LIGHT SPORT AIRCRAFT
SPECIFICATIONS
Empty Weight (no options)
Wing Span
Wing Area
Chord
Aspect ratio
Length
Height ( At Wing)
Cockpit Height
Width
Headroom
Legroom
Seats
Baggage Compartment
Fuel Capacity
Doors
Dual rudder foot controls
Central aileron and elev.
Central Flap controls
Dual throttle controls
4 Point seat harness
POWER PLANT
NOSEWHEEL & TAILWHEEL
AMPHIBIOUS
703
31.5 ft
142 ft 2
54 inches
7.01
17.2 ft
7.5 ft
54 inches
55.25 inches
33.5 inches
43.3 inches
2
Max. 66 lbs
24.8 Gallons
2
std
std
std
std
std
845
31.5 ft
142 ft 2
54 inches
7.01
19.8 ft
10.5 ft
54 inches
55.25 inches
33.5 inches
43.3 inches
2
Max 66 lbs
24.8 Gallons
2
std
std
std
std
std
ROTAX 582
ROTAX 912UL
ROTAX 912ULS
AMPHIBIOUS
PERFORMANCE AT
SEA LEVEL at MAUW
582/99 UL
65 HP
2 / 3 Blade
3.47 : 1
3.8 Gal / hr
912 UL
80 HP
2 / 3 Blade
2.43 : 1
4.2 Gal / hr
912 ULS
100 HP
2 / 3 Blade
2.43 : 1
4.6 gal / hr
912 ULS
100 HP
2 / 3 Blade
2.43 : 1
4.0 gal / hr
ROTAX 582
ROTAX 912UL
ROTAX 912ULS
AMPHIBIOUS
Take Off Roll
Rate Of Climb
Service Ceiling
Max crosswind component
Cruise Speed (65%)
Maximum level Speed
VNE
Glide Ratio
Power Off Stall, No Flaps
Power Off Stall, Flaps
Landing Ground Roll
Gross Weight
Useful Load
Load Factors
Roll Rate
Endurance (with reserve)
Range (with reserve)
472 ft
700 ft/min
12,000 ft asl
32 mph
75 mph
100 mph
125 mph
~11:1
42 mph
38 mph
235 ft
1320
617
+6 -4
~3 sec 45/45
~6.5 hrs
~500 miles
472 ft
920 ft/min
12,000 ft asl
32 mph
95 mph
105 mph
125 mph
~11:1
42 mph
38 mph
235 ft
1320
617
+6 -4
~3 sec 45/45
~7.5 hrs
~670 miles
472 ft
1050 ft/min
14,000 ft asl
32 mph
105 mph
110 mph
125 mph
~11:1
42 mph
38 mph
235 ft
1320
617
+6 -4
~3 sec 45/45
~7.0 hrs
~700 miles
540 ft (water)
850 ft/min
12,000 ft asl
20 mph
90 mph
105 mph
115 mph
~8:1
42 mph
38 mph
305 ft
1430
585
+5 -3
~3 sec 45/45
~7.0 hrs
~650 miles
Engine
Output
Propeller
Reduction ratio
Fuel Consumption (80%)
U.S. Distributor / Sales Contact: AeroSport, LLC
Tel. (262) 448-1122 - [email protected] - www.bushcatusa.com