The AirCam kit has been inspected by the FAA and meets the 51% or Major Portion Rule for Experimental-Amateur Built Aircraft.
The AirCam is constructed primarily of aircraft-grade aluminum components, and features conventional fabric-covered flying surfaces and a high-performance Dacron wing. The entire structure has been engineered and with safety and performance in mind.
AIRCRAFT
| Fuel Capacity | 28 gallons |
| Range | 340 miles at 70mph |
| Endurance | 6 hours |
DIMENSIONS
| Wingspan | 36 ft. |
| Height conventional gear
amphib. floats
|
8 ft. 6 in. 13 ft. 6 in. |
| Length | 27 ft. |
POWERPLANT
| Rotax 912ULS | |
|
|
4cyl. horizontally opposed, carbureted |
|
|
100 HP (x2) |
|
|
Warp Drive three-blade carbon fiber composite propeller (x2) |
| Rotax 912iS | |
|
|
4cyl. horizontally opposed, electronically fuel injected |
|
|
100 HP (x2) |
|
|
Warp Drive three-blade carbon fiber composite propeller (x2) |
| Rotax 914UL | |
|
|
4cyl. horizontally opposed, carbureted turbocharged |
|
|
115 HP (x2) |
|
|
Airmaster three-blade constant speed propeller (x2) |
PERFORMANCE
| Maximum Speed | 110 mph |
| Cruise Speed (smooth air)
(normal)
|
50 to 100 mph 100 mph 50 to 85 mph |
| Stall Speed | 39 mph |
| Rate of Climb solo, 50% fuel
single engine
|
1500 fpm 2000 fpm 300 fpm |
WEIGHT
| Conventional Gear (Generation 3) | |
| Empty Weight | 1100 lbs. |
| Gross Weight | 1900 lbs. |
| Useful Load | 800 lbs. |
| Conventional Gear (Generation 2) | |
| Empty Weight | 1080 lbs. |
| Gross Weight | 1680 lbs. |
| Useful Load | 600 lbs. |
| Amphibious Floats | |
| Empty Weight | 1400 lbs. |
| Gross Weight | 2000 lbs. |
| Useful Load | 600 lbs. |