The 2.5 hours of deicing is with the system running on the anti-ice setting. Posted by Bill Cox | Nov 3, 2015 | Featured Plane. A 210 needs to be flown on-speed on approach: It will float a long ways if the approach is fast. 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. But, when shes working right, theres no airplane like a Turbo 210. 172 F172F F1720086 F1720179 210 210D 21058221 21058510 172 F172G F1720180 F1720319 210 210E 21058511 21058715 172 F172H F17200655 F17200754 . In 1970, the first full six-seat variant was developed. All 210s built from 1960 to 1969 live under the shadow of this problem. ) AirplanesUSA proudly presents this clean Cessna 210D to market. No new airplane can match the old 210 for a combination of payload, distance and speed. 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. 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. Alternator Overhauled August, 2021 Bye-bye, wing struts. I flight plan for 155 knots, hauling 90 gallons of fuel and burning 12.5 GPH lean of peak. Both Precise Flight and Knots 2U offer electric-actuated speedbrakes that work well and are a good value. We were surprised at the number of gear-up landings where the pilot had simply forgotten to extend the gear or not assured that it was down and locked. 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. A good thorough preflight after an annual is essential. Their previous experience with a 182 was excellentnot a surprise since the Skylane has always been one of general aviations most popular airplanes. The Cessna Pilots Association is a great asset for Cessna owners. Still, there were major differences. Thanks to limited elevator travel, the Centurion is tough to wrangle into a full-stall break, so theres nothing particularly nasty about them. 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. 0 They sold a bunch of them. Early models relied on an engine-driven hydraulic pump, which was later upgraded to an electrohydraulic system. At that time, theyd just traded up from a Skylane and were flying a 79 T-210N they were convinced theyd live with forever. ) - Send us pictures of your plane. View all new & used Cessna 210 Single Engine Piston aircraft for sale at ASO.com. Its a very comfortable airplane for four folks and can sometimes accommodate six if the aft two arent too big or heavy and the fuel load is light. The first major change took place for model year 1964 with the 210D. 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. The 1985 210R/T210R was upgraded again. Buyers should check the saddles and replacement times on these aircraft. Many 210 lovers regard the P210R as the best of the type. As an Amazon Associate I earn from qualifying purchases. Cessna 140: The Last of Cessnas Little Taildraggers, 177RG Cardinal: Cessnas Airplane of the 70s. Fuel Burn @ 75%: 15.0 GPH CPA has an excellent buyers guide on the 210. 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 biggest issue I found was mechanics who were not familiar with the planecreating maintenance-induced problems. The aircraft was developed into 26 model variants. I just completed the installation of a new Airtex interiora huge job when done correctly. ), Best rate of climb, SL (fpm): 1145, Max operating altitude (ft): 25,000, Stall (Vso kts): 58, TO over 50 ft (ft): 2110, Ldg over 50 ft (ft): 1600, Bill Cox took his first flight in a Piper J-3 Cub in 1953 and has logged some 15,000 hours in 311 different types of aircraft since. 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. The Cabots report typical cruise speeds of 170 to 180 knots at middle altitudes, burning 20-21 gph. Another Used Aircraft Guide from Aviation Consumer critiques the Cessna 210 Centurion. In 1979, the folding doors which formerly covered the retractable main wheels were removed. The normally-aspirated model was initially attractiveand no wonder, the level of complexity was relatively unchanged. In 1972, the 210L version was developed. The final version of the P210, the R model, was introduced in 1985. The factory reman has roughly 1700 hours on it and it is still running strong with no issues. step-up aircraft. They jetted out from Massachusetts the following day, bought the airplane on the spot and have lived happily ever after. We observed that no one was injured in the gear up landingseven when the landing gear was partially extended. Annual inspections (if the engine doesnt have issues) run about $5000. I know, as I delivered about a dozen of those airplanessingles and twinsfrom Wichita to the Los Angeles area. Used parts are sometimes an option, given the relatively high population of 210s. 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 . Max take-off weight 2900 lbs. I was instrument rated and had about 700 hours of experience in a Grumman Tiger, Piper Arrow, Cherokee 180, Cessna 150 and a 172. Cessna 210. Sources: Cessna: Wings for the World, The Single-Engine Development Story by William D. Thompson. Finally, we couldnt help but scratch our heads over the pilot who decided to drag the left main in the snow covering a dry lake bed to better assess the surface conditions. Unfortunately, drag rapidly increased and sucked the aircraft down. Full power didnt helpthe airplane sunk into the snow and nosed up. I believe this figure is still on the rich side of the peak EGT. The Bonanza lacked the payload and loading flexibility, and the Saratoga was slower than either. In 1961, the fuselage and wing were entirely restructured; the fuselage became wider and deeper, and there was an added third window on the side. 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. ), a total distance over a 50-foot obstacle of 1,365 feet and an as-delivered useful load of 1,340 pounds. 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. Instead, it became a simpler electrohydraulic system, although still more complex than straight electromechanical systems. Saddle replacement was required for 1960 and 1961 models. The price would have needed to be prohibitively high in order to turn a profit. Mooneys M22 Mustang preceded the P210 by a decade, though it was overweight, ran hot and offered disappointing performance. Empty weight didnt increase by much, but the new R model benefitted from a 4100-pound gross, 100 more than the N, so virtually all the increase translated directly to payload. ( (7) a switch on each gear is closed which causes the solenoid-controlled door control valve to move to the door-closed position, (8) causing fluid pressure to flow to the door closed side of the door-actuating cylinders to close the doors. The 210 is a remarkably adaptable airplane. Best Range: 680 NM Davtron Model 902A Digital VOR This more powerful turbocharged engine is relatively easy to install in earlier T210s via an STC held by RAM Aircraft of Waco, Tex. fitness for any purpose is made or implied. 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. The second was when a gear door actuator blew apart because of incorrect assembly by an incompetent mechanic. Even so, the T210 was a great high flyer, capable of topping everything but the most aggressive of thunderstorms. 1978 CESSNA P210N Piston Single Aircraft Price: USD $269,900 USD $1,724.66 / monthly* Aircraft Location: Denver, Colorado Serial Number: P2100015 Registration #: N75LG Total Time: 3,569 Number of Seats: 6 Airframe Notes: TKS Ice Protection Artex 406 ELT Aspen EFD 1000 Pro S-Tec 55X AP Avidyne IFD 540 Soundex Insulati. 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. And make sure the elevator skin itself has not become corroded thanks to water absorption by the foam filler, especially in older 210s. No retractable gear singles nor twins are in Cessnas future. General Specs (cont.) I have learned many things about the 210 in the last 12 years. The 300A autopilot was trouble-free and working great right up to the time it was replaced with a STEC 50. 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 5.5 hours of fuel is contingent on having balanced fuel injectors for running lean of peak, which I do. The OEM 1970-vintage wire-wound potentiometers in the gauge control unit are susceptible to corrosion, which can lead to erratic readings. (Owners of older models can have their gear doors removed through an STC.). The Cessna 210s were produced from 1957 to 1986 with a total of 9,240 aircraft built. Southwind Aviation, Inc. . F. My impression is that this modification solves any engine heating problems, thereby delivering better performance than the original powerplant installation. If they decide to sell now, it will be to get out of aviation altogether. When everything is working correctly on our P210R, we see a cabin altitude of between 10,000 and 11,000 at 20,000 feet, but in fact, we rarely fly that high. Cessna 210 D & E Centurion - Performance Data. A slightly larger cabin, a 100-pound gross weight increase and a different engine (IO-470-S) resulted in the 210B. Still, like any high-performance single, the 210 can benefit from the installation of speedbrakes. Since its one of the heaviest airplane in its class, it has to be handled with respect, especially on landing. Overhauled November 2008 by Northwest Propeller Service Puyallup, WA, Garmin GNS 430W NAV/COM/GPS with GPSS 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. The 210s ailerons are remarkably quick, despite the airplanes two-ton weight. 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. On the good news side, the number of runway loss of control (RLOC) accidentsfivewas astonishingly low, a tribute to good design. Getting into the rear seats can require the agility of a gymnast, so that area is usually reserved for extra baggage. 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. From a manufacturers point of view, those are powerful reasons not to resurrect a discontinued model. 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. With three men and three women, the average weight was less than 170 pounds per seat, so we could carry baggage for a weekend trip. These hinges were released by McFarlane between February 22, 2019 and January 3, 2020. . 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. Horsepower: 1 x 285 HP. STEC 55 Approach Coupled Autopilot Search 1000's of Aircraft listings updated daily from 100's of dealers & private sellers. Cessna has published warnings to that effect. Detailed Description The solution is to immediately change tanks and follow Cessnas recommendations on fuel pump use. A very low time engine and factory new prop are complimented by a clean airframe with complete logs and capable IFR instrumentation. It was designated as the 210N. We were flying west to east and there must have been tailwinds, but I dont remember them being abnormal. 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. They are also vulnerable to ham-fisted mechanics damaging them. Steve Ells has been an A&P/IA for 44 years and is a commercial pilot with instrument and multi-engine ratings. No warranty of ) But theres little question the strutless model looks faster, sleeker and more modern. Its all there; its just not all in one place. In the 2700 hours I have flown the plane, there were only two instances where the plane was not ready to support the mission due to mechanical issues. Seven years later, in 1979, Cessna introduced another simplification by eliminating the main gear doors. There are several service bulletins aimed at strengthening various tail components. The Cabots seem to agree. While still hydraulic, it no longer relied on an engine-driven pump. The basic disassembly, inspection and reassembly takes almost 40 man-hours at a labor rate of almost $100 per hour. ), until it ate a runway in Florida. The remainder were unexplained. If fixed landing gear is more to your liking, then Piper, Cirrus and Cessna have other offerings making the cut. 0 The full cantilever, laminar flow wing came along in 1967, and power was bumped up again in 1970 to 300 hp. 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 Ventilation and heating are generally good except for the rear of the cabin. Delete cookies, By using our website, you agree to our use of cookies. 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). MTOW was again boosted to 3,100 pounds. 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 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. Got substantial flight time in a 100-series Cessna? 117 Hours SMOH Speed is the 210s true forte. Figures for a 1969 T210J show a service ceiling of 30,200 feet (! Again, if trimmed on speed, the 210 can be landed with no undue strain. Complete and Original Log Records Too, the historic nemesis of older Centurionsfatigue cracks in landing gear saddleshas apparently not abated completely. A 210 was an obvious next choice. By almost any measure, the Cessna 210 is a flexible, successful airplane. I do as much maintenance as FAR 43 App A, part C allows. We made the trip1,178 nm in a straight linewith one stop in seven hours. 0 Technicians and owners need to delve in the successive manuals for all the information. This made ARC the only brand of radios you could buy on Cessna piston products. I have interviewed P210 owners that spoke of the need to keep a close eye on engine CHTs especially during hot days. Stats. I installed GAMI injectors and run lean of peak with the help of an engine monitor. He can be contacted via email at flybillcox@aol.com. 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 Best Cruise Speed: 166 KIAS . Some owners simply replace them whether theyre cracked or not. Its not difficult to land, mind youespecially when theres some weight in the backbut it suffers its share of hard landings, swerves, runway overruns and gear collapses. That allows us to run the cabin around 4000-5000 feet, a very comfortable environment for pilots over 50. Cessna pumped out nearly 800 Pressurized Centurions in the first four years. In 1969 the dihedral angle was reduced and the engine oil sump was changed to allow the nosegear to retract further into the fuselage. Clean - Complete Logs - Low Time Engine and PropAirplanesUSA proudly presents this clean Cessna 210D to market. Accordingly, the P210s system wasnt nearly as stout as the Mirages 5.5 psi. ( 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. (6) The gear legs move to the up position. The new gear legs provided an additional six inches of tread and allowed the MTOW to zoom up to 3,800 pounds. 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. One stop in seven hours on fuel pump use the elevator skin itself has not become thanks. 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