SINUS FLEX IS FOR YOU BECAUSE YOU ARE LOOKING FOR …
FOUR AIRCRAFT IN ONE
Four aircraft in one: a perfect glider, an efficient and fast cross-country cruiser, a versatile trainer, and a flexible wingspan solution transformer.
FLEXIBILITY IN WINGSPAN
The Sinus Flex model, which transforms the airplane from a motorglider into a fast cross-country cruiser in few minutes.
CHOICE OF UNDERCARRIAGE
Choice of nose- or tail-wheel undercarriage configuration for your personal preference.
SINUS 912 & SINUS FLEX:
Sinus motorglider combines a true sense of a glider with unprecedented efficiency during powered and long-range cruise flight. With the Sinus you can take-off and land on very short runways, fly long distance cross-country and have fun gliding with a 27:1 gliding ratio… all in the same aircraft!
With the Sinus, you literally purchase three aircraft for the price of one. You get a glider, a long range super-economic cruiser and the most versatile training aircraft on the market. Thanks to its dual flight controls and a choice of either tailwheel or nosewheel undercarriage the Sinus can be used as your primary gliding and powered-aircraft trainer! The excellent performance was confirmed with a World Champion title in 2001 and a record-breaking solo flight around the world in 2004.
You can further enhance the Sinus with a very small addition – the Flex. Sinus Flex model is identical to the standard Sinus, with the added bonus of interchangeable wing-tips. The outer 5-foot portions of each wing can be easily taken away and replaced with short winglets of a Virus model! You could not decide if you wanted a Pipistrel Sinus or a Pipistrel Virus? Now you can have both, transforming a thermal-soaring Sinus motorglider into a small and fast Virus cruiser, which can fit into any hangar It is is easy and only takes five minutes!
Sinus has proven its key outstanding characteristics time and time again
Best fuel efficiency and best range:
Sinus is simply the most efficient and economical light aircraft on the market. Given its super-low fuel consumption of less than 10 liters-per-hour (2.6 gph) at a high cruise speed of 200 km/h (110 kts), you can easily fly over 1000 kilometers (540 NM) already with the standard 60 liter (16 gal.) fuel tanks. With optional long range (100 liters; 26 gal) fuel tanks your range with reserve goes beyond 1650 km (890 NM).A World Champion and Serial Winner
Having already proven itself in the gliding arena with several eye-catching achievements, including a FAI 500 km triangle, the Sinus hold a multitude of World Records and aviation milestones. Sinus was the absolute winner of the World Championship WAG 2001 in Spain and came runner-up in 2005. In 2004 Sinus was the first light aircraft to fly around the World. Since then, our owners have performed remarkable long-range flights including a non-stop flight from Pisa to Lisbon, Athens – Nordkapp flight and the first ever light aircraft Australia – New Zealand crossing! Sinus also won the legendary race Paris – Madrid Green Air Challenge 2011.
- Excellent gliding performance:
Sinus is a glider by soul. Sporting 15-meter wings and a glide ratio of 27:1 when the propeller is feathered, you can enjoy countless hours in thermals without burning a single drop of fuel. Clean aerodynamic lines and a perfect finish is what enables the Sinus to perform even better than a number of typical motorless gliders. And remember, you can always turn on the engine, when the weather is not in your favour. - Safety:
Sinus features the Safety Cockpit Concept. The entire cabin area is encased with energy absorbing structures made from Kevlar fibre, an amazing material which maintains the integrity of the cabin and makes it safe also in case of stronger impacts. Alongside our special Safety Cockpit Concept the Sinus can also be equipped with the ballistic parachute rescue system, which saves the complete aircraft together with the crew in case of severe emergencies. - Robust and reliable:
A fleet of almost 1000 of our aircraft fly on all six continents of the World in conditions that are sometimes difficult to imagine. All systems on board have withstood rigorous testing to ensure the aircraft performs at its best in hot or cold, wet or dry, low or high! Flight schools love the Sinus because of reliability, super-low operating costs and endless possibilities of flying. - Cockpit comfort and luxury:
A spacious, well ventilated side-by-side cockpit with optional leather interior will make sure you feel comfortable also during the longest adventurous flights. Even the tallest or shortest of pilots will feel at home in the Sinus, thanks to the adjustable rudder pedals. The choice of either a small or large instrument panel can make the cockpit feel like a glider or fully equipped top-of-the-line long-range cruising aircraft. With excellent sideward and downward views your air-ground or air-air photographs will make everybody envious.
TECHNICAL DATA PIPISTREL SINUS FLEX
model | SINUS 912 | VIRUS 912 |
---|---|---|
ENGINE ROTAX | ROTAX 912 UL2 | ROTAX 912 UL |
max power(with 2 carb.) | 80 hp at 5800 rpm | 80 hp at 5800 rpm |
PROPELLER | Pipistrel VARIO | Pipistrel VARIO |
SIZES | ||
wing span | 14,97 m | 12,46 m |
length | 6,6 m | 6,5 m |
height | 1,70 m | 1,85 |
wing area | 12,26 m2 | 11,0 m2 |
rudder area | 1,1 m2 | 1,1 m2 |
tail area | 1,63 m2 | 1,63 m2 |
aspect ratio | 18,3 | 13,1 |
positive flaps | 9 deg, 18 deg | 9 deg, 18 deg |
negative flaps | 5 deg | 5 deg |
center of gravity | 20% – 39% | 20% – 38% |
WEIGHTS | ||
empty weight | 285 kg | 284 kg |
empty weight light version | 275 kg | 274 kg |
max take off weight (MTOW) | 450 kg / 472.5 kg / 544 kg | 450 kg / 472.5 kg / 544 kg |
fuel tanks capacity | 2 x 30 l / 2 x 50 l | 2 x 30 l / 2 x 50 l |
useful fuel | 2 x 27 l / 2 x 45 l | 2 x 27 l / 2 x 45 l |
PERFORMANCES | DATA PUBLISHED FOR MTOM of 472.5 kg | |
stall with flaps | 63 km/h | 64 km/h |
stall without flaps | 66 km/h | 72 km/h |
cruising speed (75% power) | 200 km/h | 225 km/h |
max. horizontal speed | 220 km/h | 240 km/h |
VNE | 225 km/h | 249 km/h |
max speed with airbrakes | 160 km/h | 160 km/h |
max speed with flaps down | 130 km/h | 130 km/h |
manoeuvring speed | 141 km/h | 141 km/h |
best climb speed | 115 km/h | 130 km/h |
max climb rate | 6,5 m/sec | 6,2 m/sec |
climb rate at 140 km/h | 6,3 m/sec | 5,9 m/sec |
min.sink speed | 90 km/h | 96 km/h |
min.sink (prop. 90 deg.) | 1,03 m/sec | 1,35 m/sec |
max. sink with airbrakes | 5,5 m/sec | 5,8 m/sec |
best glide ratio speed | 95 km/h | 110 km/h |
best glide (prop. 90 deg.) | 1:27 | 1:24 |
glide at 150 km/h (prop 90 deg) | 1:18 | 1:14 |
take off run | 88 m | 90 m |
take off over 15 m obstacle | 148m | 167 m |
service ceiling | 8800 m | 8100 m |
45°-45° roll time | 4,2 sec | 3,1 sec |
fuel consumption at cruise speed | 9,2 l/hour | 9,5 l/hour |
endurance (std tanks) | 5,8 hours | 5,7hours |
range distance | 1200 km | 1150 km |
max load factor permitted ( x1,875) | +4g -2g | +4g -2g |
design safety factors & tested | minimum 1.875 | minimum 1.875 |
Note: Pipistrel reserves the right to revise this data sheet whenever occasioned by product improvement, government/authority regulations or other good cause.
SINUS ICAO DESIGNATOR: PISI
http://cfapp.icao.int/Doc8643/8643_List3.cfm?mfc=PIPISTREL
ARGENTINA
AUSTRALIA and NEW ZEALAND
Acceptance certificate on basis of B203SF 1098L, B203SF 1099L and B203SF 1102:
Sinus | Seats | Min speed (km/h) | VNE | Engine | Propeller | No. of blades | Empty weight (kg) basic | Empty weight (kg) max. permitted | MTOW | obligatory equipment |
503 | 2 | 58 | 225 | 503 | BAM 2, BAM 3, Vario | 2 | 274 | 305 | 472.5 | GRS 473 |
582 | 2 | 58 | 225 | 582 | BAM 2, BAM 3, Vario | 2 | 280 | 305 | 472.5 | GRS 473 |
912 | 2 | 58 | 225 | 912 | BAM 2, BAM 3, Vario | 2 | 295 | 309 | 472.5 |
Acceptance certificate on basis of B203SF 1102L:
Accepted Type Approval Data Sheet:
Sinus model | Seats | Min speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Empty weight (kg) basic | Empty weight (kg) max. permitted | MTOW (kg) | Mandatory equipment |
912 | 2 | 58 | 225 | 912 | BAM 2, BAM 3, VARIO | 2 | 295 | 309 | 544 | GRS 473 |
51% Kit approval:
Australian LSA:
AUSTRIA
Type Acceptance UA 014/05 – ACG:
Type Acceptance Data Sheet:
Sinus model | Seats | Min speed (km/h) | Max speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Gearbox B ratio | Noise on 300 m | Empty weight (kg) | MTOW |
503 | 2 | 63 | 183 | 183 | 503 UL | VarioL | 2 | 2.62 | / | 275 | 450 |
912 | 2 | 65 | 250 | 225 | 912 UL | Vario | 2 | 2,27 | 59.1 dB | 297.5 | 472.5 |
BELGIUM
Type Authorisations:
Type Authorisations Data Sheet:
Ref de l `autorisation de type | Sinus model | Seats | Min speed (km/h) | Cruise speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Gear C I= | Empty weight (kg) | MTOW |
ARCA | 503 | 2 | 59 | 170 | 225 | 503 | Vario FB2 | 2 | 2.62 or 3.0 | 255 | 450 |
ARCA | 503 | 2 | 63 | 181 | 225 | 582 | Vario FB2 | 2 | 2.62 or 3.0 | 259 | 450 |
BULGARIA
CHINA
The Validation Data Sheet – SINUS 912
Validation of Type Certificate – SINUS 912
Statement of design MTOM for CAAC
CZECH REPUBLIC
Technical certificate:
Type Certificate Data Sheet:
Sinus model | Seats | Min speed (km/h) | Design speed speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Gearbox ratio | Noise on 300 m | Empty weight (Kg) | MTOW Kg | obligatory equipment |
503 | 2 | 65 | 250 | 225 | 503 UL 2V | Vario | 2 | 2.62 | 54.6 dB | 285 | 472.5 | GRS 473 |
912 | 2 | 65 | 250 | 225 | 912 UL | Vario | 2 | 2,27 | 59.1 dB | 297.5 | 472.5 | GRS 473 |
DENMARK
FRANCE
Type Approval: B203SF 1098L 1 & B203SF 1097L 1
Type Approval Data Sheet (Sinus 503 Normal Versions):
Sinus | Seats | Min speed (km/h) | VNE | Engine | Propeller | No. of blades | Empty weight (kg) basic | Empty weight (kg) max. permitted | MTOW | obligatory equipment |
503 | 2 | 58 | 225 | 503 | BAM 2, BAM 3, Vario | 2 | 274 | 305 | 472.5 | GRS 473 |
/ | / | / | / | / | / | / | / | / | / | / |
503 | 2 | 57 | 225 | 503 | BAM 2, BAM 3, Vario | 2 | 260 | 284 | 450 | w/o parachute |
Type Approval: B203SF 1099L 1 & B203SF 1100L 1
Type Approval Data Sheet (Sinus 582 Normal Versions):
Sinus | Seats | Min speed (km/h) | VNE | Engine | Propeller | No. of blades | Empty weight (kg) basic | Empty weight (kg) max. permitted | MTOW | obligatory equipment |
582 | 2 | 58 | 225 | 582 | BAM 2, BAM 3, Vario | 2 | 280 | 305 | 472.5 | GRS 473 |
/ | / | / | / | / | / | / | / | / | / | / |
582 | 2 | 57 | 225 | 503 | BAM 2, BAM 3, Vario | 2 | 266 | 284 | 450 | w/o parachute |
Type Approval: B203SF 1102L 2 & B203SF 1101L 2
Type Approval Data Sheet (Sinus 912 Normal Versions):
Sinus | Seats | Min speed (km/h) | VNE | Engine | Propeller | No. of blades | Empty weight (kg) basic | Empty weight (kg) max. permitted | MTOW | obligatory equipment |
912 | 2 | 58 | 225 | 912 | BAM 2, BAM 3, Vario | 2 | 295 | 309 | 472.5 | GRS 473 |
/ | / | / | / | / | / | / | / | / | / | / |
912 | 2 | 57 | 225 | 912 | BAM 2, BAM 3, Vario | 2 | 279 | 286.5 | 450 | w/o parachute |
Type Approval: B203SF 1653L & B203SF 1652L
Type Approval Data Sheet (Sinus 503 Light Versions):
Sinus | Seats | Min speed (km/h) | VNE | Engine | Propeller | No. of blades | Empty weight (kg) basic | Empty weight (kg) max. permitted | MTOW | obligatory equipment |
503 | 2 | 58 | 225 | 912 | BAM 2, BAM 3, Vario | 2 | 265 | 305 | 472.5 | GRS 473 |
/ | / | / | / | / | / | / | / | / | / | / |
503 | 2 | 57 | 225 | 912 | BAM 2, BAM 3, Vario | 2 | 251 | 284 | 450 | w/o parachute |
Type Approval: B203SF 1655L & B203SF 1654L
Type Approval Data Sheet (Sinus 912 Light Versions):
Sinus | Seats | Min speed (km/h) | VNE | Engine | Propeller | No. of blades | Empty weight (kg) basic | Empty weight (kg) max. permitted | MTOW | obligatory equipment |
912 | 2 | 58 | 225 | 912 | BAM 2, BAM 3, Vario | 2 | 286 | 309 | 472.5 | GRS 473 |
/ | / | / | / | / | / | / | / | / | / | / |
912 | 2 | 57 | 225 | 912 | BAM 2, BAM 3, Vario | 2 | 270 | 286.5 | 450 | w/o parachute |
GERMANY
Sinus 503 Certificate link to official site: http://www.dulv.de/Dreiachs_Kennblaetter/details.php?id=18424
Sinus 912 Certificate link to official site: http://www.dulv.de/Dreiachs_Kennblaetter/details.php?id=18422
Type Certificate Data Sheet:
Sinus model | Seats | Min speed (km/h) | Design speed speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Gearbox ratio | Noise on 300 m | Empty weight (Kg) | MTOW Kg | obligatory equipment |
503 | 2 | 65 | 250 | 225 | 503 UL 2V | Vario | 2 | 2.62 | 54.6 dB | 285 | 472.5 | GRS 473 |
912 | 2 | 65 | 250 | 225 | 912 UL | Vario | 2 | 2,27 | 59.1 dB | 297.5 | 472.5 | GRS 473 |
Sinus 912 NW Certificate link to official site: http://www.dulv.de/Dreiachs_Kennblaetter/details.php?id=19017
Sinus model | Seats | Min speed (km/h) | Design speed speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Gearbox ratio | Noise on 300 m | Empty weight (Kg) | MTOW Kg | obligatory equipment |
912 NW | 2 | 65 | 250 | 225 | 912 UL | Vario | 2 | 2,27 | 59.1 dB | 294 | 472.,5 | GRS 473 |
/ | / | / | / | / | / | / | / | / | / | / | / | / |
HUNGARY
Type Documentation: Sinus 912 UL
INDIA
AC India certificate of registration
* the max. approved weight is 541.2kgs
IRELAND
ITALY
Permit to Fly for models as below:
Sinus model | Seats | Min speed (km/h) | Max speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Noise at 300 m | Empty weight (kg) | MTOW |
503 | 2 | 63 | 186 | 225 | 503 | Bam 2 | 2 | 65 dB | 255 | 450 |
582 | 2 | 63 | 200 | 225 | 582 | Bam 2 | 2 | 62 dB | 266 | 450 |
912 | 2 | 63 | 220 | 225 | 912 | Bam 2 | 2 | 63 dB | 285 | 450 |
KAZAKHSTAN
MEXICO
NETHERLANDS
Sinus model | Seats | Min speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Gearbox ratio | Noise on 300 m
| Empty weight (Kg) | MTOW Kg | obligatory equipment |
912 NW | 2 | 65 | 250 | 912 UL | VARIO | 2 | 2,27 | 59.1 dB | 294 | 472.5 | GRS 473 |
NORWAY
POLAND
Permit to Fly for models as below:
Sinus model | Seats | Min speed (km/h) | Max speed (km/h) | WNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Noise on 300 m | Empty weight (kg) | MTOW |
447 | 2 | 59 | 170 | 210 | 447 | Bam 2 | 2 | 65 dB | 240 | 450 |
503 | 2 | 63 | 186 | 225 | 503 | FB 2L or VARIO L | 2 | 65 dB | 256 | 450 |
582 | 2 | 63 | 200 | 225 | 582 | FB 2L or VARIO L | 2 | 62 dB | 274 | 450 |
912 | 2 | 63 | 220 | 225 | 912 | FB 2D or VARIO D | 2 | 63 dB | 284 | 450 |
REPUBLIC of MACEDONIA
REPUBLIC of SOUTH AFRICA
Non-Type Certified Aircraft Acceptance: J15/12/498
SLOVENIA
Type Approval: TC 99/001 – AT/ULN 01:
Type Approval Data Sheet:
Sinus model | Seats | Min speed (km/h) | Max speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Noise at 300 m | Empty weight (kg) | MTOW (kg) |
447 | 2 | 59 | 170 | 210 | 447 | Bam 2L | 2 | 65 dB | 240 | 410 |
503 | 2 | 63 | 186 | 225 | 503 | FB 2L or VARIO L | 2 | 65 dB | 265 | 450 |
582 | 2 | 63 | 200 | 225 | 582 | FB 2L or VARIO L | 2 | 62 dB | 274 | 450 |
912 | 2 | 63 | 220 | 225 | 912 | FB 2D or VARIO D | 2 | 63 dB | 284-309 | 472.5 |
SPAIN
Type Approval: C.T. No 290/I:
Type Certificate Sinus 912 – Espana
Type Approval Data Sheet:
Sinus model | Seats | Min speed (km/h) | Vmax(km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Gearbox ratio | C.G. range | Empty weight (Kg) | MTOW Kg | obligatory equipment |
503 | / | / | / | / | / | / | / | / | / | / | / | / |
912 | 2 | 65 | 203 | 225 | 912 UL | Vario | 2 | 2,27 | 20-39% MAC | 289 kg | 450 | / |
SWITZERLAND
Ecolight Certificate: Ecolight
Sinus 912 Certificate link to official site: LetterSinus
Sinus 912 NW Certificate link to official site: LetterSinusNW
Type Certificate Data Sheet:
Sinus model | Seats | Min speed (km/h) | Design speed speed (km/h) | VNE (km/h) | Engine Rotax | Propeller Pipistrel | No. of blades | Gearbox ratio | Noise on 300 m | Empty weight (Kg) | MTOW Kg | obligatory equipment |
912 TW | 2 | 65 | 250 | 225 | 912 UL | Vario | 2 | 2.62 | 59.1 dB | 297.5 | 472.5 | GRS 473 |
912 NW | 2 | 65 | 250 | 225 | 912 UL | Vario | 2 | 2,27 | 59.1 dB | 294 | 472.5 | GRS 473
|
TURKEY
CERTIFICATE OF REGISTRATION SINUS 912
USA – amateur built kit
USA – LSA certificates
http://en.wikipedia.org/wiki/Light-sport_aircraft#Aircraft
Permit to fly – CAA Qatar