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Continental O-190

The Continental O-190 (Company designations C75 and C85) is a series of engines made by Continental Motors beginning in the 1940s. Of flat-four configuration, the engines produced 75 hp (56 kW) or 85 hp (63 kW) respectively.[1]

O-190 / C75 / C85
O-190 mounted in a Funk B
Type Piston aircraft engine
Manufacturer Teledyne Continental Motors
Major applications Cessna 140

The two variants shared the same bore, stroke and compression ratio. The C85 produced ten extra horsepower by virtue of having a maximum permissible rpm of 2575 versus the 2275 of the C75.[1]

The C75 was in production from 1943 to 1952 and the C85 from 1944 to 1970.

Variants

C75

C75-8
75 hp (56 kW)[2]
C75-8
75 hp (56 kW)[2]
C75-8F
75 hp (56 kW)[2]
C75-8FH
75 hp (56 kW)[2]
C75-8FHJ
75 hp (56 kW)[2]
C75-8FJ
75 hp (56 kW)[2]
C75-8J
75 hp (56 kW)[2]
C75-12
75 hp (56 kW)[2]
C75-12F
75 hp (56 kW)[2]
C75-12FH
75 hp (56 kW)[2]
C75-12FHJ
75 hp (56 kW)[2]
C75-12FJ
75 hp (56 kW)[2]
C75-12J
75 hp (56 kW)[2]
C75-12B
75 hp (56 kW)[2]
C75-12BF
75 hp (56 kW)[2]
C75-12BFH
75 hp (56 kW)[2]
C75-15
75 hp (56 kW)[2]
C75-15F
75 hp (56 kW)[2]

C85

C85-8
85 hp (63 kW)[2]
C85-8F
85 hp (63 kW)[2]
C85-8FHJ
85 hp (63 kW)[2]
C85-8FJ
85 hp (63 kW)[2]
C85-8J
85 hp (63 kW)[2]
C85-12
85 hp (63 kW)[2]
C85-12F
85 hp (63 kW)[2]
C85-12FH
85 hp (63 kW)[2]
C85-12FHJ
85 hp (63 kW)[2]
C85-12FJ
85 hp (63 kW)[2]
C85-12J
85 hp (63 kW)[2]
C85-14F
85 hp (63 kW)[2]
C85-15
85 hp (63 kW)[2]
C85-15F
85 hp (63 kW)[2]

Applications

C75

C85

Specifications (C85)

Data from Continental Aircraft Engine Operator's Manual[1]

General characteristics

Components

Performance

  • Power output: 85 hp (63 kW) at 2,575 rpm
  • Compression ratio: 6.3:1
  • Fuel consumption: 5.4 US gal/hr
  • Oil consumption: Maximum desirable 0.4 US quarts/hr

See also

Related lists

References

  1. ^ a b c Teledyne Continental Motors: Continental Aircraft Engine Operator's Manual, pages 4-5. Teledyne Continental Motors, FAA Approved December 1980. Continental Form No. X30012
  2. ^ a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad ae af Federal Aviation Administration (1 November 2011). "Type Certificate Data Sheet No. E-233" (PDF). Retrieved 25 March 2019.
  • Gunston, Bill. (1986) World Encyclopedia of Aero Engines. Patrick Stephens: Wellingborough.
  • Erickson, Jack.

continental, company, designations, series, engines, made, continental, motors, beginning, 1940s, flat, four, configuration, engines, produced, respectively, c85o, mounted, funk, btype, piston, aircraft, enginemanufacturer, teledyne, continental, motorsmajor, . The Continental O 190 Company designations C75 and C85 is a series of engines made by Continental Motors beginning in the 1940s Of flat four configuration the engines produced 75 hp 56 kW or 85 hp 63 kW respectively 1 O 190 C75 C85O 190 mounted in a Funk BType Piston aircraft engineManufacturer Teledyne Continental MotorsMajor applications Cessna 140The two variants shared the same bore stroke and compression ratio The C85 produced ten extra horsepower by virtue of having a maximum permissible rpm of 2575 versus the 2275 of the C75 1 The C75 was in production from 1943 to 1952 and the C85 from 1944 to 1970 Contents 1 Variants 1 1 C75 1 2 C85 2 Applications 2 1 C75 2 2 C85 3 Specifications C85 3 1 General characteristics 3 2 Components 3 3 Performance 4 See also 5 ReferencesVariants EditC75 Edit C75 8 75 hp 56 kW 2 C75 8 75 hp 56 kW 2 C75 8F 75 hp 56 kW 2 C75 8FH 75 hp 56 kW 2 C75 8FHJ 75 hp 56 kW 2 C75 8FJ 75 hp 56 kW 2 C75 8J 75 hp 56 kW 2 C75 12 75 hp 56 kW 2 C75 12F 75 hp 56 kW 2 C75 12FH 75 hp 56 kW 2 C75 12FHJ 75 hp 56 kW 2 C75 12FJ 75 hp 56 kW 2 C75 12J 75 hp 56 kW 2 C75 12B 75 hp 56 kW 2 C75 12BF 75 hp 56 kW 2 C75 12BFH 75 hp 56 kW 2 C75 15 75 hp 56 kW 2 C75 15F 75 hp 56 kW 2 C85 Edit C85 8 85 hp 63 kW 2 C85 8F 85 hp 63 kW 2 C85 8FHJ 85 hp 63 kW 2 C85 8FJ 85 hp 63 kW 2 C85 8J 85 hp 63 kW 2 C85 12 85 hp 63 kW 2 C85 12F 85 hp 63 kW 2 C85 12FH 85 hp 63 kW 2 C85 12FHJ 85 hp 63 kW 2 C85 12FJ 85 hp 63 kW 2 C85 12J 85 hp 63 kW 2 C85 14F 85 hp 63 kW 2 C85 15 85 hp 63 kW 2 C85 15F 85 hp 63 kW 2 Applications EditC75 Edit Auster Arrow ERCO Ercoupe 415 C postwar 415 CD 415 D 415 H Thorp T 11C85 Edit Aerauto PL 5C Aero Flight Streak Aeronca 7DC Champion Aeronca L 16A 7BCM Champion Aeronca 11BC Chief 11CC Super Chief Aeronca 12AC Chum license built ERCO Ercoupe All American Ensign Ambrosini Rondone Carlson Sparrow Cessna 120 and 140 Commonwealth Skyranger and Trimmer Culver V Druine Turbi ERCO Ercoupe 415 E 415 F 415 G Eaves Cougar 1 Fleet 80 and 81 Fisher Celebrity Fisher Dakota Hawk Funk B 85 C Globe Swift Jurca Tempete Heinonen HK 1 LeVier Cosmic Wind Lombardi FL 3 Luscombe 8E Silvaire Deluxe Macchi MB 308 Phoenix Major Piel Emeraude Smith Miniplane Stits Playboy Taylor Titch Taylorcraft BC 12D 85 BCS 12D 85 BC 12D 4 85 BCS 12D 4 85 Model 19Specifications C85 EditData from Continental Aircraft Engine Operator s Manual 1 General characteristics Type four cylinder air cooled horizontally opposed aircraft piston engine Bore 4 0625 in 103 mm Stroke 3 625 in 92 mm Displacement 188 in 3 1 L Dry weight 180 lb 81 kg Components Fuel type 80 87 octane avgas Cooling system Air cooledPerformance Power output 85 hp 63 kW at 2 575 rpm Compression ratio 6 3 1 Fuel consumption 5 4 US gal hr Oil consumption Maximum desirable 0 4 US quarts hrSee also EditRelated lists List of aircraft enginesReferences Edit Wikimedia Commons has media related to Continental C85 a b c Teledyne Continental Motors Continental Aircraft Engine Operator s Manual pages 4 5 Teledyne Continental Motors FAA Approved December 1980 Continental Form No X30012 a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad ae af Federal Aviation Administration 1 November 2011 Type Certificate Data Sheet No E 233 PDF Retrieved 25 March 2019 Gunston Bill 1986 World Encyclopedia of Aero Engines Patrick Stephens Wellingborough Erickson Jack Horizontally Opposed Piston Aero Engines Retrieved from https en wikipedia org w index php title Continental O 190 amp oldid 1106826352, wikipedia, wiki, book, books, library,

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