The 210 is a remarkably adaptable airplane. Still, there were major differences. No Accident or Major Structural Damage History The new airplane had a service ceiling of 25,000 feet. Total Cost of Ownership: $21,439.81 We bought the scimitar-shaped Hartzell J3F (with spinner for $10,300), which has become the de facto standard propeller for this airframe. None of them apply to the Cessna 210. 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 0 The 210 has the capability to haul a lot and go a long way, plus the ability to get over the mountainseven without a turbo. The fewest and most costly versions were the T210R and P210R. Whatever would fit in the car would fit in the 210 and we would always be within weight and balance limits. Used parts are sometimes an option, given the relatively high population of 210s. But the peak had been reached. 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! You can find the TCDS for an aircraft on our website. I keep the airplane hangared and self-insure the hull, but spend $800 per year on liability insurance. 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 . Panel construction: Laser-drilled titanium: Tank capacity: 6.2 gallons (23.46 litres) Endurance: 2.5 Hours in Anti-Ice Mode . Cruise speeds of about 170 KTAS can be routine and equipped useful loads easily exceeding a half ton are common. MTOW was again upped to 3,300 pounds for the 210F/T210F. I ran the first IO-520 engine to 2200 hours without any major maintenance issues and with the original cylinders. The dealer would have a radio shop install King radios in California. As with any modern high-performance aircraft engine, an engine monitor and the understanding and application of proper powerplant management are the keys to long-term engine health. ( (4) pull back the down locks and (5) flow on to the gear actuating cylinders. It featured nose-mounted landing lights and a 24V electrical system. While a repetitive AD from 1976 addresses the issue, it still crops up from time to time in the SDRs. Once the gear legs are fully up. That means we averaged 168 knots. Cessna fitted an airtight bulkhead behind the rear seats. Call Steve Feldman at AirplanesUSA! Read another SDR entry: Nose landing gear failed to extend. The door-control valve is in the door-open position when the gear control valve is moved out of the neutral position. 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 finished P210N was about 180 pounds heavier than the T210N, one of the inevitable costs of pressurization. All data presented is for entertainment purposes and should not be used operationally. No retractable gear singles nor twins are in Cessnas future. Still, a six-seat retractable offers a good mix of the things pilots with a need to go places and carry more than two people often look for. For model year 1985 and 86, Cessna introduced the vastly upgraded P210R. Davtron Digital OAT, Press Alt, Density Alt, Voltage Display Engine 1 Time: 113 SFRM. If for some reason theyre missed, the saddles eventually break and the pilot finds out when one landing gear leg hangs up in the halfway position. . In other words, reduced power settings allow 210 owners to save fuel and yet still haul a load. They sold a bunch of them. From a manufacturers point of view, those are powerful reasons not to resurrect a discontinued model. First flown in January 1957, it was produced by Cessna until 1986. Both -R models came with 87-gallon fuel tanks as standard and were optionally equipped at the factory for 115 gallons. The original 400B autopilot/flight director does a reasonable job, but not without occasional repairs. Best Cruise Speed: 166 KIAS . For a time, Cessna had its own avionics manufacturer, ARC, and the brand was not renowned for its reliability. Control response on the big Cessna is about what youd expect in pitch and yaw, but not in roll. - Aircraft data that you believe is inaccurate or have specific experiences. By clicking below to subscribe, you acknowledge that your information will be transferred to Mailchimp for processing. Single engine piston aircraft with retractable landing gear. Best Cruise: 166 KIAS A very low time engine and factory new prop are complimented by a clean airframe with complete logs and capable IFR instrumentation. Some owners simply replace them whether theyre cracked or not. The trick? 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. 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. The 210s lineage extends back to the late 1950s, when tricycle landing gearmuch less a retractablesignified a newly designed airplane. It came with King radios, which were trouble-free right up to the time I replaced them with a Garmin stack with ADS-B. 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. It was also lighter and less expensive to build. Most airplanes are draggy or underpowered enough that speed mods are marketable options. 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. (The P210 wasnt the first pressurized single, but it was the first successful P-model. MTOW was upped again, this time to 3,400 pounds. Child seats in the baggage compartment were optional. That decided us in favor of the P210R.. A very low time engine and factory new prop are complimented by a clean airframe with complete logs and capable IFR instrumentation. Click HERE to choose your FREE download: 172 Owners Guide, 182 Owners Guide, or Digital Magazine. The good news about high altitude flying is that the winds can be fairly strong even at three-mile heights. (Interestingly, rather than mount a second door on the P-Skymaster, Cessna chose to limit the airplane to five seats.). Since pressurization remained at 3.35 psi, pilots and crew would have needed supplemental oxygen, as the cabin would have been above 12,500 feet. By continuing to use this website, you are agreeing to our Cookie Policy. 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. The problem is confined to fuselage station 209 and Cessna has kits to repair the problems or prevent them from happening. Max take-off weight 2900 lbs. In 1977, the 210M came out, with a 3800-pound gross weight, to be followed in 1979 by removing the gear doors for the 210N. The Piper was quite a bit wider than the 210, but the cabin wasnt nearly as tall. 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. 118 Hours SPOH Neither the original Skymaster nor the Cessna 210 was ever intended to be inflatable. 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. During a strong climb to 23,000 feet, no CHT topped 360 deg. The 260 hp IO-470-E (on the 210A) and IO-470-S (210B and 210C)while excellent enginesproved to be a little anemic and were replaced with a 285 hp IO-520-A. All rights reserved. New Right Fuel Cell 2016 This ridded the airframe of actuators, linkages and various switches, yielding a system with fewer failure points. 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. Some are as fast as many twins, can carry sizable payloads, can accommodate plenty of modern avionics and generally are straightforward to fly. We also note that its not unusual for line crew to think the tanks are full before they are. The dual pumps became standard with 1983 models as the turbo versions were offered with certification for flight into known icing conditions. ), Please tell us: 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. Child seats in the baggage compartment were optional. Fuelburn: 15.0 GPH The 210C Two Ten seats up to 3 passengers plus 1 pilot. Single engine piston aircraft with retractable landing gear. The semi-Fowler flaps were stretched outboard which gave way for a lower landing speed. View all new & used Cessna 210 Single Engine Piston aircraft for sale at ASO.com. The basic disassembly, inspection and reassembly takes almost 40 man-hours at a labor rate of almost $100 per hour. 0 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. Ells is the owner of Ells Aviation (EllsAviation.com) and lives in Templeton, Calif. with his wife Audrey. Total fuel burn from Connecticut to Wisconsin was almost the same on the C210 as it was on the Grumman Tiger. Its hard to believe when looking back, but the standard sacred six flight instrument panel configuration wasnt standard in the 210 until 1975. For instance, in 1961 the optional fuel capacity was increased to a whopping 84 gallons for the 210B. The Cessna 210 Centurion is powered by a Continental IO-470-E engine of 260 hp. The airplane is fast enough for our purposes, it can take us to 20,000 feet if need be, well above most of the weather, and it has the payload to carry all the miscellaneous things we usually stuff inside.. Davtron M811B Digital Timer But set the power and trim correctly and its childs play. Logs show repair to horizontal stabilizer ribs in 2007 Depending on the winds, I could do the first leg nonstop with adequate reserves. Electric Pitch Trim No other single comes close to this except the Piper Saratoga, which rings in about 30 pounds shy and flies more slowly. The model 210 was a conventional aspirated version. Fuel cost per hour: Like the 210R/T210R, the tail surfaces were larger and optional fuel tanks (in the outer wing panels) boosted the total usable fuel to 115 gallons. The P210N was immediately recognizable by its rounded windows, again a concession to pressurization. If fixed landing gear is more to your liking, then Piper, Cirrus and Cessna have other offerings making the cut. On the bad news side were 20 fuel-related accidents. The takeoff weight was increased to 1,542 kg. As a result, many buyers purchased King radios and Cessna eventually responded by refusing to offer any competing avionics for a time. 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. Teardown showed that the aluminum end had broken off a piston wrist pin, hammering an instant hole in the side of the piston. Performance Specs. Since the Centurions wereand still arehighly desired as instrument aircraft, Cessna pioneered electrical redundancy in singles with optional dual alternators and vacuum pumps. Ive flown from my base on Long Island, New York, to Nova Scotia, Grand Turk, Santa Monica and Alaska, plus many points in between during my 17 years of ownership. These qualities also make the 210 an excellent IFR aircraft, perhaps one of the best available. The 2.5 hours of deicing is with the system running on the anti-ice setting. Designated as the 210K- it is powered by an IO-520-L engine with 300 horsepower limited to five minutes. I just completed the installation of a new Airtex interiora huge job when done correctly. At the same time the MTOW for the turbocharged T210N jumped to 4,000 pound. We currently own a 1976 Cessna 210Lour second Cessna 210purchased in 2016 for $105,000. Learn more about Mailchimp's privacy practices here. Stepping up from a Piper Dakota, I considered the 210, Bonanza and a Saratoga. The keys to a smooth running system are an airworthy hydraulic pump, since some actions depend on the proper fluid pressures; and well-maintained electrical gear position switches and wiring. The aircraft was developed into 26 model variants. Dual Avionics Master Switches Chief among them: Cessna engineers had to devise a way to hide its landing gear in the belly. MAC 1700 2'nd NAV/COMM The manual specifies MIL-G-25760 grease. Both Precise Flight and Knots 2U offer electric-actuated speedbrakes that work well and are a good value. Complete and Original Log Records 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. My friends, the Cabots, formerly of Princeton, Massachusetts, have had a predilection for 210s since I met them in the early 1990s. Often the winning solution is the Cessna 210 Centurion. By 1983, base tab for a P210N had risen a full $100,000enough so that Pipers introduction of the world-beater, 1984 Malibu caused Cessna to shelve the P210 for a year while they rethought the design. They succeeded, but no one would call the results elegant. AirplanesUSA proudly presents this clean Cessna 210D to market. Alternator Overhauled August, 2021 Fuel Burn @ 75%: 15.0 GPH 0 Saddle replacement was required for 1960 and 1961 models. It is our mission to be the go to leaders in the aviation industry. The price would have needed to be prohibitively high in order to turn a profit. Many of them, too, are related to the systems general complexity. 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. I was able to sell their turbo and found them a pristine 1985 P210R in Phoenix. With the Centurion, possible downsides are finding a well-maintained example and keeping it that way, or adopting a problem child and paying big to get it rightor as weve seen so many timespractically giving it away just to get out of it. Accordingly, the P210s system wasnt nearly as stout as the Mirages 5.5 psi. 2023 GlobalAir.com. The Centurion is, at best, a truck. IFR Cert Accomplished August, 2021, Continental IO520-A Technicians and owners need to delve in the successive manuals for all the information. It was designated as the 210N. Mooneys M22 Mustang preceded the P210 by a decade, though it was overweight, ran hot and offered disappointing performance. If youre looking to travel in style above the weather in pressurized comfort, it would very hard to beat a Vitatoe-modified P210. 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. Hal Cabot feels the 210Rs pressurization system is the principal benefit. 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.. Overhaul included VAR Crankshaft and New Slick Magnetos Cessnas specs suggest the R model ascended at 1150 fpm200 fpm better than the N Centurions. The Cruise Performance tables in the IM lists a cruise speed of 180 knot cruise speeds (80 percent power/17.8 gph) at 10,000 feet and 196 knots for the same power setting/fuel burn at 20,000 feet. The bigger turbo was needed to provide enough bleed air to pump up the cabin while not restricting the airplanes climb or cruise performance. If you want a lot of 210 for your money and dont mind the chin bump and a little less room in the cabin, any 1964 to 69 210 is a good choice; the 1968 or 1969 T210 had pneumatic de-ice boots and a hot prop as options, which further upped the utility of this very capable airplane. We note that cantilever-wing 210s have long, skinny fuel tanks and the wings have little dihedral, so the airplane must be parked wings level to assure the tanks can be completely filled. In general, fit and finish in many Cessnas is not the best and the 210 is no exception: Poorly fitting doors and aging seals occasionally lead to drafty cabins. The second was when a gear door actuator blew apart because of incorrect assembly by an incompetent mechanic. 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. ), until it ate a runway in Florida. By almost any measure, the Cessna 210 is a flexible, successful airplane. Cessna Aircraft Information Manual - 210 Centurion Overview: Cessna Aircraft Information Manuals include the same data and limitations contained in the original aircraft Pilot's Operating Handbook, however they are not specific to your serial numbered aircraft. Learn more, Cessna Flyer Association1042 N Mountain Ave Suite B #337Upland, CA91786Phone: 626-844-0125, Cessna Flyer Association 2004-2022 All Rights Reserved. That original airplane was certified for a gross weight of only 2900 pounds (a number that would increase to 4100 pounds by the close of production in 1986). The T210N was also the first single, along with the P210N, to be certified for flight into known icing (FIKI) conditions. ), Please tell us: - Aircraft specific reviews and articles. Panel features a Garmin 430W and an approach coupled and auto-trimming STEC 55 autopilot. Neither had ice protection, which I installed on the 210 during my first year of ownership. Uplock assembly is spring loaded to the locked position to relieve hydraulic system pressure. Our previous Blackstone oil analysis report was glowingly positive, there was no metal in the last oil filter change and there was only about a minute of warning on the engine monitor as it showed a very rapid increase in one cylinders temperature to just above 400 degrees before it seized. Once trimmed, it goes where you point it and although some owners complain about the ride in turbulence, there should never be any question of control. Total Time: 7070 Engine 1 Time: 1480 Useful Load: 1004 Condition: Used Additional Classifications Detailed Description 1964 Cessna 210D, 7070 TT, 1480 SMOH, GNS-430W GPS, STEC 50 Autopilot, GTX 345 Transponder, King KSC-55A HSI, Horton STOHL Kit, Strike finder Avionics / Equipment Early models relied on an engine-driven hydraulic pump, which was later upgraded to an electrohydraulic system. Speed is the 210s true forte. We made the trip1,178 nm in a straight linewith one stop in seven hours. Learn more about Mailchimp's privacy practices here. 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. The new gear legs provided an additional six inches of tread and allowed the MTOW to zoom up to 3,800 pounds. 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 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 Bonanza lacked the payload and loading flexibility, and the Saratoga was slower than either. Figures provided are averages for the more common models, and have been rounded to the safer side. by the manufacturer or FAA. For both the 210B and 210C, MTOW upped to 3,000 pounds. More Info. - Send us pictures of your plane. A six-seat retractable single can be a logical and compelling. Panel features a Garmin 430W and an approach coupled and auto-trimming STEC 55 autopilot. 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. These two will mix in a plenum above the rudder pedals and youll have a rush of warm air that will easily reach the baggage area. Fewer than 175 R models were built. Fly lean of peak, send the magnetos to a good shop for inspection at least two or three times per engine overhaul cycle, use a fuel totalizer to avoid tanking more fuel than you need, and overhaul the engine-driven hydraulic power-pack more often than the engine. 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. Features. The first was when the rubber plunger in the gascolator failed and a spare wasnt available. As technicians have become more familiar with the system, many problemslanding gear door valve failures or hydraulic reservoir depletion resulting from control-cable chafing, for examplehave been minimized. You could carry full fuel, six 170-pounders and about 10 pounds of baggage. 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 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. Various components get blamed for gear problems but the overall issue is sheer complexity: Theres a lot going on when the gear is cycled. Also belying its 182 roots were a strut-braced wing and seating for four. step-up aircraft. Please send us your experiences on your aircraft. Weve seen plenty that are chewed up. A turbocharged T210 and a pressurized P210 were also offered. I do as much maintenance as FAR 43 App A, part C allows. 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. 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. Each of the four co-owners pays a fixed monthly fee of $230 (less than a car payment), which covers our hangar ($250 per month), the base annual inspection ($4220 per year), insurance ($3200 per year) and nav data subscriptions ($576 per year). Own avionics manufacturer, ARC, and the brand was not renowned its... 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These qualities also make the 210, Bonanza and a Saratoga with a Garmin with... Specific reviews and articles twins are in Cessnas future models as the 210K- it powered. Finished P210N was immediately recognizable by its rounded windows, again a concession to pressurization Cessna until 1986 FAR App. Result, many buyers purchased King radios, which were trouble-free right up to the gear valve! Turbocharged T210 and a 24V electrical system piston aircraft for sale at ASO.com airplanesusa presents... First was cessna 210d specs a gear door actuator blew apart because of incorrect assembly by an incompetent mechanic 48 states passengers.