Robin Aircraft for Travelling
| PRICES | DR401 155CDI | DR401 916is | DR401 160A Long Range | DR401 180A / CS Long-range | DR401 200AI Country | DR401 200!Ai Long-range | Panels |
|---|---|---|---|---|---|---|---|
| VFR day/night | |||||||
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Twin G5 GTN 650Xi Nav/Com Audio panel Mode-S Heated pitot |
€366,314.07 | €366,314.07 | €353,071.63 | €366,732.32 / €385,357.32 | €418,072.19 | €426,172.19 | Example panel |
| IFR | |||||||
|
G500 TXi GTN 750Xi Nav/Com GNC 255 Com 2 Audio panel Mode-S DME ELT Heated pitot Alternate static source |
€423,964.44 | €423,964.44 | €410,722.00 | €424,382.69 / €443,007.69 | €475,722.56 | €483,822.56 | Example panel |
| POPULAR OPTIONS | Price |
|---|---|
| Leather upholstery and trim | €5,180.00 |
| Long-range (50 litre) tank | €5,050 |
| S-Tec 55X autopilot for G500 TXi | €30.791.49 |
| S-Tec 30 autopilot for G5 | €27,081.48 |
| Avidyne TAS 605 | €12,378.15 |
| Electric rudder trim | €6,860 |
| SPECIFICATIONS | DR401 155CDI | DR401 916is | DR401 160A Long Range | DR401 180A / CS Long-range | DR401 200AI Long-range |
|---|---|---|---|---|---|
| Engine | TAE 125-02-114 155 cv | Rotax 916 is | Lycoming 0-320-D2A 160 | Lycoming 0-360-A3A 180 | Lycoming I0-360-A1B6 200 |
| Propeller | MT Propeller MTV/6/a/190/169 CS | MT Propeller MTV/6/a/190/169 CS | Sensenich 74DM6 S5-2-64 FP | Sensenich 76 EM8 S5-0-64 FP | MTV-12B/188/59B CS |
| Seats | Four | TBC | Four | Four | Four |
| Empty weight (typical VFR fit) | 660 kg | TBC | 600 kg | 610 kg | 690 kg |
| MTOW | 1100 kg | TBC | 1050 kg | 1,100 kg | 1,100 kg |
| Useful load (no fuel) | 440 kg | TBC | 450 kg | 490 kg | 410 kg |
| Useful load (with 5 hours of fuel) | 343 kg | TBC | 317 kg | 342 kg | 237 kg |
| Luggage compartment | 40 kg / 334 l | TBC | 40 kg / 334 l | 60 kg / 334 l | 60 kg / 334 l |
| Fuel: main tank | 109 l Jet A-1 | TBC | 190 l petrol | 189 l petrol | 189 l petrol |
| Fuel: optional tank | 50 l Jet A-1 | TBC | 50 l petrol | 50 l petrol | 50 l petrol |
| Rate of climb (sea level) | 740 fpm | TBC | 770 fpm | 827 fpm | 1,130 fpm |
| Max Cruise | 134 KTAS | TBC | 133 KTAS | 135 KTAS | 135 KTAS |
| VNE | 146 KIAS | TBC | 166 KIAS | 166 KIAS | 166 KIAS |
| VNO | 140 KIAS | TBC | 140 KIAS | 140 KIAS | 140 KIAS |
| VA | 116 KIAS | TBC | 116 KIAS | 116 KIAS | 116 KIAS |
| VFE | 92 KIAS | TBC | 92 KIAS | 92 KIAS | 92 KIAS |
| Vy (best climb rate) | 78 KIAS | TBC | 78 KIAS | 78 KIAS | 78 KIAS |
| Vx (best climb angle) | 65 KIAS | TBC | 70 KIAS | 70 KIAS | 70 KIAS |
| VSO | 49 KIAS | TBC | 50 KIAS | 51 KIAS | 53 KIAS |
| Take-off ground roll | 214 m | TBC | 295 m | 250 m | 280 m |
| Take-off to clear 15 m | 400 m | TBC | 590 m | 515 m | 420 m |
| Landing to clear 15 m | 415 m | TBC | 545 m | 530 m | 370 m |
| Landing ground roll | 175 m | TBC | 250 m | 250 m | 170 m |
| Demonstrated cross-wind limit | 22 KT | 22 KT | 22 KT | 22 KT | 22 KT |
| Fuel consumption | 24 l/hr @ 75% | TBC | 35 l/hr @ 75% | 39 l/hr @ 75% | 45.4 l/hr @ 75% |
| Max range | 944 nm | TBC | 1,026 nm | 852 nm | 645 nm |