The wingspan was extended by two feet to 38 feet, 10 inches (which made it a tight fit for a 40-foot-wide hangar door) and an additional three feet was added to the horizontal stabilizer. When all-out payload and speed are important, the 210 is hard to beat. These days, major avionics upgrades include sourcing a new instrument panel to accommodate large flight displays. Performance specifications Horsepower: 1 x 260 HP Best Cruise Speed: 160 KIAS Best Range (i): 680 NM Fuel Burn @ 75%: 15.0 GPH Stall Speed: 52 KIAS Rate of climb: 1,270 FPM Ceiling: 20,300 FT Takeoff distance: 625 FT Landing distance: 725 FT Takeoff distance over 50ft obstacle: 1,210 FT Landing distance over 50ft obstacle: 1,110 FT Weights The agony of one main gear folding backward was compounded by a nosegear that broke sideways, due to the sudden side load from passengers, baggage and 90 gallons of fuel in the wing tanks. Its a great choice for a pilot that is qualified to fly complex airplanes, can comply with the requirements supplied by his insurance adjusteror can pay for the required dual instructionand has a need for a fast, capable heavy hauler. Nose gear uplock actuator clevis assembly failed, causing nose gear assembly to stay in up and locked position. The earlier versions, Cessna 210 and 210A had four seats and powered by a Continental IO-470 engine with a rated thrust of 260 horsepower. Used parts are sometimes an option, given the relatively high population of 210s. Overhauled by Gills Engines, Reno NV December, 2008 TruAtlanticformerly Atlantic Aeroand Texas Skyways offer upgrades to the TCM 550-series engine. If they decide to sell now, it will be to get out of aviation altogether. Hangar flyers throughout the world still remark on the twist and tuck gear retraction design first developed for the 210 and later extended to all high-wing retractable Cessnas. Fully understanding the system is critical, because failure to fully maintain and rig the gear systemand doorsin accordance with ALL the requirements will often result in cracks in the expensive and hard-to-find gear doors. A standard 210F/T210F held 65 gallons, but it would be hard to find a 65-gallon version since most were delivered with the optional 84-gallon tanks. Maverick Publications, 1991; Cessna Service Newsletter SNL94-6, Propeller Airplanes Serial Number Listing, Cessna Aircraft Co., 1994; FAA TCDS 3A21, Revision 49; 210 Model History by John M. Frank, The Cessna Pilots Association; Used Aircraft Guide, Vol. The OEM 1970-vintage wire-wound potentiometers in the gauge control unit are susceptible to corrosion, which can lead to erratic readings. The 210 is a remarkably adaptable airplane. The aircraft was a remarkably high-performing load-hauler with its ability to carry serious loads at reasonable speeds and for its ability to fly almost five hours with its 90 gallons of fuel. Dual instruction, export and worldwide delivery are available. The service difficulty report (SDR) database shows many gear-related problems in the 210. CPA has an excellent buyers guide on the 210. New Battery August, 2021 The performance tables show that a more reasonable 71 percent power setting (15.5 gph) at 16,000 feet will yield a true airspeed of 179 knots. Cessnas specs suggest the R model ascended at 1150 fpm200 fpm better than the N Centurions. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 866.835.5322 (866-TELL-FAA) (Interestingly, rather than mount a second door on the P-Skymaster, Cessna chose to limit the airplane to five seats.). This ridded the airframe of actuators, linkages and various switches, yielding a system with fewer failure points. Getting into the rear seats can require the agility of a gymnast, so that area is usually reserved for extra baggage. Theres one more thing to be aware of about the 210, a trait that could bring the pilot who pushes the limits of range to grief. Fuel capacities vary between model, but there should be enough to traverse a third of the U.S. without stopping, while carrying at least three adults and lots of bags. Fewer than 175 R models were built. - Aircraft data that you believe is inaccurate or have specific experiences. Back in 1960, the first 210s began life with four seats, struts and 260 hp, but the latter only lasted until 1964 when Cessna upped power to 285 and increased seating capacity to six. Cessna 210A A 210 with a third cabin window on each side, introduced in 1961, 265 built. IFR Cert Accomplished August, 2021, Continental IO520-A Still, there were major differences. Davtron Digital OAT, Press Alt, Density Alt, Voltage Display Two additional seats were an option but the two in the aft-most seats had to be pretty small due to the wheel wells in the aft fuselage. This includes good range/endurance, loading flexibility, enough cruise speed (so that inevitable headwinds wont prolong the agony that much) and the ability to mix easily with the airliner flow at larger airports. takeoff weight: 4,000 lb (1,814 kg) A combination of large control surfaces and high aerodynamic loads make for an unusually fast ability to maneuver. No popular single-engine airplane could carry a greater payload a farther distance at a faster speed than the Cessna 210 Centurion., 1972: 28 volts and the end of the engine-driven hydraulic power. Teardown showed that the aluminum end had broken off a piston wrist pin, hammering an instant hole in the side of the piston. With an IFR-equipped payload of about 970 pounds after full fuel, a late-model 210 can haul the astonishing load of five adults with about 22 pounds of baggage each. 0 The solution is to immediately change tanks and follow Cessnas recommendations on fuel pump use. This more powerful turbocharged engine is relatively easy to install in earlier T210s via an STC held by RAM Aircraft of Waco, Tex. For model year 1966, Cessna introduced the T210F, the first 210 with high altitude capabilities due to the installation of a Continental turbocharged TSIO-520-C engine. Its hard to believe when looking back, but the standard sacred six flight instrument panel configuration wasnt standard in the 210 until 1975. That could make a 210 step-up more appealing. Cessna fitted an airtight bulkhead behind the rear seats. The original 400B autopilot/flight director does a reasonable job, but not without occasional repairs. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. They jetted out from Massachusetts the following day, bought the airplane on the spot and have lived happily ever after. Steve Ells has been an A&P/IA for 44 years and is a commercial pilot with instrument and multi-engine ratings. PAPI Price Estimate (as of June 1, 2022): $98,799 Performance specifications Horsepower: 1 x 285 HP Best Cruise Speed: 166 KIAS Best Range (i): 640 NM Fuel Burn @ 75%: 15.0 GPH Stall Speed: 53 KIAS Rate of climb: 1,210 FPM Ceiling: 21,000 FT Takeoff distance: 590 FT Landing distance: 700 FT Since then, I had an engine fail at 900 hours and a second time at 400 hoursboth times due to spalled lifters that trashed the cam. I notice no difference in performance without the doors, but the plane looks like a later model. You can find the TCDS for an aircraft on our website. The T210 Centurion is an airplane with incredible capabilities for a single-engine piston, but is not for the faint of wallet. Ive flown my Centurion 3000 hours since January 2000. Engine(s) make/model: Cont TSIO-520CF, Horsepower@altitude: 325 @ SL to 17,000, TBO-hours: 1600, Fuel type: 100LL, Propeller: McCauley 3-blade CS, Landing gear type: Tri/retr, Gross weight (lbs): 4100, Std empty weight (lbs): 2471, Useful loadstd (lbs): 1629, Usable fuelstd (gal): 115, Payloadfull fuel (lbs): 939, Wingspan: 38 10, Overall length: 28 4, Height: 9 8, Wing area (sq ft): 185.5, Wing loading (lbs/sq ft: 22.1, Power loading (lbs/hp): 12.6, Wheel size: 6.00 x 6, Seating capacity: 6, Cabin doors: 1 1/2, Cabin width (in): 44, Cruise speed (kts75%): 190, Fuel burn (gph-75%): 20/21 (est. The lure of extra hp, better speed and climb, plus the benefits of a big cabin and extra payload seduced them into buying a retractable. Later, 1968 and 1969 models came with improved saddles as original equipment, but they must be inspected at 1200 hours and annually thereafter and still run the risk of eventual cracking. All rights reserved. The Cessna 210s were produced from 1957 to 1986 with a total of 9,240 aircraft built. One of our Planephd Experts will be in touch with you shortly. The second was when a gear door actuator blew apart because of incorrect assembly by an incompetent mechanic. Cessna Cessna P210 Technical Specifications Exterior Exterior Height: 9 ft 8 in Wing Span: 36 ft 9 in Length: 28 ft 2 in External Baggage: 12 cu ft Interior Cabin Volume: 104 cu ft Internal Baggage: 14 cu ft Occupancy Crew: 1 Passengers: 5 Operating Weights Max T/O Weight: 4000 Lb Max Landing Weight: 3800 Lb Operating Weight: 2606 Lb Saddle replacement was required for 1960 and 1961 models. ), Please tell us: We also note that its not unusual for line crew to think the tanks are full before they are. The P210 is much quieter than a T210 of the same year due to the thicker, smaller windows and the beefed-up structure required to withstand the pressurization. When its time to return to Earth, the P210R is, after all, a big-wing Cessna, and that means those huge flaps are available to give the airplane near-Skylane short field performance. If I had the need and the cash, Id have a Vitatoe-modified P210 to fly my Audrey to and fro in the most comfortable, high-flying Cessna single ever built. The only caveat to flying at reduced power is Continental Motors Critical Service Bulletin CSB09-11A which advised operators to keep engine rpm at 2,300 or above in cruise. This program called for the installation of a new turbocharger and other changes designed to reduce the turbocharger discharge temperature. The P (or pressurized) 210 was approved in August 1977 and introduced for model year 1978 with production ending with model year 1986. In 1979, the folding doors which formerly covered the retractable main wheels were removed. Its a testament to the 210s basic good performance that this is not the case. JPI 450 Series Fuel Flow Com The Information Manual (IM) for a 1979 T210N cites a service ceiling of 27,000 feet, an as-delivered useful load of between 1,729 and 1,785 pounds, and the ability to leap the proverbial 50-foot obstacle in 2,160 feet. The 1985 210R/T210R was upgraded again. For tips on flying any 210, we recommend Flying the Cessna 210The Secrets Unlocked by Chuck McGill (SafeFlight International). The six-seat retractable single is a market niche to which many prospective owners aspire. Minimum runway required to clear a 50-foot obstacle is a little over 2000 feet, which is close to the figure given for the A36 Bonanza, but longer by several hundred feet than those posted by the other Bonanzas and Pipers PA-32R. Cessnas project engineer on the P-210 program, Phillip Hedrick, had his work cut out for him in attempting to sandwich a larger capacity turbo under the bonnet of the 210. At the same time the MTOW for the turbocharged T210N jumped to 4,000 pound. Unfortunately theres still a tendencey for some shops to repair landing gear system faults by replacing expensive major components, when the problem is usually just a stuck or failed sequencing switch, solenoid or a broken wire. STEC 55 Approach Coupled Autopilot Search 1000's of Aircraft listings updated daily from 100's of dealers & private sellers. Cessna 210B The full cantilever, laminar flow wing came along in 1967, and power was bumped up again in 1970 to 300 hp. ( - Send us pictures of your plane. The Cessna Pilots Association is a great asset for Cessna owners. It normally burns a quart of oil every five hours. So which model do you buy? Since the Cabots now do much of their flying in the Mountain West, a blower out front seemed a good idea. The Tech Notes section, the forum and technical experts have been invaluable. It is our mission to be the go to leaders in the aviation industry. He can be contacted via email at flybillcox@aol.com. Ninety gallons of fuel was standard tankage on 210G through -N models. Engine: Continental Motors IO-520-A 285 HP Piston Engine Length: 28 Feet, 4 Inches Height: 9 Feet, 9 Inches Wingspan: 36 Feet, 7 Inches Empty Weight: 1,860 Pounds Maximum Gross Weight: 3,099 Pounds Fuel Capacity: 65 Gallons Performance Maximum speed: 199 MPH Cruise speed: 191 MPH Stall speed: 60 MPH Service ceiling: 21,000 Feet Panel construction: Laser-drilled titanium: Tank capacity: 6.2 gallons (23.46 litres) Endurance: 2.5 Hours in Anti-Ice Mode . Various components get blamed for gear problems but the overall issue is sheer complexity: Theres a lot going on when the gear is cycled. Read another SDR entry: Nose landing gear failed to extend. The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear, single-engine high-wing general aviation aircraft produced from 1957 to 1986. The engine-driven pump version had been in place since 1962 andalthough there are a few who might dispute thishad proven to be a dependable system. (15.0 gallons/hr @ $5.40/gal), Misc: landing, parking, supplies,catering, etc, Typical Price: $90,045.00 This was also the first year of the integral fuel tanks in which the wing internal structure was sealed to form two 45-gallon (89 gallons usable) fuel tanks. The 210D Centurion seats up to 5 passengers plus 1 pilot. Aviation Consumers Used Airplane Guide says this about the 210/T210 airplane: Certified way back in 1959 as a 2,900-pound airplane with a strut-braced wing and a redline speed of 174 knots, its evolved into a 4,100-pound 325 hp pressurized behemoth with a 200-knot redline, designed to fly above 20,000 feet in icing conditions. Youll see early 1960 and 1961 210s out there priced lower than a 182. First certified in 1959 and marketed as a 1960 model, the original 210 and 210A were 2900-pound airplanes powered by a Continental IO-470-E of 260 HP, a fuel-injected version of the 182s engine. - 5175 Airframe Total Time - 1620 Engine. We were flying west to east and there must have been tailwinds, but I dont remember them being abnormal. 118 Hours SPOH Complete and Original Log Records Many of them, too, are related to the systems general complexity. We observed that no one was injured in the gear up landingseven when the landing gear was partially extended. (847) 331-3133, 5350 Total Hours since New One unexpected result was that literally hundreds of new Cessnas were delivered totally naked of any avionics at all. A year later, the 210 got a boost in takeoff horsepower, to 300 HP, still using the tried and true IO-520-L. Today, theyre retired in Mexico, and they fly back and forth to Texas, Arizona and California on a regular basis. When Cessna elected not to return the 210 to production in 1996 after the ten-year hiatus, the primary reason was that the airplane was highly labor intensive to build, and it would have been too expensive to produce. The cruise speed at 75% power is 165 knots and the stall speed is 50 knots. Stats. When flying to maximum range, be diligent in getting the tanks topped correctly. Cessna 140: The Last of Cessnas Little Taildraggers, 177RG Cardinal: Cessnas Airplane of the 70s. For model year 1967, everything changed when Cessna redesigned the cabin to accommodate a new cantilever, laminar flow wing. 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