: Pounds/ Sq Ft
POWER LOADING: Pounds/HP
FUEL CAP A CITY: Total . . . .
OIL CAPACITY . . . . . . . .
.Range
Time
.Range
Time
.Range
Time
.Range
Time
ENGINE: Teledyne Continental, Turbocharged Fuel Injection
310 BHP at 2700 RPM (5-Minute Takeoff.Rating)
285 BHP at 2600 RPM (Maximum Continuous Rating)
PROPELLER: 3-Bladed Constant Speed, Diameter
ii
. 205 KNOTS
. 198 KNOTS
. 181 KNOTS
830NM
4.4 HRS
790NM
4.5 HRS
995NM
7.1 HRS
990NM
7.4HRS
1030 FPM
28,500 FT
1150 FT
1900 FT
765 FT
1500 FT
65 KNOTS .
56KNOTS
3816 LBS
3800 LBS
2240 LBS
2306 LBS
1576 LBS
1510 LBS
240 LBS
21.7
12.3
90 GAL.
11 QTS
TSI0-520-R
BOIN.