1960-1965 Cessna 200 Series 205 206 210 Service & Repair Manual

200-SERIES SERVICE MANUAL TillS MANUAL SUPERSEDES AND REPLACES ALL PREVIOUS 200-SERIES SERVICE MANUALS. D 310-13 McCormick-Armstrong Co--1500--4/1/65 ------ - .

A LIST Of EFFECTIVE PAGES I Title "A" Page i thru iv 1-1 thru 1-10 2-1 thru 2-40. 3-1 thru 3-27 4-1 thru 4-6 5-l thru 5-10 5-lOA thru 5-lOB 5-11 5-11A thru 5-11D 5-12 thru 5-27 5-27A thru 5-27B 5-28 thru 5-47 5-47A thru 5-47F 5-48 thru 5-67 5A-l thru 5A-23 5A-23A thru 5A-23D 5A-24 thru 5A-34 5B-l thru 5B-19 5C-l thru 5C-30 6-1 thru 6-12 7-1 thru 7-10 7A-l thru 7A-11 8-1 thru 8-9 9-1 thru 9-8 10-1 thru 10-9 11-1 thru 11-5 12-1 thru 12-39-40 12-41 thru 12-54 13-1 thru 13-33 14-1 thru 14-12 15-1 thru 15-11 16-1 thru 16-23 17-1 thru 17-24 18-1 19-1 19-lA thru 19-lB 19-2 thru 19-28 20-1 thru 20-2 INSERT LATEST CHANGED PAGES, DESTROY SUPERSEDED PAGES Appendix Pages Al-l thru Al-3 A2-l thru A2-10 A3-l thru A3-4 A4-l thru A4-2 A5-l thru A5-2 A6-l A7-l A8-l A9-l Al0-1 A11-l Bl-1 B2-l thru B2-22 B3-l thru B3-3 B4-l B5-l thru B5-2 B6-l thru B6-2 B7-l thru B7-2 B8-l thru B8-2 B9-l thru B9-2 c Cl-1 thru Cl-22 C2-l 1270405 thru 16. 1 C3-l 1270625 thru 16.1 Dl-1 thru Dl-2 D2-l thru D2-13 D3-l D4-l thru D4-2 D5-l F

SECTION 1 2 3 4 5 5A 5B 5C 6 7 7A 8 9 10 11 12 13 14 15 16 17 18 19 20 APPENDIX A APPENDIX B APPENDIX C APPENDIX D TABLE OF CONTENTS GENERAL DESCRIPTION GROUND HANDLING, SERVICING, LUBRICATION, AND INSPECTION. FUSELAGE AIRFRAME HYDRAULICS AND LANDING GEAR HYDRAULICS AND LANDING GEAR- 210B THRU 210D LANDING GEAR - MODELS 205 AND 206 SERIES . HYDRAULICS AND LANDING GEAR- 210E AND ON AILERON CONTROL SYSTEM . . . . . HYDRAULIC FLAP CONTROL SYSTEMS ELECTRICAL FLAP CONTROL SYSTEMS ELEVATOR CONTROL SYSTEM ... ELEVATOR TRIM CONTROL SYSTEM RUDDER CONTROL SYSTEM . . . RUDDER TRIM CONTROL SYSTEMS POWER PLANT FUEL SYSTEM PROPELLERS . UTILITY SYSTEMS . INSTRUMENTS AND INSTRUMENT SYSTEMS ELECTRICAL SYSTEMS. ELECTRONIC SYSTEMS STRUCTURAL REPAIR PAINTING HYDRAULIC COMPONENTS REPAIR- 210 & 210A. HYDRAULIC COMPONENTS REPAIR- 210B THRU 210D . ELECTRICAL WIRING DIAGRAMS ........ . HYDRAULIC COMPONENTS REPAIR- 210E AND ON Page . 1-1 . 2-1 3-1 4-1 5-1 5A-1 5B-1 5C-1 6-1 7-1 7A-1 8-1 9-1 10-1 11-1 12-1 13-1 14-1 15-1 16-1 17-1 18-1 19-1 20-1 A1 B1 C1 D1 II

MODEL NAME MODEL SERIALS YEAR 1960 210 57001 thru 57575 1961 210A 21057576 thru 21057840 1962 210B 21057841 thru 21058085 1963 210C 21058086 thru 21058220 1964 210 CENTURION 210D 21058221 thru 21058510 1965 210 CENTURION 210E 21058511 thru 1963 205 205-0001 thru 205-0480 1964 205A 205-0481 thru 205-0577 1964 SUPER SKYWAGON 206 206-0001 thru 206-0275 1965 SUPER SKYWAGON U206 U206-0276 thru (UTILITY CARGO DOOR) 1965 SUPER SKYWAGON P206 P206-0001 thru (PASSENGER DOOR) 1965 SUPER SKYLANE P206 P206-0001 thru - - -- - - - - - - - - - ii

FOREWORD This manual contains factory recommended procedures and in- structions for ground handling, servicing and maintaining Cessna 200-Series aircraft. These include the Models 205, 206, and 210. Besides serving as a reference for the experienced mechanic, this book also covers step-by-step procedures for the less experienced man. This manual should be kept in a handy place for ready reference. If properly used, it will better enable the mechanic to main- tain Cessna 200-Series aircraft and thereby establish a reputation for reliable service. The information in this book is based on data available at the time of publication, and is supplemented and kept current by service letters and service news letters published by Cessna Aircraft Com- pany. These are sent to all Cessna Dealers so that they have the latest authoritative recommendations for servicing Cessna airplanes. Therefore, it is recommended that Cessna owners utilize the know- ledge and experience of the factory-trained Dealer Service Organi- zation. I iii

iv MAINTENANCE AND SAFETY SUGGESTIONS ON ALL 210-SERIES AIRCRAFT 1. When parting any lines, always cap or plug all lines and fittings to avoid entrance of dirt and air into the system. This applies to all test and fill equipment as well. 2. When installing any new lines or equipment, always be certain lines and equipment are clean, have been flushed with clean hydraulic fluid and are as near full of clean fluid as possible to minimize bleeding. 3. Avoid using the airplane hand pump to retract the landing gear. 4. Avoid subjecting the hydraulic system or any component to more than 2200 PSI. It is possible to exceed the pressure limit when external hand pumps are con- nected to bypass the power pack. 5. Avoid rigging adjustments or maintenance on the landing gear when the airplane is not securely on jacks. 6. Avoid pressure of more than 10 PSI to the power pack reservoir during filling operations; otherwise, damage to the reservoir seals may result. 7. Avoid using or installing gust locks on the flaps; otherwise, damage may result if flaps are accidentally operated. 8. Before performing any maintenance in any of the wheel or strut wells, always disconnect the doors to avoid injury from :mintentional actuation of the doors. ON MODEL 210 AND 210A AIRCRAFT 1. Before performing any checking, inspecting, parting of lines and/or maintenance procedures, discharge all pressure from the accumulator by op- erating the wing flaps until pressure has been expended. 2. When removing accumulator from the airplane, always release all nitrogen or air pressure from the accumulator and avoid recharging accum,Jlator until it has been reinstalled in the airplane.

SECTION 1 GENERAL DESCRIPTION 1-1. GENERAL DESCRIPTION - 210 SERIES. The Cessna 210 Series airplanes are four-place, high-wing monoplanes, of all-metal, semi-monocoque airframe construction. The 210 Series employ a fully retractable tricycle landing gear with the familiar spring- steel main gear struts. The steerable nose gear is an air-oil filled oleo strut. The landing gear is hydraulically actuated. Prior to the Model 210D, the wing flaps are also hydraulically actuated. Begin- ning with the Model 21 OD, the wing flaps are electrically actuated. An individual child's seat is located immediately aft of each rear passenger's seat on the Model 210D and on. The airplanes are powered by a single six-cylinder, horizontally- opposed, air-cooled, fuel-injection Continental engine driving an all-metal constant-speed propeller. Distinctive features of the airplane are the swept fin and rudder and the conical camber design of the wing tips. 1-2. GENERAL DESCRIPTION- 205 SERIES. The Cessna 205 Series airplanes are six-place, high-wing monoplanes, of all-metal, semi-monocoque airframe construction. The 205 Series employ a non-retractable tricycle landing gear with the familiar spring- steel main gear struts. The steerable nose gear is an air -oil filled oleo strut. The flaps are electrically actuated. The airplanes are powered by a single six-cylinder, horizontally-opposed, air-cooled, fuel- injection Continental engine driving an all-metal constant-speed propeller. Distinctive features of the airplane are the swept fin and rudder and the conical camber design of the wing tips. 1-3. GENERAL DESCRIPTION- 206 SERIES. The Cessna 206 Series airplanes are high-wing monoplanes, of all-metal, semi-monocoque airframe construction. The 206 Series employ a non-retractable tricycle landing gear with the familiar spring-steel main gear struts. The steerable nose gear is an air-oil filled oleo strut. The flaps are electrically actuated. The airplanes are powered by a single six-cylinder, horizontally-opposed, air-cooled, fuel- injection Continental engine driving an all-metal constant-speed propeller. All 206 Series are equipped with an entrance door on each side of the cabin and a baggage door on the left side of the fuselage, except the Model 206 and U206 Series. The Model 206 and U206 Series are equipped with large double cargo doors on the right side of the fuselage and an entrance door on the left side of the cabin. Except for the P206 Super Skylane, all 206 Series seating arrangements are standard one-place, but provisions are made for the addition of optional seats to make six-place airplanes. The P206 Super Sky- lane is a standard six-place airplane. Distinctive features of the airplane are the swept fin and rudder and the conical camber design of the wing tips. 1-4. Leading particulars of each model, with dimensions based on gross weight, are given in the following charts. If these dimensions are used for constructing a hangar or computing clearances, remember that such factors as nose strut inflation, tire pressures, tire sizes, and load distribution may result in some dimensions that are consider- ably different from those listed. 1-1

MODEL 210 AND 210A DESIGN GROSS WEIGHT FUEL CAPACITY (Total) Optional (210A only) OIL CAPACITY . . . . . . . . . . . . . . . . . ENGINE MODEL (Refer to Section 12 for Engine Data) PROPELLER (Constant Speed) ........ . LANDING GEAR (Retractable Hydraulic Actuated) MAIN WHEEL TIRES Pressure ... NOSE WHEEL TIRE Pressure (210) . Pressure (210A) . . . . . . . . . . . . . NOSE GEAR STRUT PRESSURE (Strut Extended) . WHEEL ALIGNMENT Camber ... . Toe-in ... . AILERON TRAVEL Up ..... . Down ............ •.• WING FLAP TRAVEL (Hydraulic-Actuated) . . . . . . RUDDER TRAVEL (Measured perpendicular to hinge line) Right ..... . Left ...... . ELEVATOR TRAVEL Up ...... . Down •.•... ELEVATOR TRIM TAB TRAVEL Up (210) . . Down (210) ... . Up (210A) .... . Down (210A) . . . . PRINCIPAL DIMENSIONS . 2900 lb . 65 gal. . 84 gal. . 12 qt . CONTINENTAL I0-470-E . 82" HARTZELL or McCAULEY . Tricycle . 15 x 6. 00 x 6, 6-ply rating . 53 psi . 5. 00 x 5, 6-ply rating . 35 psi . 45 psi . 95 psi . +40±1. 50 . 0 to . 06" . 20°±2° • 14°±2° . 0° to 38°, +2°-1 o . 27°13'±1 ° . 27°13'±1 ° . 26°30'±1 ° . 22° ±1 ° . 25°,+1°-0° .15°,+1°-0° . 10°' +2° -0° . 25°' +2° -0° Wing Span . . . . . . 36' 7" Tail Span . . . . . . 10' 10" Length . . . . . . . . . . . . . . . . . 27' 9" Fin Height (Maximum with Nose Gear Depressed and Rotating Beacon Installed on Fin) • . 9' 9" Track Width . . . . 8' 2-1/2" BATTERY LOCATION 210 . 210A ..•... 1-2 . Under Baggage Compartment Floor . Under Pilot's Seat

I MODEL 210B AND 210C DESIGN GROSS WEIGHT FUEL CAPACITY (Total) Standard ..... . Optional ..... . OIL CAPACITY . . . . . . . . . . . . . . . . . ENGINE MODEL (Refer to Section 12 for Engine Data) PROPELLER (Constant Speed) . . . . . . . . . LANDING GEAR (Retractable Hydraulic Actuated) MAIN WHEEL TIRES Pressure ... NOSE WHEEL TIRES Pressure ... NOSE GEAR STRUT PRESSURE (Strut Extended). WHEEL ALIGNMENT Camber ... . Toe-in ... . AILERON TRAVEL Up ..... . Down . . . . . . . . . . . . .. WING FLAP TRAVEL (Hydraulic Actuated) . . . . . . RUDDER TRAVEL (Measured perpendicular to hinge line) Right . . . . . . Left ..... . ELEVATOR TRAVEL Up ...... . Down ..... . ELEVATOR TRIM TAB TRAVEL Up ....... . Down .• ..... PRINCIPAL DIMENSIONS Wing Span .... . Tail Span .... . Length ................... . Fin Height (Maximum with Nose Gear Depressed and Rotating Beacon Installed on Fin) . Track Width . . . BATTERY LOCATION . • . . . . . . . 3000 lb . 65 gal. . 84 gal. . 12 qt . CONTINENTAL I0-470-S . 82" McCAULEY . Tricycle . 6. 00 x 6, 6-ply rating . 42 psi . 5. 00 x 5, 6-ply rating . 45 psi . 95 psi . +40±1. 50 . 0° to . 06" . 20°±2° . 14°±2° . 0° to 40°, +1 °-2° . 27°13'±1° . 27°13'±1° . 26°30'±1 ° . 18° ±1 ° . 20°,+1°-0° . 20°,+1°-0° . 36' 7" . 10' 10" . 27' 9" . 9' 9" . 8' 2-1/4" . Right Side of Firewall I 1-3

DESIGN GROSS WEIGHT FUEL CAPACITY (Total) Standard ..... . Optional ......... . MODEL 210D & ON OIL CAPACITY (Detergent Only) . . . . . . . . . . ENGINE MODEL (Refer to Section 12 for Engine Data) PROPELLER (Constant Speed) . . . . . . . . . LANDING GEAR (Retractable Hydraulic Actuated) MAIN WHEEL TIRES Pressure ............... . NOSE WHEEL TIRE ............ . Pressure ............... . NOSE GEAR STRUT PRESSURE (Strut Extended). WHEEL ALIGNMENT Camber ... . Toe-in ... . AILERON TRAVEL Up ..... . Down ............... . WING FLAP TRAVEL (Electrically Actuated) . . . . . RUDDER TRAVEL (Measured perpendicular to hinge line) Right ..... . Left ...... . ELEVATOR TRAVEL Up ...... . Down ..... . ELEVATOR TRIM TAB TRAVEL Up ....... . Down ...... . PRINCIPAL DIMENSIONS Wing Span .... . Tail Span .... . Length ..... . Fin Height (Maximum with Nose Gear Depressed and Rotating . 3100 lb . 65 gal. . 84 gal. . 12 qt . CONTINENTAL I0-520-A . 82" McCAULEY . Tricycle . 6. 00 x 6, 6-ply rating . 42 psi . 5. 00 x 5, 6-ply rating . 45 psi . 95 psi . 0" to . 06" . 21 °±2° . 14°30'±2° . 0°tO 40°' +1 °-2° . 27°13'±1 ° . 27°13'±1 ° . 26°30'±1° . 18° ±1° . 20°' +1 °-0 . 10°, +1°-0° . 36' 7" . 11' 8" • 27' 9" Beacon Installed on Fin) . • 9' 9" Track Width . . . . 8' 2-1/4" BATTERY LOCATION. . . . . . . . . . . . . . . . . . . . . Right Side of Firewall 1-4 ----···-·-

1960-1965 Cessna 200 Series 205 206 210 Service & Repair Manual

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