TCDS A23EU

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 Rev. No. 8 3 8 8 3 8 3 8 7 8 6 8 6 3 3 3 3 3 3 Page No. 20 21 22 23 24 Rev. No. 3 3 3 3 6 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A23EU Revision 8 Textron Aviation F337E F337G FT337E FT337GP F337F F337H FT337F FT337HP April 1, 2019 TYPE CERTIFICATE DATA SHEET NO. A23EU This data sheet, which is a part of Type Certificate No. A23EU, 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 Type Certificate A23EU was transferred from Reims Aviation S.A., 51 Aerodrome de Reims-Prunay, Reims, France, To Cessna Aircraft Company on December 11, 2006. Coincident with this transfer, the Federal Aviation Administration (FAA) has accepted responsibilities of State of Design for all airplanes, and State of Manufacture for airplanes manufactured after December 11, 2006 as defined by Annex 8 to the Convention on International Civil Aviation. Prior to December 11, 2006, products identified under Type Certificate A23EU were approved by the FAA in accordance with the Federal Aviation Regulation appropriate to Imported Products (FAR 21.29). Effective December 11, 2006, and after, these products are to be considered domestic products for the purpose of design certification, continued airworthiness, and administered under Federal Aviation Regulations §21.21. I. Model F337E, 4-6 PCLM (Normal Category), Approved February 23, 1970 Engine (Front) Continental IO-360-C (Rear) Continental IO-360-C * Fuel 100/130 minimum grade aviation gasoline * Engine Limits For all operations, 2800 rpm (210 b.hp.) Propeller and 1. McCauley constant speed full-feathering propeller installation Propeller Limits a. (Front) McCauley D2AF34C59/76C Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 11.7° low, 79.0° feathered. b. (Rear) McCauley D2AF34C61/L76C Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 10.8° low, 79.0° feathered. Rev. 8 Page 2 of 24 A23EU I. Model F337E (cont’d) c. (Front) McCauley D2AF34C301/76CTA-0 Diameter: not over 76 in., not under 75 in. No further reduction permitted Pitch setting at 30 in. station: 11.7° low, 79.0° feathered. d. (Rear) McCauley D2AF34C302/L76CTA-0 Diameter: not over 76 in., not under 75 in. No further reduction permitted Pitch setting at 30 in. station: 10.8° low, 79.0° feathered. e. (Front) McCauley D2AF34C306/78 CAA-0 Diameter: not over 78 in., not under 76.5 in. No further reduction permitted Pitch setting at 30 in. station: 11° low, 82° feathered. f. (Rear) McCauley D2AF34C307/L78CBA-2 Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 11° low, 80° feathered. g. (Front) Woodward hydraulic governor 210443 h. (Rear) Woodward hydraulic governor 210443 j. (Front) McCauley hydraulic governor CF 310D1/T1 or CF 310D2/T1 k. (Rear) McCauley hydraulic governor CF 310D1/T1 or CF 310D2/T1 l. (Front) Cessna spinner 1557303 (includes support and bulkhead assembly) m. (Rear) Cessna spinner 1457306 (includes support and bulkhead assembly). * Airspeed Limits Never exceed 225 mph. (195 knots) (CAS) Maximum structural cruising 190 mph. (165 knots) Flaps extended 120 mph. (104 knots) Maneuvering 155 mph. (135 knots) Landing gear extension 160 mph. (139 knots) C.G. Range (+137.4) to (+143.0) at 4440 lb. (landing gear extended) (+134.5) to (+143.0) at 3837 lb. or less. Straight line variation between points given. Landing gear retraction moment is +3318 in.-lb. Empty Weight C.G. Range None * Maximum Weight 4440 lb. takeoff and flight: 4400 lb. landing Number of Seats 4 - 6 (2 at +98.0 to +109.0); (2 at +133.0 to +142.0); 1 or 2 at +162.0 to +168.0) Maximum Baggage 365 lb. (reference weight and balance for additional information) Fuel Capacity 92.8 gal. (92 gal. usable) (2 tanks 46.4 gal. ea. at +150) See NOTE 1 for data on undrainable fuel Oil Capacity 10 qt. - front (+43.0) (7 qt. usable) (See NOTE 6) 10 qt. - rear (+207.5) (7 qt. usable) See NOTE 1 for data on undrainable oil. Rev. 8 Page 3 of 24 A23EU I. Model F337E (cont'd) Control Surface Movements Wing Flaps Inboard Down 25° +1, -2° Outboard Down 25° +1, -2° Ailerons Up 21° + 2° Down 14° 30' + 2° Elevator Up 26° + 1° Down 15°+ 1° Elevator tab Up 15° + 1° Down 15° + 1° Rudder Measured parallel to O.O.W.L. Inboard 15° + 0°, -2° Outboard 22° + 2° Measured perpendicularly to hinge line Inboard 17° + 0°, -2° Outboard 25° + 2° Serial Nos. Eligible Model F337E: F3370001 thru F3370024 II. Model FT337E, 4 - 6 PCLM (Normal Category), Approved February 23, 1970 Model FT337F, 4 - 6 PCLM (Normal Category), Approved January 4, 1971 Engines (Front) Continental TSIO-360-A (Rear) Continental TSIO-360-A * Fuel 100/130 minimum grade aviation gasoline * Engine Limits For all operations, 2800 rpm (210 b.hp.) 32 in. Hg MP (Critical altitude to 20,000 ft. in standard atmosphere) Propeller and 1. McCauley constant speed full-feathering propeller installation Propeller Limits a. (Front) McCauley D2AF34C91/76C-0 Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 12.7° low, 79.0° feathered. b. (Rear) McCauley D2AF34C61/L76C Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 11.8° low, 79.0° feathered. c. (Front) McCauley D2AF34C304/76CTA-0 Diameter: not over 76 in., not under 75 in. No further reduction permitted Pitch setting at 30 in. station: 12.7° low, 79.0° feathered. d. (Rear) McCauley D2AF34C302/L76CTA-0 Diameter: not over 76 in., not under 75 in. No further reduction permitted Pitch setting at 30 in. station: 11.8° low, 79.0° feathered. e. (Front) Woodward hydraulic governor 210443 f. (Rear) Woodward hydraulic governor 210443 g. (Front) McCauley hydraulic governor CF310D1-T1 or CF 310 D2/T1 h. (Rear) McCauley hydraulic governor CF310D1-T1 or CF 310 D2/T1 j. (Front) Cessna spinner 1557303 (includes support and bulkhead assembly) k. (Rear) Cessna spinner 1457306 (includes support and bulkhead assembly). Rev. 8 Page 4 of 24 A23EU II. Models FT337E, FT337F (cont'd) * Airspeed Limits Never exceed 228 mph. (198 knots) (CAS) Maximum structural cruising 190 mph. (165 knots) Flaps extended 120 mph. (104 knots) Maneuvering 155 mph. (135 knots) Landing gear extension 160 mph. (139 knots) C.G. Range (+134.5) to (+142.0) at 3837 lb. or less. (landing gear extended) (+138.3) to (+142.0) at 4630 lb. Straight line variation between points given. Landing gear retraction moment is +3318 in.-lb. Empty Weight C.G. Range None * Maximum Weight 4630 lb. takeoff and flight 4400 lb. landing Number of Seats 4 - 6 (2 at +98.0 to +109.0); (2 at +133.0 to +142.0); 1 or 2 at +162.0 to +168.0) Maximum Baggage 365 lb. (reference weight and balance for additional information) Fuel Capacity 92.8 gal. (92 gal. usable) (2 tanks 46.4 gal. ea. at +150) See NOTE 1 for data on undrainable fuel Oil Capacity 11 qt. - front (+43.0) (7 qt. usable) (See NOTE 6) 11 qt. - rear (+207.5) (7 qt. usable) See NOTE 1 for data on undrainable oil. Control Surface Movements Wing Flaps Inboard Down 25° +1°, -2° Outboard Down 25° +1°, -2° Ailerons Up 21° + 2° Down 14° 30' + 2° Elevator Up 26° + 1° Down 15°+ 1° Elevator tab Up 15° + 1° Down 15° + 1° Rudder Measured parallel to O.O.W.L. Inboard 15° + 0°, -2° Outboard 22° + 2° Measured perpendicular to hinge line Inboard 17° + 0°, -2° Outboard 25° + 2° Serial Nos. Eligible Model FT337E: F3370001 through F3370024 Model FT337F: F3370025 through F3370055 III. Model F337F, 4 - 6 PCLM (Normal Category), Approved January 4, 1971 Engines (Front) Continental IO-360-C (Rear) Continental IO-360-C * Fuel 100/130 minimum grade aviation gasoline (See NOTE 5) * Engine Limits For all operations, 2800 r.p.m. (210 b.hp.) Rev. 8 Page 5 of 24 A23EU III. Model F337F (cont'd) Propeller and 1. McCauley constant speed full-feathering propeller installation Propeller Limits a. (Front) McCauley D2AF34C59/76C Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 11.7° low, 79.0° feathered. b. (Rear) McCauley D2AF34C61/L76C Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 10.8° low, 79.0° feathered. c. (Front) McCauley D2AF34C301/76CTA-0 Diameter: not over 76 in., not under 75 in. No further reduction permitted Pitch setting at 30 in. station: 11.7° low, 79.0° feathered. d. (Rear) McCauley D2AF34C302/L76CTA-0 Diameter: not over 76 in., not under 75 in. No further reduction permitted Pitch setting at 30 in. station: 10.8° low, 79.0° feathered. e. (Front) McCauley D2AF34C306/78 CAA-0 Diameter: not over 78 in., not under 76.5 in. No further reduction permitted Pitch setting at 30 in. station: 11° low, 82° feathered. f. (Rear) McCauley D2AF34C307/L78CBA-2 Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 11° low, 80° feathered. g. (Front) Woodward hydraulic governor 210443 h. (Rear) Woodward hydraulic governor 210443 j. (Front) McCauley hydraulic governor CF310D1-T1 k. (Rear) McCauley hydraulic governor CF310D1-T1 l. (Front) Cessna spinner 557303 (includes support and bulkhead assembly) m. (Rear) Cessna spinner 1457306 (includes support and bulkhead assembly) * Airspeed Limits Never exceed 228 mph (198 knots) (CAS) Maximum structural cruising 190 mph (165 knots) Flaps extended 120 mph (104 knots) Maneuvering 155 mph (135 knots) Landing gear extension 160 mph (139 knots) C.G. Range (+140.0) to (+143.0) at 4630 lb. (landing gear extended) (+137.3) to (+143.0) at 4400 lb. (+134.5) to (+143.0) at 3837 lb. or less. Straight line variation between points given. Landing gear retraction moment is +3318 in.-lb. Rev. 8 Page 6 of 24 A23EU III. Model F337F (cont'd) Empty Weight C.G. Range None * Maximum Weight 4630 lb. takeoff and flight: 4400 lb. landing Number of Seats 4-6 (2 at +98.0 to +109.0); (2 at +133.0 to +142.0); (1 or 2 at +162.0 to +168.0) Maximum Baggage 365 lb. (reference weight and balance for additional information) Fuel Capacity 92.8 gal. (92 gal. usable) (2 tanks 46.4 gal. ea. at +150) See NOTE 1 for data on unusable fuel Oil Capacity 10 qt. - front (+43.0) (7 qt. usable) (See NOTE 6) 10 qt. - rear (+207.5) (7 qt. usable) See NOTE 1 for data on undrainable oil. Control Surface Movements Wing Flaps Inboard Down 25° +1°, -2° Outboard Down 25° +1°, -2° Ailerons Up 21° + 2° Down 14° 30' + 2° Elevator Up 26° + 1° Down 15° + 1° Elevator tab Up 15° + 1° Down 15° + 1° Rudder Measured parallel to O.O.W.L. Inboard 15° + 0°, -2° Outboard 22° + 2° Measured perpendicularly to hinge line Inboard 17° + 0°, -2° Outboard 25° + 2° Serial Nos. Eligible Model F337F: F3370025 thru F3370045 (1971 Model) F3370046 thru F3370055 (1972 Model) IV. Model F337G, 4 - 6 PCLM (Normal Category), Approved April 5, 1973 Engine (Front) Continental IO-360-G (Rear) Continental IO-360-G * Fuel 100/130 minimum grade aviation gasoline (See NOTE 5) * Engine Limits For all operations, 2800 rpm (210 b.hp.) Propeller and 1. McCauley constant speed, full-feathering propeller installations Propeller Limits a. S/NF3370056 thru F3370080 (Front) McCauley D2AF34C306/78 CAA-0 Diameter: not over 78 in., not under 76.5 in. No further reduction permitted Pitch setting at 30 in. station: 11° low, 82° feathered. b. S/N F3370080 and on (Front) McCauley D2AF34C310/90DEA-12 Diameter: not over 78.0 in., not under 76.5 in. No further reduction permitted Pitch setting at 30 in. station: 9.9° low, 82.0° feathered. c. (Rear) McCauley D2AF34C307/L78 CBA-2 Diameter: not over 76.0 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 11° low, 80° feathered. Rev. 8 Page 7 of 24 A23EU IV. Model F337G (cont'd) d. (Front) McCauley hydraulic governor CF310 D1/T1 or CF310 D2/T1 e. (Rear) McCauley hydraulic governor CF310 D1/T1 or CF310 D2/T1 f. (Front) Cessna spinner 1557303 (includes support and bulkhead assembly) g. (Rear) Cessna spinner 1457306 (includes support and bulkhead assembly). * Airspeed Limits S/N F3370056 thru F3370076 (CAS) Never exceed 228 m.p.h. (198 knots) Maximum structural cruising 190 m.p.h. (165 knots) Flaps extended 125 m.p.h. (108 knots) Maneuvering 155 m.p.h. (135 knots) Landing gear extension 160 m.p.h. (139 knots) Airspeed Limits S/N F3370077 and on (IAS) (See NOTE 7) Never exceed 200 KIAS Maximum structural cruising 168 KIAS Flaps extended 110 KIAS Maneuvering 137 KIAS Landing gear extension 140 KIAS C.G. Range (+140.0) to (+143.0) at 4630 lb. (landing gear extended) (+137.3) to (+143.0) at 4400 lb. (+134.5) to (+143.0) at 3837 lb. or less. Straight line variation between points given. Landing gear retraction moment is +3318 in.-lb. Empty Weight C.G. Range None * Maximum Weight 4630 lb. takeoff and flight: 4400 lb. landing Number of Seats 4-6 (2 at +98.0 to +109.0); (2 at +140.0); (1 or 2 at +170.0) Maximum Baggage 365 lb. (See weight and balance for landing instructions) Maximum baggage with restraining net - 160 lb. Fuel Capacity S/N F3370056 thru F3370076 92.8 gal. (92 gal. usable) (2 tanks 46.4 gal. ea. at +150.0) See NOTE 1 for data on unusable fuel. S/N F3370077 and on: 90.6 gal. (88 gal. usable) (2 tanks 45.3 gal. ea. at +149.0) See NOTE 1 for data on unusable fuel. Oil Capacity S/N F3370056 thru F3370063: 10 qt. - Front (+43.0) (7 qt. usable) 10 qt. - Rear (+207.5) (7 qt. usable) See NOTE 1 for data on undrainable oil. S/N F3370064 and on: 8 qt.-Front (+43.0) (5 qt. usable) 8 qt.-Rear (+207.5) (5 qt. usable) See NOTE 1 for data on undrainable oil. Rev. 8 Page 8 of 24 A23EU IV. Model F337G (cont'd) Control Surface Movements Wing Flaps Inboard Down 25° +1°, -2° Outboard Down 25° +1°, -2° Ailerons Up 21° + 2° Down 14° 30' + 2° Elevator Up 26° + 1° Down 15°+ 1° Elevator tab Up 15° + 1° Down 15° + 1° Rudder Measured parallel to O.O.W.L. Inboard 15° + 0°, -2° Outboard 22° + 2° Measured perpendicularly to hinge line Inboard 17° + 0°, -2° Outboard 25° + 2° Serial Nos. Eligible 1973 Model: F3370056 thru F3370063 1974 Model: F3370064 thru F3370071 1975 Model: F3370072 thru F3370076 1976 Model: F3370077 thru F3370079 1977 Model: F3370080 thru F3370084 V. Model FT337GP, 4 - 5 PCLM (Normal Category), Approved May 22, 1973 Engine (Front) Continental TSIO-360-C (Rear) Continental TSIO-360-C * Fuel 100/130 minimum grade aviation gasoline (See NOTE 5) * Engine Limits For all operations, 2800 rpm. (225 b.hp.) 37 in. Hg.MP Propeller and 1. McCauley constant speed, full feathering propeller installation Propeller Limits a. S/N FP33700001 through FP33700017 (Front) McCauley D2AF34C303/78CAA-0 Diameter: not over 78 in., not under 76 in. No further reduction permitted Pitch setting at 30 in. station: 12.5° low, 82.0 feathered. b. S/N FP33700018 and up (Front) McCauley D2AF34 C308/90 DEA-12 Diameter: not over 78.0 in., not under 76.5 in. No further reduction permitted Pitch setting at 30 in. station: 11.3° low, 82.3° feathered. c. (Rear) McCauley D2AF34C305/L78CBA-2 Diameter: not over 76 in., not under 74 in. No further reduction permitted Pitch setting at 30 in. station: 12.5° low, 80.0° feathered. d. S/N FP33700001 thru FP33700008 (Front) McCauley hydraulic governor CF310 D1/T1 or CF310 D2/T1 S/N FP33700009 thru FP33700017 (Front) McCauley hydraulic governor CFS310 D3/T1 S/N FP33700018 and on (Front) McCauley hydraulic governor DCFS310 D4/T5 Rev. 8 Page 9 of 24 A23EU V. Model FT337GP (cont'd) e. S/N FP33700001 thru FP33700008 (Rear) McCauley hydraulic governor CF310D1/T1 or CF310D2/T1 S/N FP33700009 thru FP33700022 (Rear) McCauley hydraulic governor DCFS310 D3/T1 S/N FP33700023 and on (Rear) McCauley hydraulic governor DCFS 310 D8/T1 f. (Front) Cessna spinner 1557303 (includes support and bulkhead assembly) g. (Rear) Cessna spinner 1457306 (includes support and bulkhead assembly) * Airspeed Limits S/N FP33700001 through FP33700015 (CAS) Never exceed 230 mph. (200 knots) Maximum structural cruising 190 mph. (165 knots) Flaps extended 125 mph. (108 knots) Maneuvering 155 mph. (135 knots) Landing gear extension 160 mph. (139 knots) Airspeed Limits (IAS) S/N FP33700016 and up (See NOTE 7 on use of IAS) Never exceed 205 KIAS Maximum structural cruising 169 KIAS Flaps extended 110 KIAS Maneuvering 139 KIAS Landing gear extension 140 KIAS C.G. Range S/N FP33700001 thru FP33700015 (landing gear extended) (+138.6) to (+142.0) at 4700 lb. (+134.5) to (+142.0) at 3837 lb. or less. Straight line variation between points given. Landing gear retraction moment is +3318 in.-lb. S/N FP33700016 and on (+137.7) to (+142.0) at 4700 lb. (+134.5) to (+142.0) at 3837 lb. or less Straight line variation between points given. Landing gear retraction moment is 3318 in. lb. Empty Weight C.G. Range None Maximum Weight 4700 lb. takeoff and flight: 4465 lb. landing Number of Seats S/N FP33700001 thru FP33700015 4-5 (2 at +98.0 to +109.0); (2 at +140.0); (1 optional at +170.0) S/N FP33700016 thru FP337000022 4-5 (2 at +98.0 to +109.0); (2 at +140.0 to +158.0); (1 optional at +170.0) Maximum Baggage 365 lb. (reference weight and balance for additional information) Rev. 8 Page 10 of 24 A23EU V. Model FT337GP (cont'd) Fuel Capacity S/N FP33700001 thru FP33700013 125 gal. (123 gal. usable) (2 tanks 62.5 gal. ea. at +150.0) See NOTE 1 for data on unusable fuel S/N FP33700014 and on 150.6 gal. (148 gal. usable) (2 tanks, 75.3 gal. ea. at +150.0) See NOTE 1 for data on unusable fuel Oil Capacity S/N FP33700001 thru FP33700008 11 qt. - front (+44.5) (7 qt. usable) (See NOTE 6) 11 qt. - rear (+205.9) (7 qt. usable) (See NOTE 6) See NOTE 1 for data on undrainable oil. S/N FP33700009 and on 9 qt. Front (+44.5) (5 qt. usable) 9 qt. Rear (+205.9) (5 qt. usable) See NOTE 1 for data on undrainable oil Control Surface Movements Wing Flaps Inboard Down 25° +1°, -2° Outboard Down 25° +1°, -2° Ailerons Up 21° + 2° Down 14° 30' + 2° Elevator Up 26° + 1° Down 15°+ 1° Elevator tab Up 15° + 1° Down 15° + 1° Rudder Measured parallel to O.O.W.L. Inboard 15° + 0°, -2° Outboard 22° + 2° Measured perpendicularly to hinge line Inboard 17° + 0°, -2° Outboard 25° + 2° Serial Nos. eligible 1973 FT337GP Model: FP33700001 thru FP33700008 1974 FT337GP Model: FP33700009 thru FP33700013 1975 FT337GP Model: FP33700014 thru FP33700015 1976 FT337GP Model: FP33700016 thru FP33700017 1977 FT337GP Model: FP33700018 thru FP33700022 VI. Model F337H, 4-6 PCLM (Normal Category), Approved March 2, 1978 Engine (Front) Continental IO-360-G (Rear) Continental IO-360-G * Fuel 100LL/100 minimum grade aviation gasoline See NOTE 5 * Engine Limits For all operations, 2800 rpm (210 b.hp.) Propeller and 1. McCauley constant speed full-feathering propeller installations Propeller Limits a. (Front) McCauley D2AF34C310/90DEA-12 Diameter: not over 78.0 in., not under 76.5 in. No further reduction permitted Pitch setting at 30 in. station: 9.9° low, 82.0° feathered. b. (Rear) McCauley D2AF34C307/L78CBA-2 Diameter: not over 76 in., not under 74.5 in. No further reduction permitted Pitch setting at 30 in. station: 11.0° low, 80.0° feathered. Rev. 8 Page 11 of 24 A23EU VI. Model F337H (cont'd) c. (Front) McCauley hydraulic governor DCF310D7/T1 d. (Rear) McCauley hydraulic governor DCF310D7/T1 e. (Front) Cessna spinner 1557303 (includes support and bulkhead assembly) f. (Rear) Cessna spinner 1457306 (includes support and bulkhead assembly). * Airspeed Limits (IAS) Never exceed 200 KIAS (See NOTE 7 on use of IAS) Maximum structural cruising 168 KIAS Flaps extended 110 KIAS Maneuvering 137 KIAS Landing gear extension 200 KIAS Landing gear operating speed 140 KIAS C.G. Range (+140.0) to (+143.0) at 4630 lb. (landing gear extended) (+137.3) to (+143.0) at 4400 lb. (+134.5) to (+143.0) at 3837 lb. or less. Straight line variation between points given. Landing gear retraction moment is +3318 in.-lb. Empty Weight C.G. Range None * Maximum Weights 4630 lb. takeoff and flight 4400 lb. landing Number of Seats 4-6 (2 at +98.0 to +109.0); (2 at +135.0 to +141.0); (1 or 2 at +161.0 to +167.0) Maximum Baggage 365 lb. (See weight and balance for loading instructions) Maximum baggage with restraining net - 160 lb. Fuel Capacity 90.6 gal. (88 gal. usable) (2 tanks 45.3 gal. ea. at +149.0) See NOTE 1 for data on unusable fuel Oil Capacity 8 qt. - front (+43.0) (5 qt. usable) 8 qt. - rear (+207.5) (5 qt. usable) Control Surface Movements Wing Flaps Inboard Down 25° +1°, -2° Outboard Down 25° +1°, -2° Ailerons Up 21° + 2° Down 14° 30' + 2° Elevator Up 26° + 1° Down 15°+ 1° Elevator tab Up 15° + 1° Down 15° + 1° Rudder Measured parallel to O.O.W.L. Inboard 15° + 0°, -2° Outboard 22° + 2° Measured perpendicularly to hinge line Inboard 17° + 0°, -2° Outboard 25° + 2° Serial Nos. Eligible 1978 Model: F3370085 through F3370086 Rev. 8 Page 12 of 24 A23EU VII. Model FT337HP, 4-5 PCLM (Normal Category), Approved March 2, 1978 Engine (Front) Continental TSIO-360-C (Rear) Continental TSIO-360-C * Fuel 100LL/100 minimum grade aviation gasoline See NOTE 5 * Engine Limits For all operations, 2800 rpm (225 b.hp.) 37 in. Hg. MP Propeller and 1. McCauley constant speed full feathering propeller installation Propeller Limits a. (Front) McCauley D2AF34C308/90DEA-12 Diameter: not over 78.0 in., not under 76.5 in. No further reduction permitted Pitch setting at 30 in. station: 11.3° low, 82.3° feathered. b. (Rear) McCauley D2AF34C305/L78CBA-2 Diameter: not over 76.0 in., not under 74.0 in. No further reduction permitted Pitch setting at 30 in. station: 12.5° low, 80.0° feathered. c. (Front) McCauley hydraulic governor DCFS310D7/T5 d. (Rear) McCauley hydraulic governor DCFS310D8/T1 e. (Front) Cessna spinner 1557303 (includes support and bulkhead assembly) f. (Rear) Cessna spinner 1457306 (includes support and bulkhead assembly). * Airspeed Limits (IAS) Never exceed 205 KIAS (See NOTE 7 on use of IAS) Maximum structural cruising 169 KIAS Flaps extended 110 KIAS Maneuvering 139 KIAS Landing gear extended 205 KIAS Landing gear operating speed 140 KIAS C.G. Range (+137.7) to (+142.0) at 4700 lb. (landing gear extended) (+134.5) To (+142.0) at 3837 lb. or less. Straight line variation between points given. Landing gear retraction moment is +3318 in.-lb. Empty Weight C.G. Range None * Maximum Weight 4700 lb. takeoff and flight: 4465 lb. landing Number of Seats 4-5 (2 at +98.0 to +109.0); (2 at +140.0 to +158.0); (1 optional at +170)