2006 Schweizer 300C

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The Schweizer 300C is a light utility helicopter produced by the American manufacturer Schweizer Aircraft.
The 300C was introduced in 1986 as an improved version of the Schweizer 300, featuring a new engine, improved avionics, and a redesigned tail rotor system. The engine used in the 300C is a Lycoming HIO-360-F1AD producing 210hp. The maximum speed of the 300C is 125 knots (144 mph), and the range is 350 miles.
The 300C is a popular choice for commercial operations such as news gathering, aerial photography, and air ambulance services. It is also used for private and business transportation, law enforcement, agricultural spraying, and military training.
The 300C has a two-blade main rotor and a two-blade tail rotor. It is equipped with a collective pitch control system, which allows the pilot to adjust the rotor blade angle to control the altitude of the helicopter.
The 300C has a maximum takeoff weight of 2,200 lbs. The empty weight is 1,500 lbs. The cabin has room for up to four passengers, plus the pilot.
The Schweizer 300C is considered to be a reliable and versatile light utility helicopter. It is easy to fly and maintain, making it a popular choice for both commercial and private operators.


  • Total Time: 4796
  • Engines / Mods / Prop
  • HIO-360-D1A (1,500 Hour TBO)
  • 517.5 hrs Time Since Major Overhaul
  • Main Rotors:
  • 3-Blade (5,500 Hour Life)
  • Rotor 1
  • 3,361.9 hrs Time Remaining
  • Rotor 2
  • 1,985.5 hrs Time Remaining
  • Rotor 3
  • 1,985.5 hrs Time Remaining
  • Tail Rotors: 2-Blade (9,000 Hour Life)
  • Rotor 1
  • 4,222.8 hrs Time Remaining
  • Rotor 2
  • 5,374.2 hrs Time Remaining
  • Avionics / Equipment
  • Garmin GMA 340 Audio Panel
  • Garmin GNS 530 Comm/GPS
  • Bendix/King HSI
  • Free Flight Radar Altimeter
  • UAVIONIX Tail Beacon ADS-B
  • Garmin GTX 327 Transponder
  • Dual Tanks
  • Aero Dynamix NVG Cockpit
  • ADS-B Out

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