Cessna Service Manual offers detailed servicing instructions for the Cessna 210 Centurion Series 1970-1976 aircraft. The Service repair manual will give you complete step by step information on repair, servicing and preventative maintenance for your Cessna. The manual is highly detailed with photos and illustrations to help guide you through every repair and troubleshooting procedure. This manual contains all you need to know to keep your Cessna 210 working right and is the only service repair manual you will need. It will help you understand, care for, service and lower the repair and maintenance cost for your Cessna 210.

Cover the following Cessna 210 Years & Models
1970 - 210 & Centurion Series
1971 - 210 & Centurion Series
1972 - 210 & Centurion Series
1973 - 210 & Centurion Series
1974 - 210 & Centurion Series
1975 - 210 & Centurion Series
1976 - 210 & Centurion Series

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* PDF FORMAT

* Easy navigation allowing you to identify the exact service procedures in the quickest time possible.

*Detailed illustrations, exploded diagrams, drawings.

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File Format: PDF
Printable: Yes
Language: English
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Cessna 210 Model Information

210
Four-seat production variant with a Continental IO-470-E engine, 40 degrees hydraulic flap, gear doors, introduced in 1960.[8], first flown in 1957, 575 built.[2]

210A
A 210 with a third cabin window on each side, introduced in 1961, 265 built.[2]

210B
A 210A with a cut-down rear fuselage, a rear vision window and a Continental IO-470-S engine, introduced in 1962, 245 built.[2]

210C
A 210B with some minor changes, introduced in 1963, 135 built.[2]

210D Centurion
A 210C fitted with a 285 hp (213 kW) Continental IO-520-A engine and increased take-off weight to 3,100 lb (1,406 kg)[8], introduced in 1964, 290 built.[2]

210E Centurion
A 210D with some minor changes, introduced in 1965, 205 built.[2]

210F Centurion / Turbo Centurion
A 210E with some minor changes and optional 285 hp (213 kW) turbocharged Continental TSIO-520-C engine, introduced in 1966, 300 built.[2]

210G Centurion / Turbo Centurion
A 210F with a strutless cantilver wing and modified rear window, increased take-off weight to 3,300 lb (1,497 kg)[8], introduced in 1967, 228 built.[2]

210H Centurion / Turbo Centurion
A 210G with a new flap system and instrument panel, 210 built.[2] Flap range decreased to 30 degrees, fuel capacity increased from 65 to 90 USgal (246 to 341 l). Introduced in 1968.[8]

210J Centurion / Turbo Centurion
A 210H with reduced wing dihederal, different nose profile and a Continental IO-520-J (or TSIO-520H) engine, introduced in 1969, 200 built.[2]

210K Centurion / Turbo Centurion
A 210J with rear changed to full seat to provide six seats, a IO-520-L engine with 300 hp (224 kW) limited to 5 minutes, landing gear changed, enlarged cabin with a single rear side window, weight increased to 33,800 lb (1,724 kg), produced 1970-71, 303 built.[2][8]

210L Centurion / Turbo Centurion
A 210K with nose-mounted landing lights, the electrical system changed to 24 volt, the engine driven hydraulic pump replaced with an electrical pump and a three bladed prop fitted. Improved aerodynamics led to an increase in approximately 8 kn (15 km/h) in cruise speed.[8] Produced 1972-76, 2070 built.[2]

210M Centurion / Turbo Centurion
A 210L with an optional 310 hp (231 kW) TSIO-520-R engine and minor changes, produced 1977-80, 1381 built.[2]

210N Centurion / Turbo Centurion
A 210M with open wheel wells for main landing gear and minor changes.[2] Although this change appeared only on the C210N, most early models have had gear doors removed due to extensive maintenance and handling problems, leaving them similar to the "N".[8] Produced 1981-84, 1943 built.

210R Centurion / Turbo Centurion
A 210N with longer span stabiliser and minor changes, produced 1985-86, 112 built.[2]

P210N Pressurised Centurion
A Turbo 210N with pressurized cabin, four windows each side, with a 310 hp (231 kW) Continental TSIO-520-AF engine, produced 1978-83, 834 built.[2]

P210R Pressurised Centurion
A P210N with longer span stabiliser increased take-off weight and a 325 hp (242 kW) Continental GTSIO-520-CE engine, produced 1985-86, 40 built.[2]