Cessna 200 Series Service Manual 1966-1968 – 210G T210G 206 U206 P206 Repair Manual PDF

Description

Cessna 200 Series Service Manual 1966 Thru 1968 – 210G, T210G, U206, P206 Repair Manual PDF

This Cessna 200 Series Service Manual covers factory-recommended ground handling, servicing, lubrication, inspection, and repair procedures for all 200-Series airplanes built from 1966 through 1968. It is the March 1968 original publication as updated by Change 1 (11 December 1975) and Revision 2 (1 June 2004), which incorporates Temporary Revisions 1 through 5. Coverage spans the 210F, 210G, 210H, T210F, T210G, T210H, U206A/B/C, TU206A/B/C, P206A/B/C and TP206A/B/C models. The manual is written for both experienced mechanics and less experienced technicians, with step-by-step procedures given throughout.

File Details

• Manual type: Service / maintenance manual
• Publisher: Cessna Aircraft Company
• Manual number (paper copy): D606-2-13
• Manual number (aerofiche): D606-2-13AF
• Temporary revision number: D606-2TR6
• Original date: March 1968
• Change 1 date: 11 December 1975
• Revision 2 date: 01 June 2004
• Language: English
• File format: PDF
• Page count: 609

Chapters Covered

• 1 General Description
• 2 Ground Handling, Servicing, Lubrication, and Inspection
• 3 Fuselage
• 4 Airframe
• 5 Non-Retractable Landing Gear
• 5A Retractable Landing Gear and Hydraulic System
• 6 Aileron Control System
• 7 Electrical Flap Control Systems
• 8 Elevator Control System
• 9 Elevator Trim Control System
• 10 Rudder Control System
• 11 Rudder Trim Control Systems
• 12 Powerplant
• 12A Turbocharged Powerplant
• 13 Fuel System (Except Cantilever Wing)
• 13A Fuel System (Cantilever Wing)
• 14 Propellers
• 15 Utility Systems
• 16 Instruments and Instrument Systems
• 17 Electrical Systems
• 18 Structural Repair
• 19 Painting
• 20 Wiring Diagrams
• Appendix A Hydraulic Components Repair

The Cessna 200 Series Service Manual is structured so each section breaks down into removal, installation, disassembly, repair, reassembly, adjustment, rigging and inspection, making it a complete teardown and rebuild reference rather than just a tune-up guide. Sections 5 and 5A together cover both the fixed-gear 206 and the hydraulically retractable gear used on the 210 and T210, including the Power Pack, hydraulic filter, priority valve, emergency hand pump, downlock and uplock mechanisms and the full landing gear electrical circuit. Wiring diagrams appear in Section 20 and hydraulic schematics in Section 5A.

Model and Serial Number Coverage

• 210F (1966): 21058716 – 21058818
• 210G (1967): 21058819 – 21058936
• 210H (1968): 21058937
• T210F (1966): T210-0001 – T210-0197
• T210G (1967): T210-0198 – T210-0307
• T210H (1968): T210-0308
• U206A (1966): U206-0438 – U206-0656
• U206B (1967): U206-0657 – U206-0914
• U206C (1968): U206-0915
• P206A (1966): P206-0161 – P206-0306
• P206B (1967): P206-0307 – P206-0419
• P206C (1968): P206-0420
• TU206A/B/C and TP206A/B/C use the same serial ranges as their normally aspirated counterparts

Engines, Propellers and Key Specifications

• Engine: Continental IO-520 series (210, U206, P206) – six-cylinder, horizontally opposed, air-cooled, fuel-injected
• Engine: Continental TSIO-520 series (T210, TU206, TP206) – turbocharged
• Standard propeller: 82 inch McCauley, two-blade, constant-speed
• Optional propeller: 80 inch McCauley, three-blade
• Design gross weight: 3300 lb (210), 3400 lb (T210), 3600 lb (206)
• Fuel capacity: 90 gal (210), 65 gal standard / 84 gal optional (206)
• Oil capacity: 12 qt
• Hydraulic fluid: MIL-H-5606
• Recommended fuel: Aviation grade 100/130 minimum

What This Cessna 200 Series Repair Manual Covers In Detail

Sections 1 and 2 set out the general layout of the 210 and 206 families, principal dimensions, jacking, hoisting, tie-down, leveling, fuel and oil servicing, induction filter servicing, tire and strut pressures, lubrication charts and the inspection schedule. Sections 3 and 4 address the fuselage, airframe, doors, seats, upholstery, wings, wing struts, cantilever wing, fin and horizontal stabilizer – including their respective removal, repair and installation procedures. Sections 6 through 11 cover the flight controls: aileron, electrically actuated flaps, elevator, elevator trim, rudder and rudder trim systems, with rigging instructions and cable tension values for each. Sections 12 and 12A handle the powerplant, and Section 12A specifically covers the turbocharged TSIO-520 installation, waste gate, controller, exhaust insulation and turbocharger oil lines. Sections 13 and 13A split the fuel system between the strut-braced and cantilever-wing configurations, while Section 14 covers McCauley propeller removal and governor servicing. Sections 15 through 17 cover utility systems, instruments, and the aircraft electrical system. Sections 18 and 19 cover structural repair and painting, and Section 20 provides wiring diagrams. Appendix A gives hydraulic component repair procedures for the Power Pack, actuators and the emergency hand pump.

Why This Cessna 210G T210G U206 P206 Service Manual Matters

Procedures that matter on a legacy 200-Series airframe – landing gear rigging, hydraulic Power Pack testing, downlock and uplock clearances, torque link servicing, cable tension and control surface rigging, engine oil and filter intervals, wheel alignment shimming, brake bleeding and parking brake servicing – all come with the values and limits the factory set out. Following these procedures rather than generic guesses is what keeps the airplane airworthy and protects expensive assemblies like the hydraulic rotary actuators, the saddle bearings, the Power Pack and the turbocharger system.

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This Cessna 200 Series Service Manual 1966-1968 arrives as an instant PDF download – no shipping, no waiting, no paper manual to lose. Open it on a laptop in the hangar, a tablet on the wing, or a phone under the cowling, and print the pages you want to keep next to the airplane. Buy the Cessna 210G T210G U206 P206 repair manual PDF once and it stays available for every inspection, every rigging job, and every repair for the life of the aircraft.