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  2. Cessna 172 - Wikipedia

    en.wikipedia.org/wiki/Cessna_172

    On August 31, 1969, American professional boxer Rocky Marciano was killed when the Cessna 172 in which he was a passenger crashed on approach to an airfield outside Newton, Iowa. [81] On September 25, 1978, a Cessna 172, N7711G, and Pacific Southwest Airlines Flight 182, a Boeing 727, collided over San Diego, California. There were 144 ...

  3. List of airliners by maximum takeoff weight - Wikipedia

    en.wikipedia.org/wiki/List_of_airliners_by...

    Type MTOW [kg] MLW [tonnes] TOR [m] LR [m] ICAO category FAA category; Antonov An-225: 640,000: 591.7: 3,500: Super: Super Scaled Composites Model 351 Stratolaunch

  4. Light aircraft - Wikipedia

    en.wikipedia.org/wiki/Light_aircraft

    A typical light aircraft: the Cessna 172 With a maximum gross takeoff weight of 12,500 lbs, the DHC-6 Twin Otter is an example of the upper limit of the light aircraft category. A Robinson R44 light helicopter. A light aircraft is an aircraft that has a maximum gross takeoff weight of 12,500 lb (5,670 kg) or less. [1]

  5. Lycoming O-320 - Wikipedia

    en.wikipedia.org/wiki/Lycoming_O-320

    Used in the Cessna 172 I to M models. O-320-E2F 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as E1F but with fixed pitch prop provisions. [4] O-320-E2G 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as E2D but with O-320-A sump and intake pipes. [4] O ...

  6. Maximum takeoff weight - Wikipedia

    en.wikipedia.org/wiki/Maximum_takeoff_weight

    Takeoff weight components. The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft, also known as the maximum structural takeoff weight or maximum structural takeoff mass, [1] is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits.

  7. Zero-fuel weight - Wikipedia

    en.wikipedia.org/wiki/Zero-fuel_weight

    The maximum zero fuel weight (MZFW) is the maximum weight allowed before usable fuel and other specified usable agents (engine injection fluid, and other consumable propulsion agents) are loaded in defined sections of the aircraft as limited by strength and airworthiness requirements.

  8. Class rating - Wikipedia

    en.wikipedia.org/wiki/Class_rating

    Weight-shift-control aircraft sea Class ratings may have limitations placed upon them. In the United States, if a pilot being examined for a multi-engine rating does not demonstrate the ability to control an aircraft under asymmetric thrust, their multi-engine rating will be endorsed as "Limited-to-Center Thrust". [ 2 ] (

  9. Cessna T-41 Mescalero - Wikipedia

    en.wikipedia.org/wiki/Cessna_T-41_Mescalero

    USAF T-41A Cessna T-41B of the Republic of Korea. Variants of the T-41 other than the T-41A were built under the type certificate of the Cessna 175 Skylark. [9] [10] The 175 was a close derivative of the 172 and most parts aft of the firewall are interchangeable.