Continental O-200

The Continental C90 and O-200 are a family of air-cooled, horizontally opposed, four-cylinder, direct-drive aircraft engines of 201 in³ (3.29 L) displacement, producing between 90 and 100 horsepower (67 and 75 kW).^[1]

Built by Continental Motors these engines are used in many light aircraft designs of the United States, including the early Piper PA-18 Super Cub,^[2] the Champion 7EC,^[3] the Alon Aircoupe,^[4] and the Cessna 150.^[5]

Though the C90 was superseded by the O-200, and many of the designs utilizing the O-200 had gone out of production by 1980, with the 2004 publication of the United States Federal Aviation Administration light-sport aircraft regulations^[6] came a resurgence in demand for the O-200. The light-sport aircraft standard is for small, simple single- and two-seat aircraft for which the O-200 is well-suited.

Design and development

The C90 was introduced in 1947 as a follow-on to the A65, which had been in production since 1939.^[7][8] Many of the designs powered by the C90 are upgraded variants of earlier A65 powered designs, such as the Piper J-3 Cub and PA-11 Cub Special,^[9] Aeronca 7AC,^[3] and Luscombe 8A.^[10] The engine was developed from the earlier O-190 by increasing the stroke ¹⁄₄ inch.

This engine family is considered to be dependable, according to both industry publications and the FAA.^[11][12]

In a cooperative venture, Rolls-Royce produced these same designs in England, under separate certification, with model designations beginning RR, e.g. the Rolls-Royce RR C90-12FH is the equivalent of the Continental C90-12FH; the Rolls-Royce versions are "directly interchangeable with the equivalent models manufactured by Continental."^[13] The Rolls-Royce O-200-A powers the Beagle B.121 Pup 100,^[14] the Bölkow BO 208 C Junior,^[15] the Avions Robin DR 220,^[15] and the Morane-Saulnier MS-880.^[15]

All versions of the C90 and O-200 are Four-stroke reciprocating engines and are all similar in size, displacement and weight. These engines are typically fitted with an updraft carburetor, though the C90-8FJ, -12FJ, and -14FJ are equipped with fuel injection systems. They utilize a redundant ignition system requiring no external power, driving two magnetos, each of which fires one spark plug per cylinder. Each cylinder has one intake valve and one exhaust valve, pushrod-activated.^[1]

Continental's recommended time between overhaul (TBO) for these engines is 1,800 hours of operation or 12 years in service, whichever is reached first.^[16] The standard certification for the C90 and O-200 specifies Avgas 80/87 as the minimum fuel grade.^[1] Both are eligible for operation on automobile gasoline on the basis of Supplemental Type Certificates.^[17]

Variants

C90

While the C90 is approved for takeoff power of 95 horsepower (71 kW) for 5 minutes, the designation derives from its continuous power rating of 90 hp (67 kW). As noted above, certain models of the C90 replace the usual carburetor with a fuel injection system. In addition, there are models which provide for the installation of a controllable pitch propeller and one, the C90-12FP, designed for pusher installation.^[1] While slightly less horsepower than the O200, many floatplane operators prefer the performance of the C90 over the O200, due to its higher torque at lower rpm. This is primarily due to the C90's camshaft design. The C90 is also known by its military designation of O-205.^[7]

Continental O-200D

C90-8FJ;

C90-12F

C90-12FH

C90-12FJ

C90-12FP

C90-14FJ

C90-16F

O-200

The O-200 is an updated and upgraded version of the engine, achieving increased power of 100 hp (75 kW) as a result of higher maximum rpm. The standard and most common model of the engine is the O-200-A; the -B model is designed for pusher installation, the -C model provides for the installation of a controllable pitch propeller, and the -D model is a lightweight model designed for Light Sport aircraft.^[1]

O-200-A

O-200AF

O-200-AF

UL91 and UL94 95hp alternate fuel engine. ^[18]

IOL-200

The aft engine of the round the world flight Rutan Voyager

Voyager 200

Alternative name for the IOL-200

O-205

Rolls-Royce O-200-A

(a.k.a. Rolls-Royce/Continental O-200-A) Licence production of the O-200 in the United Kingdom for Beagle Pup and the French built Cessna F150 and MS880 Rallye.

Operational history

Continental IOL-200

An engine designated the IOL-200, an O-200 variant modified with fuel injection and liquid cooling, powered the 1986 non-stop, non-refueled global circumnavigation flight of the Rutan Voyager. The 110-horsepower (82 kW) IOL-200, also referred to as the Voyager 200, was the rear engine and—unlike the forward engine, another modified engine, a Continental O-240 —ran throughout the entire 9-day flight save for a four-minute shutdown due to a fuel problem.^[19]

Formula One racer Sharp Nemesis, designed and flown by Jon Sharp, was powered by a 'stock' O-200. Between 1991 and 1999, the plane won 45 of the 48 events in which it was entered, as well as winning three Louis Blèriot medals, four Pulitzer Trophies, and setting 16 speed records in its class. In one of those records, Nemesis was clocked at over 290 mph (467 km/h).^[20] By contrast, the O-200 powered Legend Cub cruises at 95 mph (152.9 km/h).^[21]

Applications

With 23,949 Cessna 150s built, this type is the most common application for the O-200.

Specifications (O-200-A)

Data from Engine specifications: O-200-A & B.^[22]

General characteristics

• Type: Four-cylinder air-cooled horizontally opposed piston engine
• Bore: 4.06 in (103.1 mm)
• Stroke: 3.88 in (98.6 mm)
• Displacement: 201 in³ (3.29 L)
• Length: 28.53 in (724.7 mm)
• Width: 31.56 in (801.6 mm)
• Height: 23.18 in (588.8 mm)
• Dry weight: 170.18 lb (77.19 kg) dry, without accessories

Components

• Valvetrain: Hydraulic lifters, two pushrod-actuated valves—one intake, one exhaust—per cylinder
• Fuel system: Updraft carburetor with manual mixture control
• Fuel type: 80/87 avgas minimum
• Oil system: 6 US quart (5.7 L), wet sump
• Cooling system: Air-cooled

Performance

• Power output: 100 hp (75 kW)
• Specific power: 0.5 hp/in³ (23 kW/L)
• Compression ratio: 7.0:1
• Power-to-weight ratio: 0.56 hp/lb (920 W/kg)

See also

Related development

• Continental A-65
• Continental O-300

Comparable engines

• Franklin 4AC
• Lycoming O-235
• Rotax 912

Related lists

• List of aircraft engines

References

External links

Wikimedia Commons has media related to Continental O-200.

• Teledyne Continental Motors