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1961 CESSNA 210
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$49,900.00
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| Address: Evanston, WY | |
Body Style: Single Engine Prop | |
| Engine Hours: 632 SMOH | |
Airframe Time: 3932 | |
| Propeller Hours: 632 | |
Registration: N210SR | |
| Optional Features: Equipment: Oxygen with 20,700 spec service ceiling; 260 hp 6 cyl Continental IO 470-E with 3932 TT and 632 SMOH; McCauley variable prop with 632 TT; 175 mph spec cruising with 200 mph do not exceed; greeb range 65 mph to 175 mph; 65 gallon fuel tanks capacity; spec 9 to 15 normal gph; spec absolute maximum range 1,135 miles Avionics: IFR functional, but at this price upgrades or glass panel would be affordable Exterior: White with Black Stripe and Red Stripe; new windshield Interior: Red; 4 seat; 1,009 pound spec maximum load capacity; large cargo area | |
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1961 Cessna 210A $49,900 IRF, Oxygen, 20,700 foot service ceiling, Fresh annual, 3932 TTAE, 630 SMOH, NDH 175 mph cruising speed with 200 mph do not exceed. 4 seat with 1,009 pound maximum load capacity. 260 hp Continental IO 470-E 6 cylinder. WY/ or May consider trades of Light Sport Aircraft, or aircraft or rotorcaft kit less than 50% completed up to $15,000 A good old bird. Original navcoms but at this price upgrades or glass panel is more affordable. Serial Number 21057782 N210SR formerly N9487X; Manufactured April 8, 1961; 65 175 mph normal operating range green arc; 9 15 gph fuel normal cruise power range; 1,135 miles absolute maximum range; 3931.3 Total Tach Time Airframe and Engine; 3931.3 Annual Inspection August 30, 2005Engine:260 hp Continental IO 470-E 471 cubic inches 6 cylinders 8.6:1 compression ratio; 630 TSMOH engine time since major overhaul 1,500 TBO; 630 TT prop 1,200 TBO; McCauley prop High 25.8o Low 10.8o variable pitch; 65 gallon fuel tanks capacity; 4 seat; 2,900 lb maximum weight; 1,890.6 aircraft weight; 1,009.4 maximum load capacity
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