VIRUS SW 121 IS FOR YOU BECAUSE YOU ARE LOOKING FOR …
MOST ADVANCED
The most advanced and affordable 2-seat EASA Type-certified airplane in its category. The ideal Trainer or Personal Travel Airplane.
NIGHT VFR APPROVED
Comfortable interior with dual-screen glass cockpit, autopilot, Night VFR capability, with approvals for intentional spinning and glider towing.
PERFORMANCE
Robust performance and field-proven experience – this is the official trainer of Indian Airforce, Navy and NCC.
VIRUS SW 121:
The-121 is the most advanced aircraft in its category.
This is the result of over 20 years of experience in designing energy-efficient motor-planes, which follow the glider philosophy. The aircraft shapes are so clean that they enable flying with the smallest of power and noise as well as lowest fuel consumption, when keeping the performance on same level or even better. Approved for intentional spins and Night VFR, Virus SW 121 has the best flight characteristics in its category.
Structural perfection is the sum of knowledge acquired in making of 1300 aircraft of the same family of products. Certified and used in harshest conditions all over the world, the Virus SW 121 fulfills expectations of the most demanding customers, including the Indian Ministry of Defense, that acquired almost 200 Pipistrel aircraft for the official basic trainer of Indian Air Force, Navy and National Cadet Corps.
The flight characteristics of the Virus SW 121 are a testament to the aircraft with simple, extremely efficient, environmental-friendly features, but at the same time reaching superb performance that can satisfy even the most demanding pilots. Due to its advantages, excellent characteristics, low running costs and affordability, it is the best choice on the market as an advanced trainer for the training organizations.
The SW 121 features the best equipment in the category, including:
- dual-screen glass cockpit
- full-featured auto pilot
- high-speed and the longest range in category
- full airframe ballistic parachute rescue system
- certified engine capable of running on automotive fuel
- certified hydraulic constant speed propeller
- approval for intentional spins
- approval for night VFR
- airbrakes for rapid descent
- glider towing
It is important to highlight SW 121 key outstanding characteristics:
- Fast and economic performance:
It is the fastest, most capable and the most economic aircraft in the CS-LSA category. Its speed performance allows to fly at IFR speeds in/near complex airspaces and procedures, so it can be used for private use and training also at busy airports with airliners without slowing down the other traffic. - EASA Type-Certificate:
It is the first and the only EASA Type-Certified (no restrictions, category “normal”) aircraft in CS-LSA category for Night VFR operations, Intentional spins and glider-towing, the only one with an autopilot, dual redundant ADAHRS units and airbrakes. It can be used for commercial operations and it is ideal solution for PPL training. - 3D printed parts:
It is the first small aircraft in the history to be type certified with 3D printed parts. The Virus SW 121 enables the flight schools to substitute their multi-aircraft system, where they have to use at least one aircraft for basic training and another for advanced training, for one aircraft only. By combining the capability typically obtained with several aircraft into a single one, they can drastically lower the purchase price and initial costs of the training fleet. - Multiple learning purposes:
It can be used for different learning purposes: as a very simple initial trainer at the beginning of the process, until more advanced systems – such as constant speed propeller, negative flaps, airbrakes and autopilot – decide to be included. The instructor can slowly increase the difficulty of subjects in the later stages of training by gradual addition of new systems and options which the aircraft is certified for (intentional spins, longer routes and the use of auto-pilot, also during the night thanks to the night VFR approval etc.). - “En-route IFR training”
Virus SW 121 is packed with state-of-the art navigation and communication equipment: as such it can also be partially used for “en-route IFR” training in several countries This makes the Virus SW 121 the only 2-seat aircraft in the market which enables training from the simplest beginnings to the difficulty of a twin-engine aircraft for obtaining higher pilot licences. - Glider towing:
It is also certified for glider towing, which makes it even more useful, in cases where it is even more important that the flight hours on an aircraft can be fully used.
TECHNICAL DATA PIPISTREL VIRUS SW 121
model | VIRUS SW 100 EASA LSA |
---|---|
ENGINE ROTAX | Rotax EASA certified engine 912S3 100 hp, |
max power(with 2 carb.) | 100 Hp, 73,5 kW take off power |
PROPELLER | 2 blade Hydraulic CS MTV-33-1-A/170-200 EASA certified |
SIZES | |
length | 6.45 m, 26.5 ft. |
span | 10.70 m, 21.15 ft. |
height | 2.06 m, 6.75 ft. |
wing area | 9.51 m², 102.4 ft² |
wing span | 10.71 m, 35.10 ft. |
mean wing chord | 0.898 m, 2.95 ft. |
horizontal tail area | 1.02 m², 10.9 ft² |
span | 2.18 m, 7.15 ft. |
vertical tail area | 1.24 m², 13.3 ft² |
height | 1.19 m, 3.90 ft. |
aspect ratio | 11,3 |
positive flaps | 0°, +9°, +20°; marked (0), (+1), (+2) respectively |
negative flaps | 5-° marked as (-) |
center of gravity | 25% – 33% MAC |
WEIGHTS | |
Design empty weight | 349 kg, 768 lb |
max take off weight (MTOW) | 600 kg, 1323 lb |
Design useful load | 251 kg, 522 lbs |
max baggage weight | 25 kg, 55 lb |
fuel tanks capacity | 2 x 50 l |
useful fuel | 2 x 49 l |
PERFORMANCES | |
Vne – Never Exceeded Speed | 163 KTAS |
Vno – Max Structural Cruising Speed except in smooth air | 120 KIAS |
Va- Max Operating Maneuvering Speed | 100 KIAS |
Vfe- Max Flap Extended Speed | 81 KIAS |
Vae- Max Airbrakes Extended Speed | 100 KIAS |
stall without flaps | 50 KCAS |
Towing limitations | glider up to 600 kg (to meet 500 m total take off distance (over 15 m obstacle) |
best climb speed | 78 KIAS |
max climb rate | 1050 ft./min |
take off distance at SL | 160 m |
take off distance over 15 m obstacle at SL | 320 m |
Maximum take-off altitude | 10,000 ft. MSL |
Maximum operating altitude | 16,000 ft. MSL |
Permitted fuel | AVGAS, MOGAS or car fuel (min RON 95; EN228 Premium or Premium plus with max. 10% Ethanol) |
fuel consumption at 2000 ft. 75% PWR cruise speed | 18,4 l/h |
endurance @4000 ft., 65 % power) | 5h 33 min (+30 min reserve) |
range distance (+ 30 min reserve, @4000 ft., 65 % power) | 1189 km / 642 nm |
Noise level (ICAO Annex 16, Chapter 10) | 70 dB(A) (measured) |
Flight Load Factor Limits | 4.0 g+, 2.0 g- |
Note: Pipistrel reserves the right to revise this data sheet whenever occasioned by product improvement, government/authority regulations or other good cause.
EASA
Type certificate EASA.A.573 Virus SW 121
Sw121-cert
TC Data Sheet – Noise EASA.A.573 Is.1.0
TC Data Sheet – EASA.A.573 CS-LSA – Virus SW 121 – is.1.0
Intentional Spins Major Change Approval Nr. 10060479
POGOJI ODOBRITVE IN OBSEG DELA PROIZVODNE ORGANIZACIJE 21G (SI. 21G.0002)
Night VFR Major Change Approval Nr. 10063230
AUSTRIA
Cetificate of Registration Austria SW121
FRANCE
SW121 CERTIFICATE OF AIRWORTHINESS France
GERMANY
HUNGARY
SW121 CERTIFICATE OF AIRCRAFT REGISTRATION
IRAN
CERTIFICATE IRAN_2017-10-29_14-17-17
MEXICO
Mexico DGAC Type validation certificate SW 121
NETHERLANDS
POLAND
Poland SW 121 Airworthiness Review Certificate
URUGUAY