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. From a manufacturers point of view, those are powerful reasons not to resurrect a discontinued model. For both the 210B and 210C, MTOW upped to 3,000 pounds. Also belying its 182 roots were a strut-braced wing and seating for four. The weakest part of the plane has been the TSIO-520 engine and its accessories it made TBO only once. The first P210 was introduced in 1978, utilizing the push-pull P-Skymasters 3.35 psi pressurization system. takeoff weight: 4,000 lb (1,814 kg) I installed GAMI injectors and run lean of peak with the help of an engine monitor. It came with King radios, which were trouble-free right up to the time I replaced them with a Garmin stack with ADS-B. 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. Hes a former tech rep and editor for Cessna Pilots Association and served as associate editor for AOPA Pilot until 2008. As an invaluable source of wisdom and support, 210 owners should join the Cessna Pilots Association. All 210s built from 1960 to 1969 live under the shadow of this problem. If not, repetitive inspections at 1000-hour intervals are called for. But theres no free lunch. ) Various components get blamed for gear problems but the overall issue is sheer complexity: Theres a lot going on when the gear is cycled. 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 alternator has been a source of constant grief, with my B&C standby getting me home on at least seven separate occasions when the primary failed. Ninety gallons of fuel was standard tankage on 210G through -N models. The P210 was, in fact, the first pressurized single. I once rode shotgun in a 1968 T210 from Santa Maria, Calif. (KSMX) to Addison, Tex. Performance varies significantly between models, an average or most common figures are indicated. The P210N was immediately recognizable by its rounded windows, again a concession to pressurization. We made the trip1,178 nm in a straight linewith one stop in seven hours. 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. But the peak had been reached. Complete and Original Log Records View 153 CESSNA 210 For Sale PAPI Price Estimate (as of June 1, 2022): $126,134 . One example SDR: Rivets holding nose gear drag brace fitting in place worked loose over years of operation causing fitting to pull loose from aircraft structure. The price would have needed to be prohibitively high in order to turn a profit. 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. Model 210 was first flown in 1957, 575 built. I ran the first IO-520 engine to 2200 hours without any major maintenance issues and with the original cylinders. It featured nose-mounted landing lights and a 24V electrical system. Best Cruise: 160 KIAS 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. 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). I keep the airplane hangared and self-insure the hull, but spend $800 per year on liability insurance. Figures provided are averages for the more common models, and have been rounded to the safer side. The Cessna Pilots Association is a great asset for Cessna owners. Both -R models came with 87-gallon fuel tanks as standard and were optionally equipped at the factory for 115 gallons. With luck, the cracks are found during annual inspections and are fixed in any airplanes now on the market. Editor in Chief Larry Anglisano has been a staple at. - Aircraft data that you believe is inaccurate or have specific experiences. Horsepower: 285: Gross Weight: 3100 lbs: . Cessna 210 D & E Centurion - Performance Data. Owners tell us theyre better off when they pay the money now, fixing stuff before it breaks, rather than later when theres no choice. Engine 1 Time: 113 SFRM. - Send us pictures of your plane. At that time, theyd just traded up from a Skylane and were flying a 79 T-210N they were convinced theyd live with forever. The type was known, from the up-powered 210D if 1964, as the Centurion. Often the winning solution is the Cessna 210 Centurion. Given the dismal accuracy to be expected from aircraft fuel gauges, this potential mismatch between what the pilot thinks is on board and what is actually there poses a possible hazard. A very low time engine and factory new prop are complimented by a clean airframe with complete logs and capable IFR instrumentation. (4) pull back the down locks and (5) flow on to the gear actuating cylinders. 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 Cessna 210 Centurion is a six-seat, high-performance, retractable-gear, single-engine high-wing general aviation aircraft produced from 1957 to 1986. I flight plan at 150 knots and typically burn a little under 80 PPH lean of peak for six hours of endurance. Performance specifications Horsepower: 1 x 260 HP Best Cruise Speed: 165 KIAS Best Range (i): 700 NM Fuel Burn @ 75%: 13.5 GPH Stall Speed: 51 KIAS Rate of climb: 1,300 FPM Ceiling: 20,700 FT Takeoff distance: 620 FT Landing distance: 750 FT Takeoff distance over 50ft obstacle: 1,135 FT Landing distance over 50ft obstacle: 1,190 FT Weights In 1962 for the 210C, the fuselage was widened. 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 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 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. The final version of the P210, the R model, was introduced in 1985. 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. Getting into the rear seats can require the agility of a gymnast, so that area is usually reserved for extra baggage. I was able to sell their turbo and found them a pristine 1985 P210R in Phoenix. This change made it possible to enlarge the cabin interior space. A very low time engine and factory new prop are complimented by a clean airframe with complete logs and capable IFR instrumentation. Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. certified aircraft database Cessna Aircraft history and gallery C210 A Two Ten C210 B,C Two Ten . Child seats in the baggage compartment were optional. The fewest and most costly versions were the T210R and P210R. The full cantilever, laminar flow wing came along in 1967, and power was bumped up again in 1970 to 300 hp. The second was when a gear door actuator blew apart because of incorrect assembly by an incompetent mechanic. 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 1985 210R/T210R was upgraded again. Still, we used to put six adults in a T210 pretty regularly, with the smallest people in the far aft seat. Dual Push to Talk Login April 15, 10:46 AM US EDT If fixed landing gear is more to your liking, then Piper, Cirrus and Cessna have other offerings making the cut. If youre looking to travel in style above the weather in pressurized comfort, it would very hard to beat a Vitatoe-modified P210. I purchased N732AV, a 1976 C210L, in the fall of 1981. On the good news side, the number of runway loss of control (RLOC) accidentsfivewas astonishingly low, a tribute to good design. 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. The normally aspirated 210L turned out to be perfect for that mission. Panel construction: Laser-drilled titanium: Tank capacity: 6.2 gallons (23.46 litres) Endurance: 2.5 Hours in Anti-Ice Mode . Learn About Bill's Book Here, Designed by Elegant Themes | Powered by WordPress. Bose Ship Mounted Headset Connector/Adapter. 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.. CESSNA 210D Centurion Performance specifications Horsepower: 1 x 285 HP . 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. No warranty of Condition: Used. (Interestingly, rather than mount a second door on the P-Skymaster, Cessna chose to limit the airplane to five seats.). 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. Ventilation and heating are generally good except for the rear of the cabin. 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. Centurion maintenance is not trivial, especially the landing gear. ( Technicians and owners need to delve in the successive manuals for all the information. Flaps were lengthened, the ailerons were redesigned and the horizontal stabilizer widened by 10 inches. . Owners report a significant maintenance burden with annuals that run around $3000on the low end. When she gives me mechanical grief I could cry. This eliminated the chin bump in earlier models. That can be a big help if youre flying in the proper direction., One area where the 210 still had an advantage over the Malibu was vertical cabin space. 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