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Continental O-190

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

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]

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

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C75

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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

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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

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C75

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C85

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Specifications (C85)

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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

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Related lists

References

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  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.