title: Fisher FP-202 Koala
text: # Fisher FP-202 Koala
  
  The Fisher FP-202 Koala is a Canadian single-seat high wing, conventional landing gear, single engined light kit aircraft designed for construction by amateur builders. The aircraft was inspired by the design of the Piper J-3 Cub and strongly resembles that design.
  
  Fisher Flying Products was originally based in Edgeley, North Dakota, United States but the company is now located in Dorchester, Ontario, Canada.
  
  ## Development
  
  The FP-202 was designed by Fisher Aircraft in the United States in 1981 and was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. It is also a 51% approved kit for the US homebuilt aircraft category. The design goal was to provide ultralight pilots with an aircraft that looked like and flew like the classic Piper Cub, without the regulation that goes with owning a type certified aircraft. The FP-202 can achieve an empty weight of 250 lb (113 kg) when equipped with a lightweight, two-stroke engine, such as the 28 hp (21 kW) Rotax 277.
  
  The construction of the FP-202 is unusual for aircraft in its class. The aircraft's structure is entirely made from wood, with the wooden fuselage built from wood strips arranged in a geodesic form, resulting in a very strong and light aircraft with redundant load paths. Like the Cub, both the wings and fuselage on the Koala are covered with doped aircraft fabric. The wings are strut-braced and utilize jury struts. The landing gear is bungee suspended and the tail wheel is steerable. Brakes are optional. The company claims it would take an average amateur builder 250–500 hours to build the FP-202.
  
  ## Specifications (FP-202 Koala)
  
  Data from AeroCrafter and KitPlanes
  
  General characteristics
  
  * Crew: one
  * Length: 17.9 ft (5.5 m)
  * Wingspan: 29.9 ft (9.1 m)
  * Height: 5.8 ft (1.8 m)
  * Wing area: 120 sq ft (11 $m^2)$
  * Empty weight: 245 lb (111 kg)
  * Gross weight: 500 lb (227 kg)
  * Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
  * Powerplant: 1 × Rotax 277 single cylinder, air-cooled, two stroke aircraft engine, 28 hp (21 kW)
  * Propellers: 2-bladed wooden, fixed pitch
  
  Performance
  
  * Maximum speed: 62 mph (100 km/h, 54 kn)
  * Cruise speed: 57 mph (92 km/h, 50 kn)
  * Stall speed: 26 mph (42 km/h, 23 kn)
  * Range: 135 mi (217 km, 117 nmi)
  * Service ceiling: 10,000 ft (3,000 m)
  * Rate of climb: 750 ft/min (3.8 m/s)
  