TCDS 3A10

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 Rev. No. 64 61 50 61 61 61 50 61 61 58 61 61 61 50 61 61 61 Page No. 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 Rev. No. 61 61 62 61 61 61 61 50 61 61 61 61 61 61 61 61 61 Page No. 35 36 37 38 39 40 41 42 43 44 Rev. No. 61 64 61 61 61 61 61 61 63 63 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 3A10 Revision 64 Textron Aviation 310 310J 310A (USAF U-3A) 310J-1 310B E310J 310C 310 K 310D 310L 310E (USAF U-3B) 310N 310F 310P 310G T310P 310H 310Q E310H T310Q 310I 310R T310R May 9, 2024 TYPE CERTIFICATE DATA SHEET NO. 3A10 This data sheet which is part of Type Certificate No. 3A10 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, KS 67215 Type Certificate Holder Record Cessna Aircraft Company transferred to Textron Aviation Inc. on July 29, 2015 I. Model 310 (Normal Categor y), Approved March 22, 1954 Engines 2 Continental O-470-B or O-470-M (installed per Cessna Dwg. 0850000, 0951560, 0851000 and 0851755) *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (240 hp.) Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartzell hub HC82XF or HC-A2XF-2 with 68 lbs. ea. (-25) 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: low 12.5°, high 22.0°, feathered 82.0° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Hartzell C- 888 dome with 4 lbs. ea. (-23) C-807-1 bulkhead or Cessna 0752006 dome with 0850300 bulkhead or Cessna 0850311 dome with 0850300 bulkhead or Cessna 0850313 dome with 0850300 bulkhead 3A10 2 Rev. 64 I. Model 310 (cont’d) *Airspeed Limits Maneuvering 159 m.p.h. (138 knots) (TIAS) Maximum structural cruising 200 m.p.h. (173 knots) Never exceed 246 m.p.h. (214 knots) Flaps extended 130 m.p.h. (113 knots) Landing gear extended 130 m.p.h. (113 knots) *C.G. Range (Landing (+36. 0) to (+41.5) at 4600 lbs. Gear Extended) (+33.9) to (+42.1) at 4240 lbs. (+32.0) to (+42.1) at 3900 lbs. or less Straight line variation between points given Empty Wt. C.G. Range None *Maximum Weight 4600 lbs. No. of Seats 5 (Std.) (2 at +37, 3 at +71). See Manufacturer's Weight and Balance data sheet for optional seating arrangements. Maximum Baggage 200 lbs. (+96) (See NOTE 2G for placard). Anti-Icing Fluid Capacity 4-1/2 qt. (7 lbs. at +47) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35) (See NOTE 1 for data on system fuel) Oil Capacity 24 qt. (12 qt. in each engine at (0), 6 qt. unusable per engine) (See NOTE 1 for data on system oil) Control Surface Wing flaps Down 45° Movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 20° Down 28° Rudder Right 20° Left 26° Serial Nos. Eligible 35000 through 35546. Delegation Option Manufacturer No. CE-1 authorized to issue airworthiness certificates for S/N 35216 through 35546 and approve repairs and alterations of airplanes S/N 35000 through 35546 under delegation option provisions of Part 21 of the Federal Aviation Regulations (FAR). II. Model 310A (USAF U-3A) (Normal Category), Approved April 9, 1957 Engines 2 Continental O-470-M *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (240 hp.) Rev. 64 3 3A10 II. Model 310A (cont’d) Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartzell hub HC82XF-2 or HC-A2XF-2 with 68 lbs. ea. (-25) 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: low 12.5°, high 22.0°, feathered 82.0° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Hartzell C-888 dome with 4 lbs. ea. (-23) C-807-1 bulkhead or Cessna 0752006 dome with 0850300 bulkhead or Cessna 0850311 dome with 0850300 bulkhead or Cessna 0850313 dome with 0850300 bulkhead *Airspeed Limits Maneuvering 164 m.p.h. (143 knots) (TIAS) Maximum structural cruising 200 m.p.h. (173 knots) Never exceed 248 m.p.h. (215 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (Landing (+37. 3) to (+42.1) at 4830 lbs. Gear Extended) (+32.0) to (+42.1) at 3900 lbs. or less Straight line variation between points given Empty Wt. C.G. Range None *Maximum Weight Landing 4600 lbs., takeoff 4830 lbs. No. of Seats 5 (Std.) (2 at +37, 3 at +71). See Manufacturer's Weight and Balance data sheet for optional seating arrangements. Maximum Baggage 200 lbs. (+96) (See NOTE 2G for placard). Anti-Icing Fluid Capacity 4-1/2 qt. (7 lbs.) (+47) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) (See NOTE 1 for data on unusable fuel) Oil Capacity 24 qt. (12 qt. in each engine at (0); 6 qt. unusable per engine) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps Down 45° Movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 20° Down 28° Rudder Right 20° Left 26° Serial Nos. Eligible 38001 through 38161. Production Certificate No. 4 effective. Prior to civil certification U-3A airplanes must be modified in accordance with Cessna Dwg. 0800203 or Service Kit SK310-85, which may be obtained from the manufacturer. An Federal Aviation Agency (FAA) representative upon determination of compliance with the above-mentioned modification drawing may issue an airworthiness certificate. 3A10 4 Rev. 64 III. Model 310B (Normal Category), Approved May 23, 1957 Engines 2 Continental O-470-M *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2600 r.p.m. (240 hp.) Propeller and 1. 2 full-featheri ng propeller installations Propeller Limits a. Hartzell hub HC82XF-2 or HC-A2XF-2 with 68 lbs. ea. (-25) 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: low 12.5°, high 22.0°, feathered 82.0° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Hartzell C- 888 dome with 4 lbs. ea. (-23) C-807-1 bulkhead or Cessna 0752006 dome with 0850300 bulkhead or Cessna 0850311 dome with 0850300 bulkhead or Cessna 0850313 dome with 0850300 bulkhead *Airspeed Limits Maneuvering 164 m.p.h. (143 knots) (TIAS) Maximum structural cruising 200 m.p.h. (173 knots) Never exceed 248 m.p.h. (215 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (Landing (+36. 6) to (+42.1) at 4700 lbs. Gear Extended) (+32.0) to (+42.1) at 3900 lbs. or less Straight line variation between points given Empty Wt. C.G. Range None *Maximum Weight Landing 4600 lbs., takeoff 4700 lbs. No. of Seats 5 (Std.) (2 at +37, 3 at +71). See Manufacturer's Weight and Balance data sheet for optional seating arrangements. Maximum Baggage 200 lbs. (+96) (See NOTE 2G for placard). Anti-Icing Fluid Capacity 4-1/2 qt. (7 lbs.) (+47) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) (See NOTE 1 for data on unusable fuel) Oil Capacity 24 qt. (12 qt. in each engine at (0), 6 qt. unusable per engine) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps Down 45° Movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 20° Down 28° Rudder Right 20° Left 26° Rev. 64 5 3A10 III. Model 310B (cont’d) Serial Nos. Eligible 607, 35547, 35548, 35549, 35551 through 35771. Production Certificate No. 4 effective. IV. Model 310C (Normal Category ), Approved October 22, 1958 Engines 2 Continental IO-470-D *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 hp.) Propeller and 1. 2 full-feathering 2-bladed propeller installations Propeller Limits a. Hartzell hub HC82XF-2 or HC-A2XF-2 with 68 lbs. ea. (-25) 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.5°, high 22.0°, feathered 82.0° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Hartzell C- 888 dome with 4 lbs. ea. (-23) C-807-1 bulkhead or Cessna 0752006 dome with 0850300 bulkhead or Cessna 0850311 dome with 0850300 bulkhead or Cessna 0850313 dome with 0850300 bulkhead 2. 2 full feathering propeller installations a. McCauley hub D2AF36C48 with 90MF-10 blades 68 lbs. ea. (-25) Diameter: not over 80 in., not under 78 in. Pitch settings at 36 in. sta.: low 11°, feathered 77° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, McCauley Model D2840 4 lbs. ea. (-23) with D2878 bulkhead or Cessna 0850258 spinner with Cessna 0850257 bulkhead *Airspeed Limits Maneuvering 164 m.p.h. (143 knots) (TIAS) Maximum structural cruising 210 m.p.h. (183 knots) Never exceed 248 m.p.h. (215 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (Landing (+37. 3) to (+42.1) at 4830 lbs. Gear Extended) (+32.0) to (+42.1) at 3900 lbs. or less Straight line variation between points given Empty Wt. C.G. Range None *Maximum Weight Landing 4600 lbs., takeoff 4830 lbs. 3A10 6 Rev. 64 IV. Model 310C (cont’d) No. of Seats 5 (Std.) (2 at +37, 3 at +71). See Manufacturer's Weight and Balance data sheet for optional seating arrangements. Maximum Baggage 200 lb. (+96) (See NOTE 2G for placard). Anti-Icing Fluid Capacity 4-1/2 qt. (7 lbs.) (+47) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) (See NOTE 1 for data on unusable fuel) Oil Capacity 24 qt. (12 qt. in each engine at (-3.5), 6 qt. unusable per engine) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps Down 45° Movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 26° Rudder Right 0° Left 26° Serial Nos. Eligible 35550, 35772 through 35999, 39001 through 39031. Production Certificate No. 4 effective. V. Model 310D (Normal Category), Approved July 8, 1959 Engines 2 Continental IO-470-D *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 hp.) Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartzell hub HC82XF-2 or HC-A2XF-2 with 68 lbs. ea. (-25) 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.5°, high 22.0°, feathered 82.0° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Hartzell C- 888 dome with 4 lbs. ea. (-23) C-807-1 bulkhead or Cessna 0752006 dome with 0850300 bulkhead or Cessna 0850311 dome with 0850300 bulkhead or Cessna 0850313 dome with 0850300 bulkhead Rev. 64 7 3A10 V. Model 310D (cont’d) Propeller and 2. 2 full-feat hering propeller installations Propeller Limits (cont’d) a. McCauley hub D2AF 36C48 with 90MF-10 blades 68 lbs. ea. (-25) Diameter: not over 80 in., not under 78 in. Pitch settings at 36 in. sta.: low 11°, feathered 77° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or G210355 McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, McCauley Model D2840 4 lbs. ea. (-23) with D2878 bulkhead or Cessna 0850258 spinner with Cessna 0850257 bulkhead *Airspeed Limits Maneuvering 164 m.p.h. (143 knots) (TIAS) Maximum structural cruising 210 m.p.h. (183 knots) Never exceed 248 m.p.h. (215 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (Landing (+37. 3) to (+42.1) at 4830 lbs. Gear Extended) (+32.0) to (+42.1) at 4060 lbs. or less Straight line variation between points given Empty Wt. C.G. Range None Maximum Weight Landing 4600 lbs., takeoff 4830 lbs. No. of Seats 5 (Std.) (2 at +37, 3 at +71). See Manufacturer's Weight and Balance data sheet for optional seating arrangements. Maximum Baggage 200 lbs. (+96) (See NOTE 2G for placard). Anti-Icing Fluid Capacity 4-1/2 qt. (7 lbs.) (+47) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) (See NOTE 1 for data on unusable fuel) Oil Capacity 24 qt. (12 qt. in each engine at (-3.5), unusable 6 qt. per engine) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps Down 45° Movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° (Parallel to W.L.) Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 26° Rudder Right 17° Left 22° (Parallel to W.L.) Serial Nos. Eligible 39032 through 39264. Production Certificate No. 4 effective. Prior to original certification of S/N 39265 through 39299, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. 3A10 8 Rev. 64 VI. Model 310E (USAF U-3B) (Normal Category), Approved September 21, 1959 Engines 2 Continental IO-470-D *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 hp.) Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartzell hub HC82XF-2 or HC-A2XF-2 with 68 lbs. ea. (-25) 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.5°, high 22.0°, feathered 82.0° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355 McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Hartzell C- 888 dome with 4 lbs. ea. (-23) C-807-1 bulkhead or Cessna 0752006 dome with 0850300 bulkhead or Cessna 0850311 dome with 0850300 bulkhead or Cessna 0850313 dome with 0850300 bulkhead 2. 2 full-feathering propeller installations a. McCauley hub D2AF36C48 with 90MF-10 blades 68 lbs. ea. (-25) Diameter: not over 80 in., not under 78 in. Pitch settings at 36 in. sta.: low 11°, feathered 77° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355 McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, McCauley Model D2840 4 lbs. ea. (-23) with D2878 bulkhead or Cessna 0850258 spinner with Cessna 0850257 bulkhead *Airspeed Limits Maneuvering 167 m.p.h. (145 knots) (TIAS) Maximum structural cruising 210 m.p.h. (183 knots) Never exceed 252 m.p.h. (218 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (Landing (+38. 3) to (+41.6) at 4990 lbs. Gear Extended) (+35.6) to (+42.1) at 4600 lbs. (+32.0) to (+42.1) at 4060 lbs. or less Straight line variation between points given Empty Wt. C.G. Range None *Maximum Weight Landing 4750 lbs., takeoff 4990 lbs. No. of Seats 5 (Std.) (2 at +37, 3 at +71). See Manufacturer's Weight and Balance data sheet for optional seating arrangements. Maximum Baggage 200 lbs. (+96) (See NOTE 2G for placard). Anti-Icing Fluid Capacity 4-1/2 qt. (7 lbs.) (+47) Rev. 64 9 3A10 VI. Model 310E (cont’d) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) (See NOTE 1 for data on unusable fuel) Oil Capacity 24 qt. (12 qt. in each engine at (-3.5), 6 qt. unusable per engine) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps Down 45° Movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° (Parallel to W.L.) Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 26° Rudder Right 17° Left 22° (Parallel to W.L.) Serial Nos. Eligible 35912A, 310M0001 through 310M0036. Production Certificate No. 4 effective. Prior to original certification U-3B airplanes must be modified in accordance with Cessna Dwg. 0800203 or Service Kit SK310-85, which may be obtained from the manufacturer. An FAA representative upon determination of compliance with the above-mentioned modification drawing may issue an airworthiness certificate. VII. Model 310F (Normal Category), Approved July 25, 1960 Engines 2 Continental IO-470-D *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 hp.) Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartzell hub HC82XF-2 or HC-A2XF-2 with 68 lbs. ea. (-25) 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.5°, high 22.0°, feathered 82.0° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290, or C210355 McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Hartzell C888 dome with 4 lbs. ea. (-23) C-807-1 bulkhead or Cessna 0752006 dome with 0850300 bulkhead or Cessna 0850311 dome with 0850300 bulkhead or Cessna 0850313 dome with 0850300 bulkhead 2. 2 full-feathering propeller installations a. McCauley hub D2AF36C48 with 90MF-10 blades 68 lbs. ea. (-25) Diameter: not over 80 in., not under 78 in. Pitch settings at 36 in. sta.: low 11°, feathered 77° 3A10 10 Rev. 64 VII. Model 310F (cont’d) Propeller and b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) Propeller Limits (cont’d) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, McCauley Model D2840 4 lbs. ea. (-23) with D2878 bulkhead or Cessna 0850258 spinner with Cessna 0850257 bulkhead *Airspeed Limits Maneuvering 164 m.p.h. (143 knots) (TIAS) Maximum structural cruising 210 m.p.h. (183 knots) Never exceed 248 m.p.h. (215 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (Landing (+37. 3) to (+42.1) at 4830 lbs. Gear Extended) (+32.0) to (+42.1) at 4060 lbs. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight Landing 4600 lbs., takeoff 4830 lbs. No. of Seats 5 (Std.) (2 at +37, 3 at +71). See Manufacturer's Weight and Balance data sheet for optional seating arrangements. Maximum Baggage 200 lbs. (+96) (See NOTE 2G for placards) Anti-Icing Fluid Capacity 4-1/2 qt. (7 lbs.) (+47) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) (See NOTE 1 for data on unusable fuel) Oil Capacity 24 qt. (12 qt. in each engine at (-3.5), 6 qt. unusable per engine) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps Down 45° Movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° (Parallel to W.L.) Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 26° Rudder Right 17° Left 22° (Parallel to W.L.) Serial Nos. Eligible 310-0001 through 310-0016, 310-0018 through 310-0156. Production Certificate No. 312 effective. Prio r to original certification of each aircraft, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. Rev. 64 11 3A10 VIII. Model 310G (Normal Category), Approved October 2, 1961 Engines 2 Continental IO-470-D *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 hp.) Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartzell hub HC82XF-2 or HC-A2XF-2 with 68 lbs. ea. (-25) 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: low 13.5°, high 22.0°, feathered 82.0° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Hartzell C- 888 dome with 4 lbs. ea. (-23) C-807-1 bulkhead or Cessna 0752006 dome with 0850300 bulkhead or Cessna 0850311 dome with 0850300 bulkhead or Cessna 0850313 dome with 0850300 bulkhead 2. 2 full-feathering propeller installations a. McCauley hub D2AF36C48 with 90MF-10 blades 68 lbs. ea. (-25) Diameter: not over 80 in., not under 78 in. Pitch settings at 36 in. sta.: low 11°, feathered 77° b. Hydraulic governor, Woodward 210105, 210155, 4 lbs. ea. (-17) 210280, 210444, A210438, 210290 or C210355, McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, McCauley M odel D2840 with 4 lbs. ea. (-23) D2878 bulkhead or Cessna 0850 spinner with Cessna 0850257 bulkhead *Airspeed Limits Maneuvering 167 m.p.h. (145 knots) (TIAS) Maximum structural cruising 210 m.p.h. (183 knots) Never exceed 252 m.p.h. (218 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (Landing (+38. 3) to (+41.6) at 4990 lbs. Gear Extended) (+35.6) to (+42.1) at 4600 lbs. (+32.0) to (+42.1) at 4060 lbs. or less Straight line variation between points given Empty Wt. C.G. Range None *Maximum Weight Landing 4750 lbs., takeoff 4990 lbs. No. of Seats 5 (Std.) (2 at +37, 3 at +71). See Manufacturer's Weight and Balance data sheet for optional seating arrangements. Maximum Baggage 200 lbs. (+96) (See NOTE 2G for placard) Anti-Icing Fluid Capacity 4-1/2 qt. (7 lb.) (+47) 3A10 12 Rev. 64 VIII. Model 310G (cont’d) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) (See NOTE 1 for data on unusable fuel) Oil Capacity 24 qt. (12 qt. in each engine at (-3.5), 6 qt. unusable per engine) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps Down 45° Movements Main surfaces Aileron Up 20° Down 20° Elevator Up 25° Down 15° Rudder Right 25° Left 25° (Parallel to W.L.) Tabs (main surface in neutral) Aileron Up 20° Down 20° Elevator Up 10° Down 26° Rudder Right 17° Left 22° (Parallel to W.L.) Serial Nos. Eligible 310G0001 through 310G0156. Production Certificate No. 312 effective. IX. Model 310H (Normal Category), Approved July 19, 1962 Engines 2 Continental IO-470-D *Fuel Grade 100 or 100LL aviation gasoline *Engine Limits For all operations, 2625 r.p.m. (260 hp.) Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartzell hub HC82XF-2 or HC-A2XF-2 68 lbs. ea. (-25) with 8433 blades Diameter: not over 84 in., not under 78 in. Pitch settings at 30 in. sta.: