TYPE - Twin engine five-seat amphibian remanufactured from components from Republic RC-3 Seabee single engine amphibians.
WINGS - Shoulder wing strut-braced monoplane. Wing span is increased by 6 ft. A three feet wing section with engine mountings is installed at each side of fuselage. Original Seabee wings are used for outer wing sections.
HULL - Single step all metal structure. Hull below cabin floor has series of watertight compartments. To improve stability and C of G, hull length is increased by 3 ft with the addition of a plug aft of cabin. Two additional circular windows are added to rear cabin.
TAIL UNIT - Rudder area is increased for better directional control. Rudder trim-tab area is increased.
LANDING GEAR - Hydraulically retractable main wheels, mechanically retracted tail wheel. Oleo-pneumatic shock-struts.
ENGINES - Two 180 hp Lycoming fuel injected four cylinder horizontally-opposed engines mounted above wing leading edges and driving two-bladed tractor propellers. The original Seabee fuel tank of 85 US gal capacity remains in the keel compartment below rear cabin floor. An auxiliary 16 US gal fuel tank is installed in the tail, just below tailplane.
ACCOMMODATION - Cabin seats five (+ one), four indiviual seats in two front rows, a bench seat aft.
The UC-1 Twin Bee is a twin-engine five-seat conversion of the Republic RC-3 Seabee amphibian. The conversion was developed by Mr. Joseph W. Gigante of United Consultant Corporation 1959 -1965. His company later was known as STOL Aircraft Corporation of Norwood, Massachusetts. Prototype and conversions were built in the old hangars of Helio Aircraft at Norwood Airport, MA.
In her original configuration, the prototype had two 180 hp Lycoming O-360-A1A engines, and made her first flight in 1960 with a Helio test pilot at controls. Later most test flights were made by test pilot Peter Annis. During development, engine model was changes to injection type, the cowlings were redesigned and the tail control surface areas were increased.
After extensive flight tests for five years, the UC-1 Twin Bee was awarded the US FAR Aircraft Type Certificate No: A6EA on 25 June 1965. The first production aircraft was delivered one year later.
Conversion is accomplished by replacing the Seabee's original 215 hp Franklin engine by two 180 hp Lycoming IO-360-B1D engines, driving 2-blade CS/feathering tractor propellers.
The original wing span is increased by 6 ft, to 43.33 ft, by adding a 3-foot wing-root extension on each side. The hull is stretched 3 ft by inserting a "plug" just aft of cabin, to counter-act shift of CG. Further the rudder/trim-tab area is increased according to the increased power. The fuel capacity is increased from 75 US gal to 101 US gal by the addition of a new 85 US gal main fuel tank above step and 16 US gal fuel tank in the tail boom. The instrument panel, and the seat tracks, are moved forward to allow a fifth seat in the original cargo area. To date 23 conversions have been completed, the last one in 1987.
1992-09-24'Registration Pending', New York.
1995-11-20 Mr. James E. Schuster 506 E Pioneer Road Fond Du Lac, WI 54935-6474 USA
1995-05-11 Mr. Jay L. Merten Dallas, TX USA
2002-03-12 Mr. Hardy F. Lebel 140 High Street Apt. 201 Westerly, RI 02891-1800 USA
2005-02-01 ESP Aviation LLC
3511 Silverside Road STE 105
Wilmington, DE 19810-4902
Ricci Rowe (Owner)
Ricci Rowe grew up in Central Florida, attended the University of Florida and currently flies for Southwest Airlines where he is a Senior Captain and Check-airman. Ricci's involvement in aviation started with his first airplane ride at 6 mos of age in a Cessna 195 (N1TB) that was purchased new by family friend Tommy Bartlett. Ricci now owns this plane and still flies it regularly.
As a young man Ricci skied in the famous Tommy Bartlett Water Ski Show in Wisconsin. Learning to fly at an young age in the Canadian bush he developed a love for the adventures of seaplane flying. Flying a single engine Seabee to places like I-Falls, Kenora, Churchill, York Factory and Camp Manateau.