TCDS 3A21

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 3A21 Revision 50 Textron Aviation Inc 210 210K 210A T210K 210B 210L 210C T210L 210D 210M 210E T210M 210F 210N T T210F P210N 210G T210N T T210G 210R 210H P210R T T210H T210R 210J 210-5 (205) T T210J 210-5A (205A) November 18, 2021 TYPE CERTIFICATE DATA SHEET NO. 3A21 This data sheet which is part of Type Certificate No.3A21 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 Type Certificate Holder Record Cessna Aircraft Company transferred to Textron Aviation Inc. on July 29, 2015 I. Model 210, 4 PCLM (Normal Category), Approved April 20, 1959 Engine Continental IO-470-E *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 b.hp.) Propeller and 1. (a) Hartzell HC-A2XF-1/8433-2 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13.5°, high 28.0° (b) Cessna spinner 0752006 or 2. (a) McCauley D2A36C33/90M-8 or D2A34C49/90A-8 or D2A34C58/90AT-8 Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.8°, high 25.8° (b) Cessna spinner 0752004 3. Woodward hydraulic governor 210270, 210280, 210340 or 210345 Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev.No. 50 30 30 27 47 29 47 47 47 47 47 27 47 47 47 47 40 40 44 44 Page No. 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 Rev.No. 44 30 30 27 27 50 27 29 27 27 27 27 31 31 34 36 40 48 44 44 Page No. 41 42 43 44 45 Rev.No. 44 44 46 46 46 3A21 Page 2 of 45 Rev. 50 I. Model 210 (cont’d) *Airspeed Limits (CAS) Never exceed 200 m.p.h. (174 knots) Maximum structural cruising 175 m.p.h. (152 knots) Maneuvering 130 m.p.h. (113 knots) Flaps extended 110 m.p.h. ( 96 knots) Landing gear operating speed 160 m.p.h. (139 knots) Landing gear extension speed 160 m.p.h. (139 knots) C.G. Range (Landing (+38.4) to (+46.5) at 2900 lb. Gear Extended) (+34.5) to (+46.5) at 2550 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Empty Wt. C.G. Range None *Maximum Weight 2900 lb. No. of Seats 2 (2 at +36, 2 at +70) Maximum Baggage 120 lb. (+95) Fuel Capacity 65 gal. (55 gal. usable); two 32.5 gal. tanks in wings at +48. See NOTE 1 for data on unusable fuel Oil Capacity 12 qt. (-19.4), 6 qt. usable See NOTE 1 for data on undrainable oil Control Surface Wing flaps Up 0° Down 38° +2°, -1° Movements Ailerons Up 20° ±2° Down 14° ±2° Elevator Up 26°30' ±1° Down 22° ±1° Elevator tab Up 25° +1°, -0° Down 15° +1°, -0° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0 W.L.) Serial Nos. Eligible Model 210: 618, 57001 through 57575 (1960 Model) II. Model 210A, 4 PCLM (Normal Category), Approved June 14, 1960 Engine Continental IO-470-E *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 b.hp.) Propeller and 1. (a) Hartzell HC-A2XF-1/8433-2 Propeller Limits Diameter: not over 82 in., not under 80 Pitch settings at 30 in. sta.: low 13.5°, high 28.0° (b) Cessna spinner 0752006 or 2. (a) McCauley D2A36C33/90M-8 or D2A34C49/90A-8 or D2A34C58/90AT-8 Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.8°, high 25.8° (b) Cessna spinner 0752004 3. Woodward hydraulic governor 210270, 210280, 210340, 210345 Rev. 50 Page 3 of 45 3A21 II. Model 210A (cont’d) *Airspeed Limits (CAS) Never exceed 200 m.p.h. (174 knots) Maximum structural cruising 175 m.p.h. (152 knots) Maneuvering 130 m.p.h. (113 knots) Flaps extended 110 m.p.h. ( 96 knots) Landing gear operating speed 160 m.p.h. (139 knots) Landing gear extended speed 160 m.p.h. (139 knots) C.G. Range (Landing (+38.4) to (+44.4) at 2900 lb. Gear Extended) (+33.7) to (+44.4) at 2250 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Empty Wt. C.G. Range None *Maximum Weight 2900 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage 120 lb. (+103) Fuel Capacity 65 gal. (55 gal. usable); two 32.5 gal. tanks in wings at +48. See NOTE 1 for data on unusable fuel Oil Capacity 12 qt. (-19.4), 6 qt. usable See NOTE 1 for data on undrainable oil Control Surface Wing flaps Up 0° Down 38° +2°, -1° Movements Ailerons Up 20° ±2° Down 14° ±2° Elevator Up 26°30' ±1° Down 22° ±1° Elevator tab Up 10° +2°, -0° Down 25° +2°, -0° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0. W.L.) Serial Nos. Eligible Model 210A: 616, 21057576 through 21057840 (1961 Model) III. Model 210B, 4 PCLM (Normal Category), Approved June 27, 1961 Model 210C, 4 PCLM (Normal Category), Approved June 14, 1962 Engine Continental IO-470-S *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 b.hp.) Propeller and 1. (a) Hartzell HC-A2XF-1/8433-2 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13.5°, high 28.0° (b) Cessna spinner 0752006 or 2. (a) McCauley D2A36C33/90M-8 or D2A34C49/90A-8 or D2A34C58/90AT-8 Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.8°, high 25.8° (b) Cessna spinner 0752004 3. Woodward hydraulic governor 210270, 210280, 210340, 210345, 210451, 210452 3A21 Page 4 of 45 Rev. 50 III. Model 210B, Model 210C (cont’d) *Airspeed Limits (CAS) Never exceed 225 m.p.h. (196 knots) Maximum structural cruising 190 m.p.h. (165 knots) Maneuvering 132 m.p.h. (115 knots) Flaps extended 110 m.p.h. ( 96 knots) Landing gear operating speed 160 m.p.h. (139 knots) Landing gear extended speed 160 m.p.h. (139 knots) C.G. Range (Landing (+39.2) to (+45.0) at 3000 lb. Gear Extended) (+33.0) to (+45.0) at 2250 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Empty Wt. C.G. Range None *Maximum Weight 3000 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage 120 lb. (+103) Fuel Capacity 65 gal. (63.4 gal. usable); two 32.5 gal. tanks in wings at +48. See NOTE 1 for data on unusable fuel Oil Capacity 12 qt. (-19.4), 6 qt. usable. See NOTE 1 for data on undrainable oil Control Surface Wing flaps Up 0° Down 40° +1°, -2° Movements Ailerons Up 20° ±2° Down 14° ±2° Elevator Up 26°30' ±1° Down 18° ±1° Elevator tab Up 20° +1°, -0° Down 20° +1°, -0° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0 W.L.) Serial Nos. Eligible Model 210B: 21057841 through 21058085 (1962 Model) Model 210C: 21058086 through 21058139 and 21058141 through 21058220 (1963 Model) IV. Model 210-5 (205), 6 PCLM (Normal Category), Approved June 14, 1962 Model 210-5A (205A), 6 PCLM (Normal Category), Approved July 19, 1963 Engine Continental IO-470-S *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 b.hp.) Propeller and 1. (a) Ha rtzell HC-A2XF-1A13.5/8433-2 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: low 13.5°, high 28.0° (b) Cessna spinner 0752614 or 2. (a) McCauley D2A36C33/90M-8 or D2A34C49/90A-8 or D2A34C58/90AT-8 Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.8°, high 25.8° (b) Cessna spinner 0752614 3. Woodward hydraulic governor 210270, 210280, 210340, 210345, 210451, 210452 Rev. 50 Page 5 of 45 3A21 IV. Model 210-5 (205), Model 210-5A (205A) (cont’d) *Airspeed Limits (CAS) Never exceed 210 m.p.h (182 knots) Maximum structural cruising 170 m.p.h. (148 knots) Maneuvering 138 m.p.h. (120 knots) Flaps extended 110 m.p.h. ( 96 knots) C.G. Range (Landing (+40.5) to (+47.4) at 3300 lb. Gear Extended) (+33.0) to (+47.4) at 2250 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight 3300 lb. No. of Seats 6 (2 at +36, 2 at +69, 2 at +100) Maximum Baggage Reference weight and balance data Fuel Capacity 65 gal. (63.4 gal. usable); two 32.5 gal. tanks in wings at +48. See NOTE 1 for data on unusable fuel. Oil Capacity 12 qt. (-19.4), 6 qt. usable. See NOTE 1 for data on undrainable oil. Control Surface Wing flaps Up 0° Down 40° +1°, -2° Movements Ailerons Up 20° ±2° Down 14° ±2° Elevator Up 26°30' ±1° Down 18° ±1° Elevator tab Up 20° +1°, -0° Down 20° +1°, -0° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0. W.L.) Serial Nos. Eligible Model 210-5 (205) : 641, 205-0001 through 205-0480 (1963 Model) Model 210-5A (205A) : 205-0481 through 205-0577 (1964 Model) V. Model 210D, 4 PCLM (Normal Category), Approved July 19, 1963 Engine Continental IO-520-A *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2700 r.p.m. (285 b.hp.) Propeller and 1. (a) McCauley D2A34C58/90AT-8 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.3°, high 25.8° (b) Cessna spinner 0752004 (c) Woodward hydraulic governor D210452 2. McCauley constant speed propeller installation (with incorporation of Cessna Service Kit SK210-171) (a) McCauley D2A37C230 hub with 90REB-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: Low 12.8°, high 28.3° (b) Cessna spinner 0752004-2 (c) Woodward hydraulic governor D210452 3A21 Page 6 of 45 Rev. 50 V. Model 210D (cont’d) *Airspeed Limits (CAS) Never exceed 225 mph. (196 knots) Maximum structural cruising 190 mph. (165 knots) Maneuvering 134 mph. (116 knots) Flaps extended 110 mph. ( 96 knots) Landing gear operating speed 160 mph. (139 knots) Landing gear extended speed 160 mph. (139 knots) C.G. Range (Landing (+39.2) to (+46.6) at 3100 lb. Gear Extended) (+33.0) to (+46.6) at 2250 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Empty Wt. C.G. Range None *Maximum Weight 3100 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage Reference weight and balance data Fuel Capacity 65 gal. (63.4 gal. usable); two 32.5 gal. tanks in wings at +48. See Note 1 for data on unusable fuel. Oil Capacity 12 qt. (-19.4), 6 qt. usable. See Note 1 for data on undrainable oil. Control Surface Wing flaps Up 0° Down 40° +1°, -2° Movements Ailerons Up 21° ±2° Down 14°30' ±2° Elevator Up 26°30' ±1° Down 18° ±1° Elevator tab Up 20° +1°, -0° Down 10° +1°, -0° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0. W.L.) Serial Nos. Eligible Model 210D: 21058221 through 21058510 (1964 Model) VI. Model 210E, 4 PCLM (Normal Category), Approved September 17, 1964 Engine Continental IO-520-A *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2700 rpm. (285 b.hp.) Propeller and 1. (a) McCauley E2A34C64/90AT-8 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.3°, high 25.8° (b) Cessna spinner 1250411 (c) Woodward hydraulic governor D210452 2. (a) McCauley E2A34C73/90AT-8 Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.3°, high 25.8° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor D210452 Rev. 50 Page 7 of 45 3A21 VI. Model 210E (cont’d) Propeller and 3. McCauley constant speed propeller installation (with Propeller Limits (cont’d) incor poration of Cessna Service Kit SK210-171) (a) McCauley E2A37C233 hub with 90REB-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: Low 12.8°, high 28.3° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor D210452 *Airspeed Limits (CAS) Never exceed 225 mph. (196 knots) Maximum structural cruising 190 mph. (165 knots) Maneuvering 134 mph. (116 knots) Flaps extended 110 mph. ( 96 knots) Landing gear operating speed 160 mph. (139 knots) Landing gear extended speed 160 mph. (139 knots) C.G. Range (Landing (+39.2) to (+46.6) at 3100 lb. Gear Extended) (+33.0) to (+46.6) at 2250 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Empty Wt. C.G. Range None *Maximum Weight 3100 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage Reference weight and balance data Fuel Capacity 65 gal. (63.4 gal. usable); two 32.5 gal. tanks in wings at +48. See Note 1 for data on unusable fuel. Oil Capacity 12 qt. (-19.5), 6 qt. usable See Note 1 for data on undrainable oil. Control Surface Wing flaps Up 0° Down 40° +1°, -2° Movements Ailerons Up 21° ±2° Down 14°30' ±2° Elevator Up 26°30' ±1° Down 18° ±1° Elevator tab Up 20° +1°, -0° Down 10° +1°, -0° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0. W.L.) Serial Nos. Eligible Model 210E: 21058511 through 21058715 (1965 Model) VII. Model T210F, 4 PCLM (Normal Category), Approved August 3, 1965 Engine Continental TSIO-520-C *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2700 r.p.m., 32.5 in. Hg. mp. (285 b.hp.) Propeller and 1. (a) McCauley E2A34C70/90AT-8 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 11.8°, high 32.0° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor G210452 3A21 Page 8 of 45 Rev. 50 VII. Model T210F (cont’d) Propeller and Propeller Limits (cont’d) *Airspeed Limits (CAS) C.G. Range (Landing Gear Extended) Empty Wt. C.G. Range *Maximum Weight No. of Seats Maximum Baggage Fuel Capacity Oil Capacity Control Surface Movements Serial Nos. eligible 2. (a) McCauley D3A32C77/82NK-2 Diameter: not over 80 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.2°, high 32.5° (b) Cessna spinner 1250419-2 (c) Woodward hydraulic governor G210452 3. (a) McCauley D3A32C88/82NC-2 Diameter: not over 80 in., not under 78 in. Pitch settings at 30 in. sta.: low 14.0°, high 33.0° (b) Cessna spinner 1250419-2 (c) Woodward hydraulic governor G210452 4. McCauley constant speed propeller installation (with incorporation of Cessna Service Kit SK210-171) (a) McCauley E2A37C234 hub with 90REC-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: Low 14.3°, high 34.5° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor G210452 Never exceed 225 mph. (196 knots) Maximum structural cruising 190 mph. (165 knots) Maneuvering 131 mph. (114 knots) Flaps extended 110 mph ( 96 knots) Landing gear operating speed 160 mph. 139 knots) Landing gear extended speed 160 mph. (139 knots) (+39.0) to (+46.6) at 3300 lb. (+33.0) to (+46.6) at 2480 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) None 3300 lb. 4 (2 at +36, 2 at +70) Reference weight and balance data 65 gal. (63 gal. usable); two 32.5 gal. tanks in wings at +48. See Note 1 for data on unusable fuel. 12 qt. (-19.4), 6 qt. usable. See Note 1 for data on undrainable oil. Wing flaps Up 0° Down 40° +1°, -2° Ailerons Up 21° ±2° Down 14°30' ±2° Elevator Up 26°30' ±1° Down 18° ±1° Elevator tab Up 20° ±1° Down 20° ±1° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0. W.L.) Model T210F: T210-0001 through T210-0197 (1966 Model) Rev. 50 Page 9 of 45 3A21 VIII. Model 210F, 4 PCLM (Normal Category), Approved August 3, 1965 Engine Continental IO-520-A *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2700 rpm. (285 b.hp.) Propeller and 1. (a) McCauley E2A34C73/90AT-8 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.3°, high 25.8° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor D210452 2. (a) McCauley D3A32C77/82NK-2 Diameter: not over 80 in., not under 78 in. Pitch settings at 30 in. sta.: low 11.3°, high 27.6° (b) Cessna spinner 1250419-2 (c) Woodward hydraulic governor D210452 3. (a) McCauley D3A32C88/82NC-2 Diameter: not over 80 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.8°, high 28.1° (b) Cessna spinner 1250419-2 (c) Woodward hydraulic governor D210452 4. McCauley constant speed propeller installation (with incorporation of Cessna Service Kit SK210-171) (a) McCauley E2A37C233 hub with 90REB-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: Low 12.8°, high 28.3° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor D210452 *Airspeed Limits (CAS) Never exceed 225 mph. (196 knots) Maximum structural cruising 190 mph. (165 knots) Maneuvering 131 mph (114 knots) Flaps extended 110 mph ( 96 knots) Landing gear operating speed 160 mph (139 knots) Landing gear extended speed 160 mph. (139 knots) C.G. Range (Landing (+39.0) to (+46.6) at 3300 lb. Gear Extended) (+33.0) to (+46.6) at 2400 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Empty Wt. C.G. Range None *Maximum Weight 3300 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage Reference weight and balance data Fuel Capacity 65 gal. (63 gal. usable), two 32.5 gal. tanks in wings at +48. See NOTE 1 for data on unusable fuel. Oil Capacity 12 qt. (-19.4), 6 qt. usable See NOTE 1 for data on undrainable oil. 3A21 Page 10 of 45 Rev. 50 VIII. Model 210F (cont’d) Control Surface Wing flaps Up 0° Down 40° +1°, -2° Movements Ailerons Up 21° ±2 Down 14°30' ±2° Elevator Up 26°30' ±1° Down 18° ±1° Elevator tab Up 20° ±1° Down 20° ±1° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0. W.L.) Serial Nos. Eligible Model 210F: 21058716 through 21058818 (1966 Model) IX. Model T210G, 4 PCLM (Normal Category), Approved August 23, 1966 Model T210H, 4 PCLM (Normal Category), Approved August 16, 1967 Engine Continental TSIO-520-C *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2700 rpm., 32.5 in. Hg. mp. (285 b.hp.) Propeller and 1. (a) McCauley E2A34C70/90AT-8 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 11.8°, high 32.0° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor G210452 (d) McCauley hydraulic governor C290D2/T2 or C290D4/T2 2. (a) McCauley D3A32C88/82NC-2 Diameter: not over 80 in., not under 78 in. Pitch settings at 30 in. sta.: low 14.0°, high 33.0° (b) Cessna spinner 1250419-2 (c) Woodward hydraulic governor G210452 (d) McCauley hydraulic governor C219D2/T2 or C290D4/T2 3. (a) McCauley D3A32C77/82NK-2 (T-210G Only) Diameter: not over 80 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.2°, high 32.5° (b) Cessna spinner 1250419-2 (c) Woodward hydraulic governor G210452 4. McCauley constant speed propeller installation (with incorporation of Cessna Service Kit SK210-171) (a) McCauley E2A37C234 hub with 90REC-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: Low 14.3°, high 34.5° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor G210452 *Airspeed Limits (CAS) Never exceed 225 mph. (196 knots) Maximum structural cruising 190 mph (165 knots) Maneuvering 135 mph. (117 knots) Flaps extended 110 mph. ( 96 knots) Landing gear operating speed 160 mph. (139 knots) Landing gear extended speed 160 mph. (139 knots) C.G. Range (Landing (+39.7) to (+47.8) at 3400 lb. Gear Extended) (+35.5) to (+47.8) at 2800 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Rev. 50 Page 11 of 45 3A21 IX. Model T210G, Model T210H (cont’d) Empty Wt. C.G. Range None *Maximum Weight 3400 lbs. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage Reference weight and balance data. Fuel Capacity 90 gal. (89 gal. usable), two 45.0 gal. tanks in wings at +43. See Note 1 for data on unusable fuel Oil Capacity 12 qt. (-19.4), 6 qt. usable. See Note 1 for data on undrainable oil Control Surface Wing flaps Up 0° Down 30° Movements Ailerons Up 20° ±2° Down 15° ±2° Elevator Up 23° ±1° Down 15° ±1° Elevator tab Up 20° ±1° Down 5° ±1° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0. W.L.) Serial Nos. Eligible Model T210G: T210-0198 through T210-0307 (1967 Model) Model T210H: T210-0308 through T210-0392 (1968 Model) X. Model 210G, 4 PCLM (Normal Category), Approved August 23, 1966 Model 210H, 4 PCLM (Normal Category), Approved August 16, 1967 Engine Continental IO-520-A *Fuel 100/130 minimum grade aviation gasoline *Engine Limits For all operations, 2700 rpm. (285 b.hp.) Propeller and 1. (a) McCauley E2A34C73/90AT-8 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 10.3°, high 25.8° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor D210452 (d) McCauley hydraulic governor C290D2/T5 or C290D3/T5 2. (a) McCauley D3A32C88/82NC-2 Diameter: not over 80 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.8°, high 28.1° (b) Cessna spinner 1250419-2 (c) Woodward hydraulic governor D210452 (d) McCauley hydraulic governor C290D2/T5 or C290D3/T5 3. McCauley constant speed propeller installation (with incorporation of Cessna Service Kit SK210-171) (a) McCauley E2A37C233 hub with 90REB-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: Low 12.8°, high 28.3° (b) Cessna spinner 1250415 (c) McCauley hydraulic governor C290D2/T5 or C290D3/T5 3A21 Page 12 of 45 Rev. 50 X. Model 210G, Model 210H (cont’d) *Airspeed limits (CAS) Never exceed 225 mph (196 knots) Maximum structural cruising 190 mph (165 knots) Maneuvering 135 mph. (117 knots) Flaps extended 110 mph. ( 96 knots) Landing gear operating speed 160 mph. (139 knots) Landing gear extended speed 160 mph. (139 knots) C.G. Range (Landing (+39.7) to (+47.8) at 3400 lb. Gear Extended) (+35.5) to (+47.8) at 2800 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Empty wt. C.G. Range None *Maximum Weight 3400 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage Reference weight and balance data Fuel Capacity 90 gal. (89 gal. usable); two 45.0 gal. tanks in wings at +43. See Note 1 for data on unusable fuel. Oil Capacity 12 qt. (-19.4); 6 qt. usable See Note 1 for data on undrainable oil. Control Surface Wing flaps Up 0° Down 30° Movements Ailerons Up 20° ±2° Down 15° ±2° Elevator Up 23° ±1° Down 15° ±1° Elevator tab Up 20° ±1° Down 5° ±1° Rudder Right 24° ±1° Left 24° ±1° (measured parallel to 0.0. W.L.) Serial Nos. Eligible Model 210G: 21058819 through 21058936 (1967 Model) Model 210H: 21058937 through 21059061 (1968 Model) XI. Model T210J, 4 PCLM (Normal Category), Approved July 17, 1968 Engine Continental TSIO-520-H *Fuel 100/130 minimum grade aviation gasoline *Engine limits For all operations, 2700 rpm., 32.5 in. Hg. mp. (285 b.hp.) Propeller and 1. (a) McCauley E2A34C70/90AT-8 Propeller Limits Diameter: not over 82 in., not under 80 in. Pitch settings at 36 in. sta.: low 11.8°, high 32.0° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor G210452 (d) McCauley hydraulic governor C290D2/T2 or C290D4/T2 2. (a) McCauley D3A32C88/82NC-2 Diameter: not over 80 in., not under 78 in. Pitch settings at 30 in. sta.: low 14.0°, high 33.0° (b) Cessna spinner 1250419-2 (c) Woodward hydraulic governor G210452 (d) McCauley hydraulic governor C219D2/T2 or C290D4/T2 Rev. 50 Page 13 of 45 3A21 XI. Model T210J (cont’d) Propeller and 3. McCauley constant speed propeller installation (with Propeller Limits (cont’d) incor poration of Cessna Service Kit SK210-171) (a) McCauley E2A37C234 hub with 90REC-8 blades Diameter: not over 82 in., not under 80 in. Pitch settings at 30 in. sta.: Low 14.3°, high 34.5° (b) Cessna spinner 1250415 (c) Woodward hydraulic governor G210452 (d) McCauley hydraulic governor C219D2/T2 or C219D4/T2 Airspeed Limits (CAS) Never exceed 225 mph. (196 knots) Maximum structural cruising 90 mph. (165 knots) Maneuvering 135 mph (117 knots) Flaps extended 110 mph. ( 96 knots) Landing gear operating speed 160 mph (139 knots) Landing gear extended speed 160 mph (139 knots) C.G. Range (Landing (+39.7) to (+47.8) at 3400 lb. Gear Extended) (+35.5) to (+47.8) at 2800 lb. or less Straight line variation between points given. Moment change due to retracting landing gear (+2456 in.-lb.) Empty wt. C.G. Range None *Maximum Weight 3400 lb. No. of Seats 4 (2 at +36, 2 at +70) Maximum Baggage Reference weight and balance data. Fuel Capacity 90 gal. (89 gal. usable), two 45.0 gal. tanks in wings at +43. See Note 1 for data on unusable fuel. Oil Capacity 10 qt. (-12.5), 8 qt. usable