Continental O-190: Difference between revisions

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{{Short description|Series of small American piston aircraft engines}}
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{|{{Infobox aircraft begin
{|{{Infobox aircraft begin
  |name= O-190 / C75 / C85
  |name= O-190 / C75 / C85
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==References==
==References==
{{Commons category|Continental C85}}
{{Reflist}}
* Gunston, Bill. (1986) ''World Encyclopedia of Aero Engines''. Patrick Stephens: Wellingborough.
* Gunston, Bill. (1986) ''World Encyclopedia of Aero Engines''. Patrick Stephens: Wellingborough.
* Erickson, Jack. ''[https://web.archive.org/web/20081202141950/http://home.comcast.net/~aeroengine/Continental1.html Horizontally-Opposed Piston Aero Engines]''
* Erickson, Jack. ''[https://web.archive.org/web/20081202141950/http://home.comcast.net/~aeroengine/Continental1.html Horizontally-Opposed Piston Aero Engines]''
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{{Continental aeroengines}}
{{Continental aeroengines}}


[[Category:Continental aircraft engines|O-190]]
[[index.php?title=Category:Continental aircraft engines|O-190]]
[[Category:Boxer engines]]
[[index.php?title=Category:Boxer engines]]
[[Category:1940s aircraft piston engines]]
[[index.php?title=Category:1940s aircraft piston engines]]

Latest revision as of 15:03, 26 May 2025

O-190 / C75 / C85
O-190 mounted in a Funk B

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

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

<templatestyles src="Div col/styles.css"/>

Specifications (C85)

Template:Pistonspecs

See also

Related lists

References

Template:Continental aeroengines

O-190 index.php?title=Category:Boxer engines index.php?title=Category:1940s aircraft piston engines

  1. 1.0 1.1 Teledyne Continental Motors: Continental Aircraft Engine Operator's Manual, pages 4-5. Teledyne Continental Motors, FAA Approved December 1980. Continental Form No. X30012
  2. 2.00 2.01 2.02 2.03 2.04 2.05 2.06 2.07 2.08 2.09 2.10 2.11 2.12 2.13 2.14 2.15 2.16 2.17 2.18 2.19 2.20 2.21 2.22 2.23 2.24 2.25 2.26 2.27 2.28 2.29 2.30 2.31 Type Certificate Data Sheet No. E-233.  (18 February 2025)  Retrieved 18 February 2025 from FAA Dynamic Regulatory System