The Collins Dipper was an American homebuilt flying boat that was designed and produced by Collins Aero of Chadds Ford, Pennsylvania and first flown in 1982. The aircraft was supplied in the form of plans for amateur construction. Only one was built and none remain registered.

Design and development

The Dipper was a conversion of a Cessna 150, adding a fiberglass hull and nose to the Cessna land plane. Development was protracted and started in 1964, leading to a first flight in 1982.

The Dipper featured a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit with doors, retractable tricycle landing gear and a single engine in pusher configuration mounted above the cabin on struts.

The aircraft is made from aluminum and fiberglass, retaining the Cessna 150's wing and lift struts. The 33.4ft (10.2m) span wing employs a NACA 2412 airfoil, mounts flaps and has a wing area of 160sqft (15m2). The standard engine used was the 180hp (134kW) Lycoming O-360 powerplant.

The aircraft nose wheel retracted forward and the main landing gear retracted upwards into the rear window space.

The Dipper had a typical empty weight of 1,100lb (500kg) and a gross weight of 1,760lb (800kg), giving a useful load of 660lb (300kg). With full fuel of 39 U.S. gallons (150L; 32impgal) the payload for pilot, passengers and baggage is 426lb (193kg).

The manufacturer estimated the conversion time from the plans as 1000 hours.

Operational history

In 1998, the company reported that 13 sets of plans had been sold and one aircraft was flying.

By December 2013, no examples remained registered in the United States with the Federal Aviation Administration.

Specifications (Dipper)

Data from AeroCrafter and The Incomplete Guide to Airfoil Usage

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 25ft 5in (7.75m)
  • Wingspan: 33ft 5in (10.19m)
  • Wing area: 160sqft (15m2)
  • Airfoil: NACA 2412
  • Empty weight: 1,100lb (499kg)
  • Gross weight: 1,760lb (798kg)
  • Fuel capacity: 39 U.S. gallons (150L; 32impgal)
  • Powerplant: 1 × Lycoming O-360 four cylinder, air-cooled, four stroke aircraft engine, 180hp (130kW)
  • Propellers: 2-bladed wooden

Performance

  • Maximum speed: 125mph (201km/h, 109kn)
  • Cruise speed: 115mph (185km/h, 100kn)
  • Stall speed: 50mph (80km/h, 43kn)
  • Range: 400mi (640km, 350nmi)
  • Service ceiling: 18,000ft (5,500m)
  • Rate of climb: 1,400ft/min (7.1m/s)
  • Wing loading: 11.0lb/sqft (54kg/m2)

External links