Four-seat twin-engined kit build aircraft, designed to be operated from both land and water. For water operations detachable floats can be fitted (TRX version). Kit is designed to comply with FAA 51% rule. Major components of kit will already be assembled. ICAO type designation is ‘CAT2’.
Model TR is aircraft without floats attached; model TRX is with floats attached. Single-engined Models SR and SRX are planned (which see).
price: (September 2005)
model TR: US$ 79000
model TRX: US$ 94000

last update: 17 April 2006

Design started in 1997. Prototype C-GYCC flew in single-engined form in 2001 and converted to twin-engined form in 2002. Production of kits expected to start in 2005.

- Aircraft has a central cabin seating 4, attached to gull wing as a pod.
- Twin tailbooms are mounted below wing, housing the retractable main landing gear.
- “Power Arch” on top of wing, capable of supporting either 1 or 2 powerplants.
- Optional amphibious floats can be attached to the tailbooms within 45 minutes; each float has a 284 l (10.0 cu ft) stowage compartment.
- Aircraft has all-composite construction.
- Fully retractable tricycle landing gear with free castoring nosewheel.
- Main landing gear extends through cutouts in floats allowing aircraft to take-off and land on hard surface with floats attached.

- Two Jabiru 3300 6-cylinder horizontally-opposed engines, each delivering 120 hp (88 kW).
- Each engine drives a 3-blade constant-speed propeller, manufactured by Airmaster.
- Total fuel capacity 256 l (68 USG).

- Electrical system: 14V DC system standard.
- Pneumatic system: for landing gear actuation.

Can be fitted with wide range of avionics depending upon the builders choice.

Four seats in standard 2+2 layout. Aircraft configuration creates exceptional visibility. Backseat is removable for increased luggage space, cabin has been designed specifically for camping. Door on each side of cabin, dual controls.

N/A

External:# wing span;10.37 m / 34.00 ft# overall length; 8.23 m / 27.00 ft# fuselage length; 8.05 m / 26.40 ft# overall height; 2.71 m / 8.90 ft# wing area; 15.3 sq m / 165 sq ft# .;.# Internal:# cabin length; 2.74 m / 108.0 in# cabin width; 1.45 m / 57.0 in# cabin height; 1.17 m / 46.0 in

TR (no floats attached)# max. t-o weight; 1225 kg / 2700 lbs# empty weight; 726 kg / 1600 lbs# useful load; 499 kg / 1100 lbs# wing loading; 80 kg/sq m / 16.4 lb/sq ft# power loading; 5.1 kg/hp / 11.3 lb/hp# .;.# TRX (floats attached)# max. t-o weight; 1225 kg / 2700 lbs# empty weight; 816 kg / 1800 lbs# useful load; 408 kg / 900 lbs# wing loading; 80 kg/sq m / 16.4 lb/sq ft# power loading; 5.1 kg/hp / 11.3 lb/hp

TR (no floats attached), estimated# max. speed, S/L; 161 kts / 292 km/h# cruise speed (TAS), 65% power, 7000 ft; 148 kts / 274 km/h# max. range, 75% power, S/L; 900 nm / 1667 km# max. range, 65% power, S/L; 950 nm / 1759 km# max. range, 55% power, S/L; 1000 nm / 1852 km# service ceiling; 14000 ft / 4267 m# max. rate of climb; 1200 fpm / 6.1 m/s# stall speed, flaps down; 43 kts / 80 km/h# t-o run; 137 m / 450 ft# t-o distance over 15 m (50 ft) obstacle; 168 m / 550 ft# landing distance over 15 m (50 ft) obstacle; 168 m 550 ft# landing run; 137 m / 450 ft# .;.# TRX (floats attached), estimated# max. speed, S/L; 143 kts / 265 km/h# cruise speed (TAS), 65% power, 7000 ft; 130 kts / 241 km/h# max. range, 75% power, S/L; 800 nm / 1482 km# max. range, 65% power, S/L; 850 nm / 1574 km# max. range, 55% power, S/L; 900 nm / 1667 km# service ceiling; 14000 ft / 4267 m# max. rate of climb; 1100 fpm / 5.6 m/s# stall speed, flaps down; 43 kts / 80 km/h# t-o run; 152 m / 500 ft# t-o distance over 15 m (50 ft) obstacle; 183 m / 600 ft# landing distance over 15 m (50 ft) obstacle; 168 m / 550 ft# landing run; 137 m / 450 ft