200 ‒ Series

  • For decades, students taking to the air in training airplanes were introduced to the wonders of flight powered by the Continental® O-200. The O-200-D lightweight engines weighs in at 190 lbs. The O200-D Lightweight offers aircraft builders a certified and pedigreed engine that is lighter in weight without compromising performance, durability or service life. This engine packs a powerful punch with 100 continuous horsepower at 2750 RPM. Pilots always remember the airplane they first soloed. With the amazing 200 series, they'll remember the engine too.

    Continental Motors 200 Series Engine

    The 200 Series is a family of 4-cylinder, 4-stroke, spark ignited, air-cooled, horizontally opposed, direct-drive reciprocating aircraft engines designed for fixed pitch, ground adjustable, or electric constant speed propeller. The engines are made with a wet oil sump, caruretor with manual mixture control, continuous fuel injection, and Full Authority Digital Engine Control (FADEC) fuel control.


    Certified Fuels

    80/87, 100/100LL AvGas

    Displacement

    3292 to 3929 cm³201 to 240 in³

    Power

    75 to 93 kW100 to 125 HP

    Maximum Rated RPM

    2750 to 2800 r/min2750 to 2800 RPM

    Bore

    103.2 mm (200)4.062 in (200)
    112.7 mm (240)4.438 in (240)

    Stroke

    98.4 mm (200, 240)3.875 in (200, 240)

    Compression Ratio

    7.0:1 (200)8.5:1 (200D, 240)

    Height

    589 to 667 mm23.18 to 26.25 in

    Width

    798 to 802 mm31.4 to 31.56 in

    Length

    666 to 739 mm26.22 to 29.1 in

    Typical Weight

    88 to 131 kg193 to 239 lbs

    Time Between Overhaul (TBO)

    Up to 2200 to 2400 hrs *

    Turbo Model Availability

    No

     * Most engine models manufactured after February 2012 have a TBO increase of 200 hours. Engines used in frequent type service have an additional 200 hour increase. See Service Information Letter SIL98-9B for details. 

    200 Series Details

    Model # CYL Rated Power1 Bore x Stroke Displacement Typical Weight
    Incl. Accessories
    Certified Fuel
    Grade
    Compression Ratio Time Between Overhaul (TBO)2  FAA
    TCDS
    O-200-A 4 75 kW @ 2750 103.2 x 98.4 mm 3292 cm³ 97.0 kg 80/87 7.0:1 Up to 2200 hrs
    or 12 years
    E-252
    100 HP @ 2750 4.062 x 3.875 in 201 in³ 214 lbs
    O-200-D 4 75 kW @ 2750 103.2 x 98.4 mm 3292 cm³ 88.0 kg 100LL 8.5:1 Up to 2400 hrs
    or 12 years
    E-252
    100 HP @ 2750 4.062 x 3.875 in 201 in³ 193 lbs

    240 Series Details

    Model # CYL Rated Power1 Bore x Stroke Displacement Typical Weight
    Incl. Accessories
    Certified Fuel
    Grade
    Compression
    Ratio
    Time Between Overhaul (TBO)2 FAA
    TCDS 
    IO-240-B 4 93 kW @ 2800 112.7 x 98.4 mm 3929 cm³ 123 kg 100/100LL 8.5:1 Up to 2400 hrs
    or 12 years
    E750
    125 HP @ 2800 4.438 x 3.875 in 240 in³ 283 lbs
    IOF-240-B
    (FADEC)
    4 93 kW @ 2800 112.7 x 98.4 mm 3929 cm³ 131 kg 100/100LL 8.5:1 Up to 2400 hrs
    or 12 years
    E750
    125 HP @ 2800 4.438 x 3.875 in 240 in³ 289 lbs


    1. Engine rated power at sea level standard day inlet conditions (29.92 in Hg, 59°F, 0 water vapor) with maximum allowable cylinder head and oil temperatures with full rich (maximum) fuel flow. 

    2. See Maintenance Manual M-0 for details and applicability.




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