The Cessna 210 Centurion
Type : Six-Seat cabin Monoplane
Origin: United States
Specifications:
Powerplants:
210L – One 225kW (300hp) Continental IO-520-L fuel injected flat six piston engine driving a three blade constant speed McCauley prop.
T210M – One 230kW (310hp) fuel injected and turbocharged TSIO-520-R, driving a constant speed three blade prop.
T210N – One 231kW (310hp)fuel injected and air-cooled turbocharged flat-six Continental Motors TSIO-520-R driving constant three blade prop.
Performance:
210L – Max speed – 324km/h (175 knots)
Max cruising speed – 317km/h (171 knots)
Long range cruising speed – 249km/h (134 knots)
Initial rate of climb – 950ft/min.
Stall speed: 58 knots (67 mph, 108 km/h) CAS, flaps down, power off
Service ceiling 17,300ft.
T210M – Max speed – 380km/h (205 knots)
Max cruising speed – 367km/h (198 knots)
Long range cruising speed – 260km/h (140 knots)
Initial rate of climb – 1030ft/min
Service ceiling – 28,500ft
Range at long range cruising speed 1455km (785nm).
T210N – Maximum speed: 204 knots (235 mph, 378 km/h) at 17,000 ft (5,200 m)
Cruise speed: 193 knots (222 mph, 358 km/h) at 20,000 ft (6,100 m)
Stall speed: 58 knots (67 mph, 108 km/h) CAS, flaps down, power off
Range: 900 nmi (1,036 mi, 1,668 km) econ cruise at 10,000 ft (3,050 m)
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Service ceiling: 27,000 ft (8,230 m)
Rate of climb: 930 ft/min (4.7 m/s)
Wing loading: 22.9 lb/ft² (111.8 kg/m²)
Power/mass: 0.078 hp/lb (0.13 kW/kg)
Weights:
210 – Empty 1015kg (2238lb), max takeoff 1725kg (3800lb).
T210M – Empty 1022kg (2250lb), max takeoff 1725kg (3800lb).
T210N – Empty 1045kg (2303lb), max takeoff 1814kg (4000lb).
Dimensions:
210 – Wing span 11.15m (36ft 9in)
Length 8.59m (28ft 2in)
Wing area 16.3m2 (175.5sq ft).
T210M – Wing span 11.21m (36ft 9in)
Length 8.59m (28ft 2in)
Height 2.87m (9ft 5in)
Wing area 16.3m2 (175.5sq ft).
T210N – Wingspan: 36 ft 9 in (11.20 m)
Height: 9 ft 8 in (2.95 m)
Wing area: 175 ft² (16.23 m²)
Additional Information for all models:
Wings:
Cantilever high wing monoplane.
Airfoil: NACA 642A215 at root, NACA 641A412 (A=0.5)
Dihedral 1o30’. Incidence 1o30’ at root, -1o30’ at tip.
All-metal structure except glass-fiber conical camber tips.
All-metal Frise-type ailerons
Fuselage:
All-metal semi-monocoque structure.
Landing Gear:
Hydraulically-retractable tricycle type with single wheel on each unit. Nose units retracts forward , main units aft and inward. Chrome-vanadium tapered steel tube main legs. Cleveland McCauley wheels with tubed tyres. Steerable nose-wheel with oleo-pneumatic shock absorber. Main wheel tyre size 9.00-6, 8-ply rating, pressure 3.79 bars (55 psi).
Nose wheel tyre size 5.00-5, 6-ply rating, pressure 3.45 bars (50 psi).
Cessna hydraulic disc brakes.
Fuel tank: Integral fuel tank in wings, max usable capacity 329 litres (87 US gallons).
Refuelling points above wing. Oil capacity 10.5 litres (2.75 US gallons)
Systems:
Integral hydraulic-electric unit for landing gear. Hydraulic system for brakes.
Electrical power supply: 28V 60A engine-driven alternator.
Oxygen system of 2.1 m3 (74 ft3)
Avionics and Equipment:
Optional avionics plus 400B IFCS, a dual loop nav antenna system, and a series encoding/alternating altimeter system. Electric clock, outside air temperatuere gauge, rate of climb indicator, sensitive altimeter, turn coordinator, cylinder head temperature gauge, recording tachometer, armrests, control locks, tinted windscreen. Omni-vision rear window, audible stall and landing gear warning systems, taxi-light, control pedestal lights, variable-intensity instrument panel lights, map lights, etc.
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External Dimensions:
Wing Span – 11.20m (36ft 9in)
Wing chord at root : 1.68m (5ft 6in)
Wing chord at tip : 1.22m (4ft 0in)
Wing aspect ratio – 7.66
Length overall – 8.59m (28ft 2in)
Height overall – 2.95m (9 ft 8in)
Tailplane span – 3.96m (13ft 0in)
Wheel track – 2.64m (8ft 8in)
Wheelbase – 1.83m (6ft 0in)
Propeller diameter – 2.03m (6ft 8in)
Passenger doors
Max height – 1.02m (3ft 4in)
Max width – 0.91m (3ft 0in)
Height to sill – 0.91m (3ft 0in)
Baggage Compartment door
Max height – 0.38m (1ft 11/4in)
Max width – 0.72m (2ft 9/2in)
Internal Dimensions:
Cabin
Length – 3.50m (11ft 6in)
Max width – 1.07m (3ft 6in)
Max height – 1.22m (4ft 0 in)
Floor area – 2.69m2 (29.0 sq.ft)
Volume – 3.96m3 (139.9 cu.ft)
Baggage space – 0.46m3 (16.25 cu.ft)
Areas:
Wings, gross – 16.25m3 (175 sq.ft)
Ailerons (total) – 1.75m2 (18.86 sq.ft)
Trailing-edge flaps – 2.74m2 (29.50 sq.ft)
Fin, incl dorsal fin – 0.95m2 (10.36 sq.ft)
Tailplane – 1.73 m2 (18.57 sq.ft)
Elevators incl tab – 1.87m2 (20.08 sq.ft)
Weights and Loading:
Empty weights
Centurion – 977kg (2153lb)
Centurion II – 1006kg (2219lb)
Turbo Centurion – 1015kg (2237lb)Turbo Centurion II – 1045kg (2303lb)
Max Takeoff and landing weight
Centurion, Centurion II – 1724kg (3800lb)
Turbo Centurion,Turbo Centurion II – 1814kg (4000lb)
Max ramp weight
Centurion, Centurion II – 1729kg (3812lb)
Turbo Centurion,Turbo Centurion II – 1822kg (4016lb)
Max wing loading:
Centurion, Centurion II – 106kg/m2 (21.7 psf)
Turbo Centurion,Turbo Centurion II – 111.8kg/m2 (22.9 psf)
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Max power loading:
Centurion, Centurion II – 7.69kg/kW (12.7 lb/hp)
Turbo Centurion,Turbo Centurion II – 7.85kg/kW (12.9 lb/hp)
Performance:
Max level speed:
Centurion, Centurion II at S/L– 175knots (325 km/h; 202mph)Turbo Centurion,Turbo Centurion II at 17000ft– 204knots (378 km/h; 235mph)
Max cruising speed:
Centurion, Centurion II 75% power at 6500ft – 168knots (311 km/h; 193mph)
Turbo Centurion,Turbo Centurion II 80% power at 20000ft– 193knots (358 km/h; 222mph) At 1000ft – 176knots (326 km/h; 203mph)
Stalling Speed, flaps up, power off:
Centurion, Centurion II – 65knots (121 km/h; 75mph) CAS
Turbo Centurion,Turbo Centurion II – 67knots (124 km/h; 77mph) CAS
Stalling Speed, flaps down, power off:
Centurion, Centurion II – 56knots (104 km/h; 64.5mph) CASTurbo Centurion,Turbo Centurion II – 58knots (108 km/h; 67mph) CAS
Max rate of climb at S/L:
Centurion, Centurion II – 290m (950ft)/min
Turbo Centurion,Turbo Centurion II – 283m (930ft)/min
Service ceiling :
Centurion, Centurion II – 5275m (17300ft)
Turbo Centurion,Turbo Centurion II – 8230m (27000ft)
Take-off run:
Centurion, Centurion II – 381m (1250ft)
Turbo Centurion,Turbo Centurion II – 396m (1300ft)
Take-off to 15m (50ft):
Centurion, Centurion II – 619m (2030ft)
Turbo Centurion,Turbo Centurion II – 658m (2160ft)
Landing from 15m (50ft): – 457m (1500ft)
Landing Run: – 233m (765ft)
Range – Centurion, Centurion II with max fuel, at recommended lean mixture with allowances for engine-start, taxi, T-O climb and 45min reserves at 45%power
Max cruising speed at 1980m (6500ft) – 765 nm (1418km; 881miles)
Econ cruising speed at 3050m (10000ft) – 1025nm (1899km; 1180miles)
Turbo Centurion,Turbo Centurion II – with max fuel, at recommended lean mixture with allowances for engine-start, taxi, T-O climb and 45min reserves at 45%power
Max cruising speed at 3050m (10000ft) –685 nm (1269km; 789miles)
Max cruising speed at 6100m (20000ft) – 715 nm (1325km; 823miles)
Econ cruising speed at 3050m (10000ft) – 900nm (1668km; 1036miles)
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Econ cruising speed at 6100m (20000ft) – 880nm (1631km; 1013miles)
