Skip to main content

Meet the Viper SD4 RTC

Exclusive sport aircraft certified by EASA. Brilliant way to become a professional pilot

Parameters

Viper SD4 RTC

The Viper SD4 RTC demonstrated successful compliance with the requirements of the CS-LSA Amdt.1 regulation and was granted a certificate type by EASA. The Viper SD4 RTC became the first aircraft and one of the few in Europe with EASA type certificate for aircraft of the LSA (Light Sport Aircraft) category, MTOW 600 kg.

Extended chassis

for soft landing even on uneven grasslands

Rescue parachute

rigidly built parachute for the whole aircraft

Propeller

supplies the aircraft with energy to overcome air drag and gain forward speed

Electric buoyancy flaps

with accelerated change of 3 positions secured by powerful electric motors

Winglets

increase the lift of wings and extend the range

A directional rudder

effectively increases directional stability during take-off

Comfort cabin

spacious cabin with excellent view

EASA Certified

Confirmation of prescribed criteria, competence, quality and safety of the aircraft

Ideal for pilot training

Unique comfort, modern equipment, top quality, low cost and consumption

Glass Cockpit

Avionic equipment

State-of-the-art avionics technologies – extensive use and premium design. Two 10” Dynon SkyView digital instruments, flight and engine data indicators, provide a perfect overview. Certified analogue instruments speedometer, altimeter and compass guarantee high reliability and quality. The instrument panel includes an important safety instrument, the ELT – an emergency signal transmitter that accurately displays the position of the aircraft in the event of adverse situations, including in difficult-to-reach terrain. The extensive equipment is complemented by the Intercom device, a system for communication between the crew in the cabin.

Certifed compass
ELT – Emergency Locator Transmitter
Transponder, Certified altimeter
Primary Glass Cockpit SkyView 10″
Secondary Glass Cockpit SkyView 10″
Electric 3-stage flaps
Intercom
Certified airspeed, radio
Ignition and section switches
Carburetor heating, cylinder air, cabin heating, 12V socket
Configuration

High Value Added Aircraft

The obtained EASA certificate is an appreciation of creative work of development specialists, perfect sophistication of production with maximum emphasis on customer orientation of all processes carried out. The prerequisite for obtaining the EASA CS-LSA certificate was successfully mastering corkscrew tests. The plane passed the tests successfully. The test consists in the need to remove the corkscrew within 3 seconds. As soon as the aircraft reaches the corkscrew, it must exit the corkscrew at the next turn or time period of 3 seconds. The SPIN corkscrew test result confirms the high level of safety of the Viper SD4 aircraft. The EASA certificate entitles Viper SD4 RTC to be used in aviation schools for PPL pilot training with the possibility of continuing the goal of becoming a traffic pilot. The configuration of the aircraft clearly confirms this claim.

engine

Engine

Rotax 912 100 hp – ULS or S2 certified
engine

Engine equipment

fuel flow indicator, additional electric pump

Propeller

Propeller

Neuform CR 3 -65, adjustable on the ground

Safety

Safety

BRS recovery system, ELT emergency locator transmitters

Digital avionics

Digital avionics

2x Dynon SkyView 10” engine/flying data + GPS mode

Analog avionics

Analog avionics

certified instruments: ASI, ALT, compass

Avionics

Communication

radio ATR 833, transponder TRT 800 S mode, Intercom

Flight control

Flight control

electric flaps, electric trim (H+V)

Lights

Lights

position and strobe lights, landing lights, position beacon

Cabin

Cabin

safety seat belts, cargo area blinds

Interior

Interior

cabin heating, air ventilation system

exterior

exterior

side steps, aerodynamic wheel covers

CS-LSA
Wing span
8,34 m

27,4 ft

Height
2,27 m

7,5 ft

Length
6,44 m

21,2 ft

Engine 4-stroke Rotax 912
ULS/S2 100 HP
Preopeller 3-blades, gorund adj.
DUC FLASH-R Certified (Neuform CR3-65)
Cruising speed
190 km/h

102,6 kt

Stall speed
91 km/h

49,1 kt

Climb rate
4,6 m/s

905,5 ft

Take-off distance over 15 m (50 ft) obstacle
420 m

1 377 ft

Landing distance over 15 m (50 ft) obstacle
450 m

1 476 ft

Durability
7,5 hrs
Range
1 350 km

729 nm

Consumption (NAT 99+) / 1 hour
14,5 L

3,8 US gal

Tank volume
100 L

26,4 US gal

Max. take off weight incl. BRS
600 kg

1 320 lbs