Cessna 1985 P210R

Saturday, December 01, 2007 at 12:00 AM ET

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Key Takeaways:

The article provides detailed specifications for the 1985 Cessna P210R aircraft, which is powered by a 325 HP Continental TSIO-520CF engine.
Key performance metrics include a cruise speed of up to 210 knots (at 75% power), a maximum range of 1137 nautical miles (at 65% power), and a service ceiling of 23,000 feet.
The aircraft features a 6-seat capacity, a useful load of 1629 lbs, and a baggage capacity of 200 lbs, with a gross weight of 4100 lbs.

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cessna

Cessna 1985 P210R

Engine make/model:

Cont. TSIO-520CF

Horsepower:

325

TBO hrs.:

1600

Propeller type:

CS

Landing Gear type:

Tri./Retr.

Gross weight (lbs.):

4100

Empty weight, std. (lbs.):

2471

Useful load, std. (lbs.):

1629

Fuel (lbs.):

115

Wingspan:

33 ft. 5 in.

Overall length:

28 ft. 4 in.

Height:

9 ft. 8 in.

Seating capacity:

6

Cabin width (in.):

42

Cabin height (in.):

48

Baggage capacity (lbs.):

200

PERFORMANCE

Cruise speed (kts.):

75% power:

210

65% power:

196

Max range (w/ reserve) (nm):

75% power:

1045

65% power:

1137

Fuel consumption (gph):

75% power:

18.2

65% power:

15.8

Estimated endurance (65% power with 1-hr. reserve) (hrs):

6 hrs.

Stall speed (gear, flaps down) (knots):

55

Best rate of climb (fpm):

1150

Service ceiling (ft.):

23,000

Takeoff ground roll (ft.):

1325

Landing ground roll (ft.):

840