Explorer
The most advanced and affordable 2-seat EASA Type-certified airplane in its category. With its comfortable interior, dual-screen glass cockpit, CS propeller, airbrakes and autopilot, it is the ideal Trainer or Personal Travel Airplane.
SPINS & NIGHT VFR APPROVED
Capable of glider towing, night VFR, with intentional spinning approvals and capable of advanced UPRT training, SW 121 is just made to train future commercial pilots.
PERFORMANCE
Robust performance and field-proven experience – this is the official trainer of Indian Airforce, Navy and NCC. It cruises at 2 NM per minute, climbs at 1000 fpm, is complex and full of automation.
#pipistrel #shortwind #virus-sw121
Category
Cruising
ENGINE ROTAX
Rotax EASA certified engine 912S3 100 hp
DESCRIPTION
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:
|
It is important to highlight SW 121 key outstanding characteristics:
|
TECHNICAL CHARATERISTICS
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- |
DESCRIPTION
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:
It is important to highlight SW 121 key outstanding characteristics:
|
TECHNICAL CHARATERISTICS
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- |