By continuing to use this website, you are agreeing to our Cookie Policy. Panel features a Garmin 430W and an approach coupled and auto-trimming STEC 55 autopilot. The type was known, from the up-powered 210D if 1964, as the Centurion. Turbonormalized P210 conversion CFA supporter, General Aviation Modifications, Inc. (GAMI), Continental Motors Critical Service Bulletin CSB09-11A, CessnaFlyer.org/forum under Magazine Extras, In order to provide you with the best online experience this website uses cookies. . IFR Cert Accomplished August, 2021, Continental IO520-A Cessna Cessna 210 Technical Specifications Exterior Exterior Height: 9 ft 7 in Wing Span: 36 ft 6 in Length: 28 ft 2 in Interior Cabin Height: 4 ft Cabin Width: 3 ft 8 In Cabin Volume: 104 cu ft Internal Baggage: 21 cu ft Occupancy Crew: 1 Passengers: 5 Operating Weights Max T/O Weight: 3800 Lb Max Landing Weight: 3800 Lb Operating Weight: 2389 Lb ), Please tell us: Furthermore, the Centurions have an unusually long center of gravity envelope (the longest in class) that tolerates loading extremes that would make other models in this class virtually unflyable, namely the Bonanza. They are also vulnerable to ham-fisted mechanics damaging them. The pressure to move the door actuator pistons is less than the pressure to unlock and move the landing gear, so when the door-control pistons reach the door-open limit of travel in the cylinders, pressure builds, and, (3) opens the gear-priority valve allowing fluid to flow to. 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. 2023 GlobalAir.com. Cox Airparts in Wichita can overhaul these controllers. A 210 was an obvious next choice. - Use this form or email to reach out to us: feedback@planephd.com. This, in turn, caused nose gear to retract on ground.. Centurion maintenance is not trivial, especially the landing gear. The Cessna 210D is powered by a Continental IO-520-A engine of 285 hp. Also belying its 182 roots were a strut-braced wing and seating for four. ) Laser-drilled titanium panels with 800 holes per square inch. More Info Nathan Bates Springdale, AR USA Compare SAVE Last Update: 03/25/2023 1961 CESSNA 210A $82,500 Reg# N9410X TT: 2600 Performance Specs A&P/IA owned 1961 Cessna 210A Centurion! With luck, the cracks are found during annual inspections and are fixed in any airplanes now on the market. Overhauled by Gills Engines, Reno NV December, 2008 The turbocharged version outsold the normally aspirated 210F by a 3:1 margin. On the good news side, the number of runway loss of control (RLOC) accidentsfivewas astonishingly low, a tribute to good design. This is almost always true. Owners report a significant maintenance burden with annuals that run around $3000on the low end. As mentioned earlier, the landing gear control system in 1960 and 61 210s used a poppet-valve type landing gear/flap system controller. They sold a bunch of them. Engine 1 Time: 113 SFRM. The Tech Notes section, the forum and technical experts have been . The dealer would have a radio shop install King radios in California. I have owned a Cessna 210 with three partners for 12 years, three engines, three propellers and two airframes. In 1962 for the 210C, the fuselage was widened. Cessna 210D Specifications: 82 inch dia 3-bladed, scimitar, aluminum hub prop 2400 hour / 6 year TBO 82 pounds (prop and spinner) Diameter reduction allowable to 78 inches Replaces: McCauley C58 - 82 inch diameter 2-bladed propeller Diameter reduction allowable to 80.0 inches 1200-1500 hour / 5 year TBO Oil fill requirement per AD 91-15-04 Ells also loves utility and bush-style airplanes and operations. Overhauled November 2008 by Northwest Propeller Service Puyallup, WA, Garmin GNS 430W NAV/COM/GPS with GPSS Davtron Model 902A Digital VOR We observed that no one was injured in the gear up landingseven when the landing gear was partially extended. It was also lighter and less expensive to build. Cessna T210N Turbo Centurion II Specs General characteristics Crew: One Capacity: Five passengers Length: 28 ft 2 in (8.59 m) Wingspan: 36 ft 9 in (11.20 m) Height: 9 ft 8 in (2.95 m) Wing area: 175 ft (16.23 m) Empty weight: 2,303 lb (1,045 kg) Max. If not, repetitive inspections at 1000-hour intervals are called for. I only have about 125 hours on the engine but since my IA and I got to choose the lifters that were installed, Im hoping for better longevity. Please select all the ways you would like to hear from AVIATION GROUP LTD: You can unsubscribe at any time by clicking the link in the footer of our emails. ( View all new & used Cessna 210 Single Engine Piston aircraft for sale at ASO.com. In Cessna: Wings for the World, Bill Thompson writes, In 1979 a cost-reduction program led to the elimination of the main gear doors and associated actuators and priority valves.. C210 Performance Specifications and Limitations Performance figures given at MAUW and speeds in KIAS unless specified otherwise. GlobalAir.com is your partner in connecting you with relevant information and resources. 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. In 1970, the first full six-seat variant was developed. The cruise speed at 75% power is 162 knots and the stall speed is 51 knots. Learn more about Mailchimp's privacy practices here. 117 Hours SMOH ), Pressurization doesnt take kindly to large openings in the fuselage, and for that reason, the first P-210s left door was significantly reinforced to help seal the cabin, and the beloved right door had to be excluded. 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. 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. Both -R models came with 87-gallon fuel tanks as standard and were optionally equipped at the factory for 115 gallons. The engine was upgraded to a Continental 325 hp TSIO-520-CE. In late 1959, the Cessna 210 was introduced to the aviation market. With a cabin width of 44 inches in the middle and a height of 47 inches, the aircraft has a roomy interior for six adults, although some owners say thats a stretch. Got substantial flight time in a 100-series Cessna? Annual inspections (if the engine doesnt have issues) run about $5000. Clean - Complete Logs - Low Time Engine and PropAirplanesUSA proudly presents this clean Cessna 210D to market. A year later, the 210 got a boost in takeoff horsepower, to 300 HP, still using the tried and true IO-520-L. A small paragraph says book fuel burn figures can be reduced by one gallon per hour below 70 percent power. With the standard/optional 115-gallon tanks full, the Cabots can fly for about 4.5 hours plus reserveenough for cross country trips of 800 nm. Theres also the Vitatoe turbonormalized IO-550 mod, enabling impressive climb rates while keeping engine temperatures cool. 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. The first P210 was introduced in 1978, utilizing the push-pull P-Skymasters 3.35 psi pressurization system. (Interestingly, rather than mount a second door on the P-Skymaster, Cessna chose to limit the airplane to five seats.). Accordingly, the P210s system wasnt nearly as stout as the Mirages 5.5 psi. Some notable ADs include: AD 91-22-1, which calls for replacing cracked and chafing wires in the nosegear tunnel on all 210s; AD 94-12-8, regarding calibration and labeling of the fuel system; and AD 93-13-9, concerning replacement of the air induction hose on T210s. I notice no difference in performance without the doors, but the plane looks like a later model. In 1972 the electrical system on the 210L was upgraded to 28 volts, and the landing gear extension/retraction system was changed from one powered by an engine-mounted hydraulic pump to one which the pump was powerpack-mounted and electrically powered. Cessna 210 D & E Centurion - Performance Data. Only one additional modelthe 210R, with the same IO-520-L and a 3850-pound grosswould come out before production ended as Cessna extracted itself from the piston-powered airplane business. Strutless cantilever wings appeared in 1967 with the 210G. 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. Both Precise Flight and Knots 2U offer electric-actuated speedbrakes that work well and are a good value. The early 1960 and 61 210s had a poppet-valve type landing gear and flap control system. John Frank, noted Cessna 210 expert, wrote this about the 1970 210: Cessna had finally reached the peak of the mountain after a decade of climbing and could now look down on all the competition. The first turbocharged version was introduced in 1966, and there were scores of other, minor changes made throughout the 70s. But, when shes working right, theres no airplane like a Turbo 210. F. My impression is that this modification solves any engine heating problems, thereby delivering better performance than the original powerplant installation. No Accident or Major Structural Damage History When Cessna restarted producing propeller airplanes in 1996 the offerings were limited to fixed-gear single engine airplanes. Alternator Overhauled August, 2021 The AiResearch TEO-4 turbo allowed flight as high as a theoretical 27,000 feet, though oxygen systems of the day werent rated for anything above 25,000 feet. These days, however, it seems long-term service of basic components like rod ends and other mechanical parts is exacting a toll. In 1979 the landing gear system was greatly simplified by removing the main landing gear doors and the associated hydraulics and electrical components. Cessnas specs suggest the R model ascended at 1150 fpm200 fpm better than the N Centurions. I was so disappointed that after spending close to $30,000 on a new engine the plane flew no differently than it had on the old engine. Many 210 lovers regard the P210R as the best of the type. It is equipped with improved avionics and also offered normally aspirated and turbocharged type or Turbo Centurion II. (KADS). It performed with great power and reliability right up until it seized in flight and left my co-owner and his wife gliding to a successful deadstick landing on a nearby runway, frantically hand-pumping the gear down. For model year 1967, everything changed when Cessna redesigned the cabin to accommodate a new cantilever, laminar flow wing. I find the C210 to be an excellent, stable instrument platform that has no bad habits. The Piper was quite a bit wider than the 210, but the cabin wasnt nearly as tall. Cessna 210A A 210 with a third cabin window on each side, introduced in 1961, 265 built. Big news came in 1964, with the 210D, which received not only Continental's IO-520-A, but a 1700-hour TBO and another 100-pound gross weight increase. Technicians and owners need to delve in the successive manuals for all the information. 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. 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. It was running great when we installed a factory remanufactured IO-520 in 1994. Big news came in 1964, with the 210D, which received not only Continentals IO-520-A, but a 1700-hour TBO and another 100-pounds gross weight . You could carry full fuel, six 170-pounders and about 10 pounds of baggage. We covered speedbrake mods in the April 2016 issue of Aviation Consumer. step-up aircraft. The 210 was, simply, an airframe that was adaptable to a lot of different things and it offered a lot of utility and performance at a relatively reasonable price.. Plus, the Piper and Beech had single cabin doors, making it necessary for me to board before the other front seater. The horizontal stabilizer offered a wider elevator to lend more pitch response to what had been a ponderous regime, and the wing sported three feet more span to improve climb. Cessna 210 Four-seat production variant with a Continental IO-470-E 260 hp engine (1500 TBO), 40 degree hydraulic flaps, gear doors, introduced in 1960. 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. . Typical straightforward annuals run about $5000. TKS fluid exudes from plane's leading edges. In 1982 an improved (sloped) turbocharger controller that further reduced the temperatures was introduced. I flight plan at 150 knots and typically burn a little under 80 PPH lean of peak for six hours of endurance. (847) 331-3133, 5350 Total Hours since New Before that, though, Cessna made minor improvements in 1961, bringing out the 210A, still powered by the IO-470-E with a 1500-hour TBO. I purchased N732AV, a 1976 C210L, in the fall of 1981. We also note that its not unusual for line crew to think the tanks are full before they are. 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. The Cessna 210s were produced from 1957 to 1986 with a total of 9,240 aircraft built. 873 serial numbers were issued for pressurized 210s. A turbocharged T210 and a pressurized P210 were also offered. Pitch forces are relatively heavy and although roll rate is adequate, the controls are not well harmonized when compared to, say, the 36-series Bonanzas. Flight planning or any other aircraft operations should only be done using official technical information provided Certified way back in 1959 as a 2900-pound airplane with a strut-braced wing and a redline speed of 174 knots, it ultimately evolved into a 4100-pound, 325-HP pressurized behemoth with a 200-knot redline, designed to fly above 20,000 feet in icing conditions. The 210 is a remarkably adaptable airplane. For tips on flying any 210, we recommend Flying the Cessna 210The Secrets Unlocked by Chuck McGill (SafeFlight International). Thirty-one of these improved P210s were produced in 1985, and seven in 1986 prior to the end of production. U.S. Department of Transportation Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 866.835.5322 (866-TELL-FAA) Single engine piston aircraft with retractable landing gear. Another group is the Cessna Owner Organization. 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. Single-engine. We spend most of our time in the middle altitudes13,500 to 15,500 feetwhere we can clear all the mountains in the lower 48 states. Performance Specs. Child seats in the baggage compartment were optional. fitness for any purpose is made or implied. Also of interest is an IO-550 engine upgrade, which is generally done in conjunction with a prop upgrade. Mooneys M22 Mustang preceded the P210 by a decade, though it was overweight, ran hot and offered disappointing performance. Please send us your experiences on your aircraft. - Features that would be useful to you. With the heat on full, add in some outside air. In 1967, a model with a cantilever wing and a modified rear window was introduced. In other words, reduced power settings allow 210 owners to save fuel and yet still haul a load. To view the various models currently available, please check out our Cessna aircraft for sale for descriptions and photos or . It normally burns a quart of oil every five hours. In late 2014 I was a passenger during a demonstration flight of a P210 that had been upgraded with a turbo-normalized IO-550 engine in accordance with an STC owned by Vitatoe Aviation in Circleville, Ohio. For more than five decades, active and dedicated aircraft owners and pilots have turned to AVIATION CONSUMER to answer their most important buying questions. 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 takeoff weight was increased to 1,542 kg. Search 1000's of Aircraft listings updated daily from 100's of dealers & private sellers. One pilot who went off the end of the runway and tore up his airplane said that hed come down final at 110 knotssome 30 knots fastbecause of tall trees in the approach path. Huh? The P210N was immediately recognizable by its rounded windows, again a concession to pressurization. Single engine piston aircraft with retractable landing gear. Sierra also makes STOL kits, as does Horton. Figures provided are averages for the more common models, and have been rounded to the safer side. Model year 1977 saw an engine upgrade in the T210M to a TSIO-520-R engine that had a takeoff power rating of 310 hp (2,700 rpm with a five-minute limit). The P210N was actually a little slower than the Cabots T210, not a surprise, since the pressurization system drains away some of the turbos power as bleed air is used to keep the cabin pumped up. You can also contact your nearest Flight Standards District Office , Aircraft Certification Office, or Manufacturing Inspection District Office. I found that all the answers needed to understand and maintain the 210 landing gear systems are in the Cessna service manualshowever, not all the information is in any one manual. That translates into a useful load of between 1,580 and 1,620 pounds. The semi-Fowler flaps were stretched outboard which gave way for a lower landing speed. Its not kidding. This more powerful turbocharged engine is relatively easy to install in earlier T210s via an STC held by RAM Aircraft of Waco, Tex. The turbocharged models were also retired with the 1986 T210R, by then sporting a 325-HP TSIO-520-CE with a 1600-hour TBO and a 4100-pound gross. Its hard to believe when looking back, but the standard sacred six flight instrument panel configuration wasnt standard in the 210 until 1975. Read another SDR entry: Nose landing gear failed to extend. One of our Planephd Experts will be in touch with you shortly. The affected aileron hinge is used in Cessna aircraft models 150, 152, 170, 172, 175, 180, 182, 185, 205, and 210. This change made it possible to enlarge the cabin interior space. Most were pilots who had taken off with reduced fuel to start with, including a non-certificated pilot who decided to take a friend for a night joyride. In each of those events, some component in the gear system had failed or the hydraulic fluid had leaked outin our opinion the 210 gear system should be maintained assertively and any problem fixed immediately, not deferred. The P210 was, in fact, the first pressurized single. Dual instruction, export and worldwide delivery are available. I believe this figure is still on the rich side of the peak EGT. If they decide to sell now, it will be to get out of aviation altogether. Flaps were lengthened, the ailerons were redesigned and the horizontal stabilizer widened by 10 inches. Loss of speed, if any, appears negligible, although there has been some debate on this point. The service difficulty report (SDR) database shows many gear-related problems in the 210. In 1972, the 210L version was developed. Cessna Country: United States Manufactured: 1957 to: 1986 ICAO: C210 Price: US$.044 million (1967) Performance Weights Dimensions Avionics: Engine: 1x Continental IO-520L Piston Power: 300 horsepower Max Cruise Speed: 204 knots 378 Km/h Approach Speed (Vref): 58 knots Travel range: 900 Nautical Miles 1,667 Kilometers Fuel Economy: Service Ceiling: Since its one of the heaviest airplane in its class, it has to be handled with respect, especially on landing. All data presented is for entertainment purposes and should not be used operationally. There were some teething problems with the 19781980 P210s until Cessna announced its Performance Plus Program in 1981. At 65 percent power at 16,000 feet the IM cites speeds of 170 knots at 14.3 gph. Davtron Digital OAT, Press Alt, Density Alt, Voltage Display Best Range (i): 640 NM. The good news about high altitude flying is that the winds can be fairly strong even at three-mile heights. It is said of the Centurion that if you can close the doors it will fly. STEC 55 Approach Coupled Autopilot Dual instruction, export and worldwide delivery are available. The Cessna Pilots Association is a great asset for Cessna owners. Submitter recommends every 100 hours check clevis assembly for security of cotter key in clevis assy for locking effectiveness.. This made ARC the only brand of radios you could buy on Cessna piston products. 1964 Cessna 210D Centurion PRICE REDUCED! Activate My Web Access . Used parts are sometimes an option, given the relatively high population of 210s. Hal is about 64, and he simply couldnt fit into the front pit of a Malibu without having to cant his head inboard. DIY Beginners Checklist: Preparing to Do Some Maintenance Yourself. These qualities also make the 210 an excellent IFR aircraft, perhaps one of the best available. Whatever would fit in the car would fit in the 210 and we would always be within weight and balance limits. This version is powered by a Continental IO-520-A engine with a rated thrust of 285 horsepower. Dual Push to Talk The position of the fuel caps on top of the wing, as designed, places them at the high point of the tanks. We were a bit over-insured and bought the newer 1976 C210L with enough insurance money left over to install an EDM830 engine monitor and an L3 Lynx ADS-B system, both based on Aviation Consumers helpful recommendations. Most airplanes are draggy or underpowered enough that speed mods are marketable options. (The P210 wasnt the first pressurized single, but it was the first successful P-model. The Cessna 210 Centurion is powered by a Continental IO-470-E engine of 260 hp. CPA has an excellent buyers guide on the 210. Owners tell us that real-world cruise speeds lie in the 160- to 170-knot range, with climb rates of about 750 FPM at 120 knots indicated, although many do cruise climbs of 500 FPM all the way to altitude for better speed and cooling. There is also the non-pressurized, cabin-class Piper Matrix, but its price point may not make many prospective purchasers lists. The Centurion is, at best, a truck. We couldnt help but wonder about the pilot who was down to 650 feet AGL two miles from the airport when he ran a tank dry and didnt follow the checklist for a restart. MAC 1700 2'nd NAV/COMM By the time the 1970 model 210K arrived, Cessna had added extra baggage space, two additional seats and a 3400-pound gross weight. On the bad news side were 20 fuel-related accidents. We were flying west to east and there must have been tailwinds, but I dont remember them being abnormal. In 1970, the Centurion II was introduced. Nose gear uplock actuator clevis assembly failed, causing nose gear assembly to stay in up and locked position. It was designated as the 210G. 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. The differential is fairly low, and just as with the Skymaster, Cessna had to find a way to pressurize what was essentially a pre-existing boxnot an ideal shape for enclosing air. Garmin GPS 155XL TSO IFR 2'nd GPS We noticed a definite improvement in takeoff power with the new propeller (or was it the engine? Beautiful, Well Maintained 1964 Cessna 210D. But set the power and trim correctly and its childs play. We use cookies to help you get the best experience when using our website. Over 50 ft obstacle: 1365 ft: Over 50 ft obstacle: 1355 ft: Rate Of Climb: 1000 fpm: Ceiling: 18300 ft: Related Specs: P210R pressurized; P210N II pressurized ('81 has less performance) T210R Turbo Centurion; T210N . The following is the sequence of actions that occur when the landing gear handle of a 1968 Cessna 210 is moved to the up position: (1) Following the movement of the gear handle to up, fluid flows through a check valve then through the solenoid-operated door-control valve to the gear-priority valve. Best Range: 680 NM Steve Ells has been an A&P/IA for 44 years and is a commercial pilot with instrument and multi-engine ratings. Cessna 210 Centurion - Specifications - Technical Data / Description Cessna 210 Centurion Touring / Utility Aircraft Photo : Karsten Palt The Cessna 210 Centurion is a single-engine six-seat light touring- and utility aircraft with retractable landing gear produced by the American manufacturer Cessna Aircraft. I have learned many things about the 210 in the last 12 years. I do as much maintenance as FAR 43 App A, part C allows. Serial Number 910074 By the time production ended with the 1986 model year, the turbocharged models had outsold the normally aspirated version by nearly two to one. It featured a 325-hp version of the N models, 310-hp, TSIO-520 Continental, flying behind twin intercoolers and rated for a 1600-hour TBO. The fewest and most costly versions were the T210R and P210R. Fuel-injected Continental engines such as the ones in 210s are very good candidates for operation on the lean side of peak, provided they are equipped with GAMIjectors and a modern engine monitor. The 210D Centurion seats up to 5 passengers plus 1 pilot.

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