TCDS 3A25

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Rev. No. 28 25 25 25 25 25 27 25 27 27 25 27 25 27 Page No. 15 16 17 18 19 20 21 22 23 24 25 26 27 Rev. No. 25 27 25 28 25 25 25 25 25 25 25 27 27 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 3A25 Revision 28 Textron Aviation 320 320F 320-1 335 320A 340 320B 340A 320C 320D 320E September 20, 2024 TYPE CERTIFICATE DATA SHEET NO. 3A25 This data sheet which is part of Type Certificate No. 3A25 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 320, Skyknight, (Norma l Category), Approved May 24, 1961 Engines Two Continental TSIO-470-B *Fuel 100/130 minimum grade aviation gasoline (See NOTE 5). *Engine Limits For all operations, 2600 rpm, 260 hp, 35 in. Hg MP Critical altitude is 16,000 ft. in standard atmosphere. Propeller and 1. Two Hartzell full-feathered, propeller: Propeller Limits Hub: HC-A2XF-2 Blade: 8433 Diameter: Not over 80 in., not unde r 78 in. (no further reduction permitted) Pitch at 30-inch station: Low pitch: 15.0° High pitch: 22.0° Feathered: 84.0°, ±2° a. Hydraulic governor: W oodward 210290, C210355, A210438, 210444. b. Propeller spinner and bulkhead assembly: Cessna 0850319-1 dome with 0850309-1 bulkhead. *Airspeed Limits Never exceed 252 m.p.h. (218 knots) (CAS) Maximum structural cruising 210 m.p.h. (183 knots) Maneuvering 167 m.p.h. (145 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) 3A25 2 Rev. 28 I. Model 320 (cont’d) *C.G. Range (+38.3) to (+41.6) at 4990 lb. (+42.1) at 4600 lb. (+32.0) to (+42.1) at 4060 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight Landing: 4750 lb. Takeoff: 4990 lb. 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) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) or 133 gal. (with 2 wing tip tanks and 2 auxiliary tanks 15.5 gal. each at +47). (See NOTE 1 for data on system fuel) Oil Capacity 6.5 gal. (3.25 gal in each engine at (-3.5), unusable 1.5 gal. per engine) (See NOTE 1 for data on system oil) Control Surface Wing flaps 45° Down Movements Main surfaces Aileron 20° Up 20° Down Elevator 25° Up 15° Down Rudder 25° Right 25° Left (Parallel to W.L.) Tab (main surface in neutral) Aileron 20° Up 20° Down Elevator 10° Up 26° Down Rudder 17° Right 22° Left (Parallel to W.L.) Serial Nos. Eligible 320-0001 thru 320-0110 II. Model 320-1, Skyknight, (Norma l Category), Approved May 10, 1962 Engines Two Continental TSIO-470-B *Fuel 100/130 minimum grade aviation gasoline (see NOTE 5). *Engine Limits For all operations, 2600 rpm, 260 hp, 35 in. Hg MP Critical altitude is 16,000 ft. in standard atmosphere. Propeller and 1. Two Hartzell full-feathered, propeller: Propeller Limits Hub: HC-A2XF-2 Blade: 8433 Diameter: Not over 80 in., not unde r 78 in. (no further reduction permitted) Pitch at 30-inch station: Low pitch: 15.0° High pitch: 22.0° Feathered: 84.0°, ±1° a. Hydraulic governor: 1) Woodward 210280, C210355, A210438, 210444. 2) McCauley DCFU290D1/T2, DCFU290D2/T2. b. Propeller spinner and bulkhead assembly: Cessna 0850319-1 dome with 0850309-1 bulkhead. Rev. 28 3 3A25 II. Model 320-1 (cont’d) *Airspeed Limits Never exceed 257 m.p.h. (224 knots) (CAS) Maximum structural cruising 210 m.p.h. (183 knots) Maneuvering 170 m.p.h. (148 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (+38.0) to (+43.1) at 5200 lb. (+43.6) at 4800 lb. (+32.0) to (+43.6) at 4300 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight Landing: 5200 lb. Takeoff: 5200 lb. Number 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) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) or 133 gal. (with 2 wing tip tanks and 2 auxiliary tanks, 15.5 gal. each at +47) (See NOTE 1 for data on unusable fuel) Oil Capacity 6.5 gal. (3.25 ga l. in each engine at (-3.5), unusable 1.5 gal. per engine (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps 45° Down Movements Main surfaces Aileron 20° Up 20° Down Elevator 25° Up 15° Down Rudder 25° Right 25° Left (Parallel to W.L.) Tab (main surface in neutral) Aileron 20° Up 20° Down Elevator 10° Up 26° Down Rudder 17° Right 22° Left (Parallel to W.L.) Serial Nos. Eligible All Model 320 (S ection I) Serial Nos. are eligible, upon modification in accordance with Cessna AK320-28. III. Model 320A, (Normal Category), Approved May 10, 1962 Engines Two Continental TSIO-470-B *Fuel 100/130 minimum grade aviation gasoline (See NOTE 5). *Engine Limits For all operations, 2600 rpm, 260 hp, 35 in. Hg MP Critical altitude is 16,000 ft. in standard atmosphere. 3A25 4 Rev. 28 III. Model 320A (cont’d) Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartzell hubs HC-A2XF-2 with 8433 blades Diameter: not over 80 in., not under 78 in. No further reduction permitted Pitch settings at 30 in. sta.: low 15.0°, high 22.0°, feathered 84 ±1° b. Hydraulic governor, Woodward 210280, C210355, A210438, 210444; McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Cessna 0850319-1 dome with 0850309-1 bulkhead *Airspeed Limits Never exceed 257 m.p.h. (224 knots) (CAS) Maximum structural cruising 210 m.p.h. (183 knots) Maneuvering 170 m.p.h. (148 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (+38.0) to (+43.1) at 5200 lb. (+43.6) at 4800 lb. (+32.0) to (+43.6) at 4300 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight Landing: 5200 lb. Takeoff: 5200 lb. Number 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), 60 lb. on upper rack (+124), 80 lb. per side on floor (+124) (See NOTE 2G for placards) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) or 133 gal. (with 2 wing tip tanks and 2 auxiliary tanks 15.5 gal. each at +47) (See NOTE 1 for data on unusable fuel) Oil Capacity 6.5 gal. (3.25 gal. in each engine (-3.5), unusable 1.5 gal. per engine) (See NOTE 1 for data on undrainable oil) Control Surface Wing flaps 45° Down Movements Main surfaces Aileron 20° Up 20° Down Elevator 25° Up 15° Down Rudder 25° Right 25° Left (Parallel to W.L.) Tab (main surface in neutral) Aileron 20° Up 20° Down Elevator 10° Up 26° Down Rudder 17° Right 22° Left (Parallel to W.L.) Serial Nos. Eligible 320A0001 thru 320A0047 Rev. 28 5 3A25 IV. Model 320B, (Normal Category), Approved May 16, 1963 Engines Two Continental TSIO-470-C *Fuel 100/130 minimum grade av iation gasoline. See NOTE 5 *Engine Limits For all operations, 2600 rpm, 260 hp, 35 in. Hg MP Critical altitude is 16,000 ft. in standard atmosphere Propeller and 1. 2 full-feathe ring propeller installations Propeller Limits a. Hartze ll hubs HC-A2XF-2 with 8433 blades Diameter: not over 80 in., not under 78 in. No further reduction permitted Pitch settings at 30 in. sta.: low 15.0°, high 22.0°, feathered 84 ±1° b. Hydraulic governor, Woodward 210280, C210355, A210438, 210444; McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Cessna 0850319-1 dome with 0850319-1 bulkhead *Airspeed Limits Never exceed 257 m.p.h. (224 knots) (CAS) Maximum structural cruising 210 m.p.h. (183 knots) Maneuvering 170 m.p.h. (148 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (+38.0) to (+43.1) at 5200 lb. (+43.6) at 4800 lb. (+32.0) to (+43.6) at 4300 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight Landing: 5200 lb. Takeoff: 5200 lb. Number 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. on floor at (+96), 80 lb. per side on floor at (+124), 60 lb. on upper rack at (+124), 120 lb. per nacelle at (+63) Oil Capacity 6.5 gal. (3.25 ga l. in each engine at (-3.5), unusable 1.5 gal. per engine) (See NOTE 1 for data on undrainable oil) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35) or 133 gal. (with 2 wing tip tanks and 2 auxiliary tanks 15.5 gal. each at +47) (See NOTE 1 for data on unusable fuel) Control Surface Wing flaps 35° Down Movements Main surfaces Aileron 20° Up 20° Down Elevator 16.5° Up 15° Down Rudder 25° Right 25° Left (Parallel to W.L.) Tab (main surface in neutral) Aileron 20° Up 20° Down Elevator 10° Up 26° Down Rudder 17° Right 22° Left (Parallel to W.L.) Serial Nos. Eligible 320B0001 thru 320B0062 3A25 6 Rev. 28 V. Model 320C, Skyknight, (Normal Category), Approved April 24, 1964 Engines Two Continental TSIO-470-D *Fuel 100/130 minimum grade aviation gasoline (see NOTE 5). *Engine Limits For all operations, 2600 rpm, 260 hp, 35 in. Hg MP Critical altitude is 16,000 ft. in standard atmosphere. Propeller and 1. 2 McCauley full-f eathering propeller installations Propeller Limits a. McCauley hubs D2AF34C54 with 84HF blades Diameter: not over 81 in., not under 78 in. No further reduction permitted Pitch settings at 30 in. sta.: low 14.0°, high 15.6°, feathered 82.7° b. Hydraulic governor, Woodward 210280, C210355, 210444, A210438; McCauley DCFU290D1/T2, DCFU290D2/T2 c. Propeller spinner, Cessna 0850331-2 dome with 0850257-7 bulkhead *Airspeed Limits Never exceed 257 m.p.h. (224 knots) (CAS) Maximum structural cruising 210 m.p.h. (183 knots) Maneuvering 170 m.p.h. (148 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (+38.0) to (+43.1) at 5200 lb. (+43.6) at 4800 lb. (+32.0) to (+43.6) at 4300 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight Landing: 5200 lb. Takeoff: 5200 lb. 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. on floor at (+96), 80 lb. per side on floor (+124), 120 lb. per nacelle (+63) Oil Capacity 6.5 gal. (3.25 ga l. in each engine at (-3.5), unusable 1.5 gal. per engine) (See NOTE 1 for data on undrainable oil) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) or 133 gal. (with 2 wing tip tanks and 2 auxiliary tanks 15.5 gal. each at +47) (See NOTE 1 for data on unusable fuel) Control Surface Wing flaps 35° Down Movements Main surfaces Aileron 20° Up 20° Down Elevator 16.5° Up 15° Down Rudder 25° Right 25° Left (Parallel to W.L.) Tab (main surface in neutral) Aileron 20° Up 20° Down Elevator 10° Up 26° Down Rudder 17° Right 22° Left (Parallel to W.L.) Serial Nos. Eligible 320C0001 thru 320C0073 Rev. 28 7 3A25 VI. Model 320D, Skyknight, (Normal Category), Approved April 9, 1965 Engines Two Continental TSIO-520-B or TSIO-520-BB *Fuel 100/130 minimum grade aviation gasoline (see NOTE 5). *Engine Limits For all operations, 2700 rpm, 285 hp, 35 in. Hg MP Critical altitude is 16,000 ft. in standard atmosphere. Altitude Max. Allowable MP 16,000 ft. 32.0 in. Hg 18,000 ft. 30.7 in. Hg 20,000 ft. 29.0 in. Hg 22,000 ft. 26.4 in. Hg 24,000 ft. 24.3 in. Hg 26,000 ft. 22.2 in. Hg 28,000 ft. 20.2 in. Hg 30,000 ft. 18.5 in. Hg Propeller and 1. 2 full-feathering 2-bladed propeller installations Propeller Limits a. McCaul ey hubs D2AF34C71 with 84JF blades Diameter: not over 81 in., not under 79 in. No further reduction permitted Pitch settings at 30 in. sta.: low 13.3°, high 14.8°, feathered 82.7° b. Hydraulic governor, Woodward B210446, A210529 c. Propeller spinner, Cessna 0855032-1 dome with 0855032-2 bulkhead 2. 2 full-feathering 3-bladed pr opeller installations (See NOTES 7 & 8). a. McCauley hubs 3AF32C87 with 82NC-4 blades or McCauley hubs 3AF32C72 with 82N-4 blades Diameter: not over 78 in., not under 74 in. No further reduction permitted Pitch settings at 30 in. sta.: 3AF32C72 Hubs: low 12.7°, feathered 82.3° 3AF32C87 Hubs: low 13.0°, feathered 82.6° b. Hydraulic governor, Woodward B210446, A210529 c. Propeller spinner, 3-bladed, McCauley D-3534 dome with D-3537 bulkhead 3. 2 full-feathering 3-bladed propeller installations (See NOTE 8). a. McCauley hubs 3AF 32C504 with 82NEA-4 blades Diameter: not over 78 in., not under 74 in. No further reduction permitted Pitch settings at 30 in. st a.: low 13.0°, feathered 82.6° b. Hydraulic governor, Woodward B210446, A210529 c. Propeller spinner, 3-bladed, Mc Cauley D3534 dome with D3537 bulkhead *Airspeed Limits Never exceed 257 m.p.h. (224 knots) (CAS) Maximum structural cruising 210 m.p.h. (183 knots) Maneuvering 170 m.p.h. (148 knots) Flaps extended 140 m.p.h. (122 knots) Landing gear extended 140 m.p.h. (122 knots) *C.G. Range (+38.0) to (+43.1) at 5200 lb. (+43.6) at 4800 lb. (+32.0) to (+43.6) at 4300 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None 3A25 8 Rev. 28 VI. Model 320D (cont’d) *Maximum Weight Landing: 5200 lb. Takeoff: 5200 lb. 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. on floor at (+96), 80 lb. per side on floor (+124), 120 lbs per nacelle (+63) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) or 143 gal. (with 2 wing tip tanks and 2 auxiliary tanks 20.5 gal. each at +47) (See NOTE 1 for data on unusable fuel) Oil Capacity 6.5 gal. (3.25 ga l. in each engine at (-3.5), unusable 1.5 gal. per engine) (See NOTE 1 for data on unusable oil) Control Surface Wing flaps 35° Down Movements Main surfaces Aileron 20° Up 20° Down Elevator 16.5° Up 15° Down Rudder 29.3° Right 29.3° Left (parallel to W.L.) Tab (main surface in neutral) Aileron 20° Up 20° Down Elevator 10° Up 26° Down Rudder 17° Right 22° Left (parallel to W.L.) Serial Nos. Eligible 623, 320D0001 thru 320D0130 VII. Model 320E, Executive Skyknight, (N ormal Category), Approved July 26, 1966 Engines Two Continental TSIO-520-B or TSIO-520-BB *Fuel 100/130 minimum grade aviation gasoline (see NOTE 5). *Engine Limits For all operations, 2700 rpm, 285 hp, 32 in. Hg MP Critical altitude is 16,000 ft. in standard atmosphere. Altitude Max. Allowable MP Sea level 32.0 in. Hg 16,000 ft. 32.0 in. Hg 18,000 ft. 30.7 in. Hg 20,000 ft. 29.0 in. Hg 22,000 ft. 26.4 in. Hg 24,000 ft. 24.3 in. Hg 26,000 ft. 22.2 in. Hg 28,000 ft. 20.2 in. Hg 30,000 ft. 18.5 in. Hg 32,000 ft. 17.0 in. Hg Rev. 28 9 3A25 VII. Model 320E (cont’d) Propeller and 1. 2 full-feathering 2-bladed propeller installations Propeller Limits a. McCauley Hubs D2AF34C71 with 84JF blades Diameter: not over 81 in., not under 79 in. No further reduction permitted Pitch settings at 30 in. sta.: low 13.3°, high 14.8°, feathered 82.7° b. Hydraulic governor, Woodward B210446, A210529 c. Propeller spinner, Cessna 0855032-1 dome with 0855032-2 bulkhead 2. 2 full-feathering 3-bladed propeller installations (See NOTE 8) a. McCauley hubs 3AF32C87 with 82NC-4 blades or McCauley hubs 3AF32C504 with 82NEA-4 blades Diameter: not over 78 in., not under 74 in. No further reduction permitted Pitch settings at 30 in. st a.: low 13.0°, feathered 82.6° b. Hydraulic governor, Woodward B210446, A210529 c. Propeller spinner, 3-bladed, McCauley D-3534 dome with D-3537 bulkhead *Airspeed Limits Never exceed 257 mph (224 knots) (CAS) Maximum structural cruising 210 mph (183 knots) Maneuvering 170 mph (148 knots) Flaps extended 160 mph (139 knots) Landing gear extended 160 mph (139 knots) *C.G. Range (+39.3) to (+43.1) at 5300 lb. (+43.6) at 4900 lb. (+32.0) to (+43.6) at 4300 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight Landing: 5300 lb. Takeoff: 5300 lb. 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. on floor at (+96), 80 lb. per side on floor (+124), 120 lb. per nacelle (+63) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) or 143 gal. (with 2 wing tip tanks and 2 auxiliary tanks 20.5 gal. each at +47) or 183 gal. (with 2 wing tip tanks, 2 auxiliary ta nks and 2 wing locker transfer tanks 20 gal. each at +49.0) (See NOTE 1 for data on system fuel) Oil Capacity 6.5 gal. (3.25 ga l. in each engine at (-3.5), unusable 1.5 gal. per engine) (See NOTE 1 for data on system oil) 3A25 10 Rev. 28 VII. Model 320E (cont’d) Control Surface Wing flaps 35° Down Movements Main surfaces Aileron 20° Up 20° Down Elevator 16.5° Up 15° Down Rudder 29.3° Right 29.3° Left (parallel to W.L.) Tab (main surface in neutral) Aileron 20° Up 20° Down Elevator 10° Up 26° Down Rudder 17° Right 22° Left (parallel to W.L.) Serial Nos. Eligible 320E0001 thru 320E0110 VIII. Model 320F, Executive Skyknight, (Normal Category), Approved May 10, 1967 Engines Two Continental TSIO-520-B or TSIO-520-BB *Fuel 100/130 minimum grade aviation gasoline (see NOTE 5). *Engine Limits For all operations, 2700 rpm, 285 hp, 32 in. Hg MP Critical altitude is 16,000 ft. in standard atmosphere. Altitude Max. Allowable MP Sea level 32.0 in. Hg 16,000 ft. 32.0 in. Hg 18,000 ft. 30.7 in. Hg 20,000 ft. 29.0 in. Hg 22,000 ft. 26.4 in. Hg 24,000 ft. 24.3 in. Hg 26,000 ft. 22.2 in. Hg 28,000 ft. 20.2 in. Hg 30,000 ft. 18.5 in. Hg 32,000 ft. 17.0 in. Hg Propeller and 1. 2 full-feathering 2-bladed propeller installations Propeller Limits a. McCauley Hubs D2AF34C71 with 84JF blades Diameter: not over 81 in., not under 79 in. No further reduction permitted Pitch settings at 30 in. sta.: low 13.3°, high 14.8°, feathered 82.7° b. Hydraulic governor, Woodward B210446, A210529 c. Propeller spinner, Cessna 0855032-1 dome with 0855032-2 bulkhead 2. 2 full-feathering 3-bladed propeller installations (See NOTE 8) a. McCauley hubs 3AF32C87 with 82NC-4 blades or McCauley hubs 3AF32C504 with 82NEA-4 blades Diameter: not over 78 in., not under 74 in. No further reduction permitted Pitch settings at 30 in. st a.: low 13.0°, feathered 82.6° b. Hydraulic governor, Woodward B210446, A210529 c. Propeller spinner, 3-bladed, McCauley D-3534 dome with D-3537 bulkhead *Airspeed Limits Never exceed 257 m.p.h. (224 knots) (CAS) Maximum structural cruising 210 m.p.h. (183 knots) Maneuvering 170 m.p.h. (148 knots) Flaps extended 160 m.p.h. (139 knots) Landing gear extended 160 m.p.h. (139 knots) Rev. 28 11 3A25 VIII. Model 320F (cont’d) *C.G. Range (+39.3) to (+43.1) at 5300 lb. (+43.6) at 4900 lb. (+32.0) to (+43.6) at 4300 lb. or less Straight line variation between points given. Empty Wt. C.G. Range None *Maximum Weight Landing: 5300 lb. Takeoff: 5300 lb. 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. on floor at (+96), 80 lb. per side on floor (+124), 120 lb. per nacelle (+63) Fuel Capacity 102 gal. (2 wing tip tanks, 51 gal. each at +35.0) or 143 gal. (with 2 wing tip tanks and 2 auxiliary tanks 20.5 gal. each at +47) or 183 gal. (with 2 wing tip tanks, 2 auxiliary ta nks and 2 wing locker transfer tanks 20 gal. each at +49.0) (See NOTE 1 for data on system fuel) Oil Capacity 6.5 gal. (3.25 ga l. in each engine at (-3.5), unusable 1.5 gal. per engine) (See NOTE 1 for data on system oil) Control Surface Wing flaps 35° Down Movements Main surfaces Aileron 20° Up 20° Down Elevator 16.5° Up 15° Down Rudder 29.3° Right 29.3° Left (parallel to W.L.) Tab (main surface in neutral) Aileron 20° Up 20° Down Elevator 10° Up 26° Down Rudder 17° Right 22° Left (parallel to W.L.) Serial Nos. Eligible 658, 320F0001 thru 320F0045 IX. Model 340, (Normal Category), Approved October 15, 1971 Engines Two Teledyne Continental TSIO-520-K or TSIO-520-KB *Fuel 100/130 minimum grade aviation gasoline (see NOTE 5). *Engine Limits For all operations, 2700 rpm, 285 hp, 33.0 in. Hg MP up to critical altitude of 16,000 ft., in standard atmosphere. Above 16,000 ft., the following maximum MP applies for maximum rpm. Altitude (ft.) Max. Allowable MP (in. Hg) 16,000 ft. 33.0 18,000 ft. 30.2 20,000 ft. 28.0 23,000 ft. 24.5 26,000 ft. 21.5 29,000 ft. 19.0 3A25 12 Rev. 28 IX. Model 340 (cont’d) Propeller and 1. 2 full-feathering 2-bl aded propeller standard installations Propeller Limits a. McCauley hubs D2AF34C71 with 84JF-3 blades Diameter: not over 81 in., not under 79 in. No further reduction permitted Pitch settings at 30 in. st a.: low 13.3°, feathered 82.7° b. Hydraulic governor, Woodward B210446, A210529; McCauley DCFS290D1/T3, DCFUS2990D1/T3, DCFS290D7/T3, DCFUS290D7/T3 or DCFUS290D13/T3 c. Propeller spinner, McCauley D-3800 dome with D3818 bulkhead 2. 2 full-feathering 3-bladed optio nal propeller installations (See NOTE 8). a. McCauley hubs 3AF32C87 with 82NC-4 blades or McCauley hubs 3AF32C504 with 82NEA-4 blades Diameter: not over 78 in., not under 74 in. No further reduction permitted Pitch settings at 30 in. st a.: low 13.0°, feathered 82.6° b. Hydraulic governor, Woodward B210446, A210529; McCauley DCFS290D1/T3, DCFUS290D1/T3, DCFS290D7/T3, DCFUS290D7/T3 or DCFUS290D13/T3 c. Propeller spinner, McCauley D-3534 dome with D3796 bulkhead *Airspeed Limits S/N 340-0001 thru 340-0300 (CAS) Maneuvering 179 m.p.h. (155 knots) Maximum structural cruising 230 m.p.h. (200 knots) Never exceed 270 m.p.h. (234 knots) Flaps extended 15° 180 m.p.h. (156 knots) Flaps extended 45° 160 m.p.h. (139 knots) Landing gear extended 160 m.p.h. (139 knots) S/N 340-0301 and On Maneuvering 155 knots (179 m.p.h.) Maximum structural cruisi ng 200 knots (230 m.p.h.) Never exceed 234 knots (270 m.p.h.) Flaps extended 15° 160 knots (184 m.p.h.) Flaps extended 45° 140 knots (161 m.p.h.) Landing gear extended 140 knots (161 m.p.h.) *C.G. Range Landing gear extended (+150.41) to (+155.59) at 5975 lb. (T.O. and landing) to (+155.96) at 5575 lb. (+146.09) to (+155.96) at 5075 lb. or less Straight line variation between points given. Landing gear retracted moment change: +860 in.-lb. Empty Wt. C.G. Range None *Maximum Weight Landing: 5975 lb. Takeoff: 5975 lb. No. of Seats 6 (2 at +137.0, 2 at +175.0, 2 at +204.0). See Manufacturer's Equipment List for optional seating arrangements.