## Su-90 "Copper" Medium Lift Aircraft

  The Su-90 is designed to transport heavy cargoes at long distances. It is a turboprop powered aircraft, with two engines on the overhead wing. It also has a large ramp at the tail section to also to allow vehicles to enter that way. The Su-90 can transport large loads despite the size, which is superior to most aircraft, which sacrifice cargo space to passenger space. Light vehicles, troops, and other equipment can be carried in the cargo bay, as well as aircraft engines have been demonstrated as the kind of equipment the Su-90 can carry. The Su-90 is operated by a three man crew, the pilot, the copilot, and the loadmaster. All the areas for each crewmember have excellent seating, designed to give the pilot comfort while in a stressful condition. All instrumentation is clearly displayed, as well as a monitor hooked up to a camera in the cargo bay to allow the pilot to check the status of the bay. The most modern electronics are installed, with the state of the art installed. Included is a GPS system to show the pilot where he or she is. All data is presented on three MFDs, similar to fighter aircraft. Chaff and flare systems are installed for the military versions, but if you are needing them, Sukhoi offers a full line of chaff/flare dispensers for you. Also, the Su-90 features a retracting wheel system to allow the plane to depress to accomodate loads that cannot be sent up the ramp, or the ramp is too steep. This is especially useful for fragile components, where the risk of the cargo slipping and injuring or damaging precious equipment is high. This feature is especially important with engines, as the cradle can be inserted without damaging it. Also included are tires designed for use on unpaved surfaces, further enhancing the utility of this plane, allowing it to operate almost anywhere, which these days is what's needed, and the Su-90 can provide you with that assurance.
  The Su-90 incorporates advanced fly-by-wire systems to allow the "Copper" to be maneuverable despite the role of the airplane. Also, advanced sensors, ECM/ECCM also can be added to the enhance effective capability of the plane. All of the avionics are state-of-the-art to make a reliable aircraft for the next century more reliable. It can also mount various weapons on four hardpoints, with two on each wing. Any number of weapons can be carried, though self defense missiles are nominally carried.
  The Su-90 is also offered in a 20 passenger airliner. This is commonly used in Aeroflot shuttle runs. This features multiple APPS systems to offer protection to the customer. The civilian is still fitted for inflight refueling, which has given the Su-90 a little edge over most aircraft, which do not feature this accessory. Since this is designed for commercial hops, this does not feature a bar but a lavatory is provided for comfort on a long flight.

  Type | Handling | Speed | Accel | B/A | Sig | APilot | Load | Cost
  Military | 4 | 135/320 | 25 | 9/12 | 3 | 3 | 10,325 kg | 1,687,500¥
  Civilian | 4 | 135/320 | 25 | 9/12 | 3 | 3 | 725 kg | 1,227,500¥

  Military Model
  Seating: 2 +1 bucket seats
  Access: 2 standard + rear ramp
  Economy: 0.75 km per liter
  Fuel: 5,000 liters
  Cargo: 563 CF
  Sensors: Advanced (3)
  Landing/Takeoff Profile: STOL
  Other Features: Datajack Port, Rigger Adaptation, 150 man hours life support (30 for crew, the rest reserved for any passengers, is normally turned off), 4 external hardpoints that can carry at least 400 kg of weaponry, Variable Height Wheels, Retractable Refueling Probe (internal).
  Civilian Model
  Seating: 3 bucket seats + 20 bucket seats.
  Access: 2 standard doors
  Economy: 0.75 km per liter
  Fuel: 5,000 liters
  Cargo: 2 + 5 + 50 CF
  Sensors: Advanced (3)
  Landing/Takeoff Profile: STOL
  Other features: Same as Military model, except the hardpoints are removed, the refueling probe is left on as an option in case of emergencies. Life support is 230 hours and the aisle is 2-aisle-2 layout, and 20 APPS systems for the passengers, bathroom.
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  Fresh Productions, 1997