The dynamic elegance of the all metal low wing aircraft will take you to your destination as the crow flies, in leather seats with a state of the art carbon-fibre cockpit and offering panoramic views of the world you're leaving behind. The impressively engineered design offers comfortable flight characteristics and is generously forgiving for novice pilots. The excellent equipment is an integration of highly advanced flying, navigation, communication and high-end monitoring systems, displayed on large, clear LCD screens.
The comprehensive equipment of the ergonomic cockpit is complemented with electrically operated flaps, balancing and autopilot. The highest level of safety of the crew and aircraft is assured with a rescue parachute system for the entire plane (AEPS). ATTACK VIPER SD4 version RTC and NVFR has demonstrated compliance with CS-LSA Amdt.1 and has been awarded a type certificate by the EASA (certificate number EASA.A.606). It is also certified in several national locations and aviation categories.
UL | CS-LSA / LSA | |
---|---|---|
Engine 4-stroke Rotax 912 | UL 80 HPULS 100 HP | ULS 100 HP |
Fuel tank volume | 70 L 100 L | 100 L |
Consumption (NAT 95) / 1 hod. | 16,4 L | 16,4 L |
Wing span | 8,4 m | 8,4 m |
Length | 6,4 m | 6,4 m |
Height | 2,2 m | 2,2 m |
Take-off distance | 150 m | 180 m |
Landing distance | 140 m | 160 m |
Range | 705 km | 1 200 km |
Cruising speed | 200 km/h | 200 km/h |
Max. speed | 240 km/h | 240 km/h |
Stall speed | 65 km/h | 75 km/h |
Climb rate | 6 m/s | 5 m/s |
Durability | 3 h 45 m - 750 km | 6 h - 1200 km |
Max. take-off weight incl. BRS | 472,5 kg | 600 kg |
UL | CS-LSA / LSA | |
---|---|---|
Engine 4-stroke Rotax 912 | UL 80 HPULS 100 HP | ULS 100 HP |
Fuel tank volume | 18,5 US gal26,4 US gal | 26,4 US gal |
Consumption (NAT 95) / 1 hod. | 4,3 US gal | 4,3 US gal |
Wing span | 27 ft 4 in | 27 ft 4 in |
Length | 21 ft | 21 ft |
Height | 7 ft 3 in | 7 ft 3 in |
Take-off distance | 492 ft | 590 ft |
Landing distance | 459 ft | 524 ft |
Range | 405 nmi | 648 nmi |
Cruising speed | 108 kts | 108 kts |
Max. speed | 130 kts | 130 kts |
Stall speed | 35 kts | 40 kts |
Climb rate | 1 181 ft/min | 984 ft/min |
Durability | 3 h 45 m - 405 nmi | 6 h - 648 nmi |
Max. take-off weight incl. BRS | 1 041 lbs | 1 320 lbs |
UL | CS-LSALSA | |
---|---|---|
Engine4-strokeRotax 912
|
UL 80 HPULS 100 HP
|
ULS 100 HP
|
Fueltankvolume
|
70 L 100 L
|
100 L
|
Consumption1 hod.
|
16,4 L
|
16,4 L
|
Wing span
|
8,4 m
|
8,4 m
|
Length
|
6,4 m
|
6,4 m
|
Height
|
2,2 m
|
2,2 m
|
Take-offdistance
|
150 m
|
180 m
|
Landingdistance
|
140 m
|
160 m
|
Range
|
705 km
|
1 200 km
|
Cruisingspeed
|
200 km/h
|
200 km/h
|
Max.speed
|
240 km/h
|
240 km/h
|
Stallspeed
|
65 km/h
|
75 km/h
|
Climbrate
|
6 m/s
|
5 m/s
|
Durability
|
3 h 45 m750 km
|
6 h1200 km
|
Max.take-offweight incl. BRS
|
472,5 kg
|
600 kg
|
UL | CS-LSALSA | |
---|---|---|
Engine4-strokeRotax 912
|
UL 80 HPULS 100 HP
|
ULS 100 HP
|
Fueltankvolume
|
18,5 US gal26,4 US gal
|
26,4 US gal
|
Consumption1 hod.
|
4,3 US gal
|
4,3 US gal
|
Wing span
|
27 ft 4 in
|
27 ft 4 in
|
Length
|
21 ft
|
21 ft
|
Height
|
7 ft 3 in
|
7 ft 3 in
|
Take-offdistance
|
492 ft
|
590 ft
|
Landingdistance
|
459 ft
|
524 ft
|
Range
|
405 nmi
|
648 nmi
|
Cruisingspeed
|
108 kts
|
108 kts
|
Max.speed
|
130 kts
|
130 kts
|
Stallspeed
|
35 kts
|
40 kts
|
Climbrate
|
1 181 ft/min
|
984 ft/min
|
Durability
|
3 h 45 m405 nmi
|
6 h648 nmi
|
Max.take-offweight incl. BRS
|
1 041 lbs
|
1 320 lbs
|