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Introduction
WT9 Dynamic LSA – Club, TOW
The WT9 Dynamic LSA aircraft is certified according to EASA Certification Specification for Light Sport Aeroplanes
CS-LSA, Amendment 1 dated 29th July 2013.
Thank you EASA team!
Benefits
Low noise emission – EASA Type Certificate Data Sheet For Noise Read more in FAQ..
Low consumption
Low operating costs
Recommended for SEPL training
Dynon Avionics Skyview glass cockpit
Three step warning system for stall speed with stick shaker
Emergency parachute system
TOW version:
-
- Online TOW view
- Rear camera
- More safety and comfort
- Lower towing costs
- Adjustable constant speed propeller
Performance
Weights
| Maximum takeoff weight | 600.0 kg | 1323 lb |
| Maximum landing weight | 600.0 kg | 1323 lb |
| Maximum load per seat | 120.0 kg | 265 lb |
| Maximum total front baggage weight | 2 x 10.0 kg | 2 x 22 lb |
| Maximum total rear baggage weight | 2 x 20.0 kg | 2 x 44 lb |
Top Speeds at Sea Level (Non TOW version)
| IAS | KIAS | ||
| Top speeds at sea level | At 5800 rpm | 240 | 130 |
| At 5500 rpm | 230 | 124 |
Top Speeds at Sea Level (TOW version)
| IAS | KIAS | ||
| Top speeds at sea level | At 5700 rpm* | 250 | 135 |
| At 5500 rpm | 240 | 130 |
* Propeller regulator in CONSTANT SPEED mode permits to set max. 5700 rpm.
Cruise Speeds at Altitudes and Power Setting (Non TOW version)
| Presurre altitude | Engine speed | MAP | Cruise speeds | |
| ft | rpm | inHg | IAS | KIAS |
| 2000 | 5500 | 24.2 | 223 | 120 |
| 4000 | 5500 | 24.4 | 216 | 117 |
| 6000 | 5500 | 22.6 | 211 | 114 |
| 8000 | 5500 | 21.4 | 201 | 109 |
| 10000 | 5500 | 19.9 | 192 | 104 |
Cruise Speeds at Altitudes and Power Setting (TOW version)
| Presurre altitude | Engine speed | MAP | Cruise speeds | |
| ft | rpm | inHg | IAS | KIAS |
| 2000 | 5500 | 27.1 | 229 | 124 |
| 4000 | 5500 | 25.1 | 219 | 118 |
| 6000 | 5500 | 23.1 | 209 | 113 |
| 8000 | 5500 | 21.3 | 199 | 108 |
| 10000 | 5500 | 20.1 | 191 | 103 |
Fuel Operating Ranges (Non TOW version)
| Endurances and ranges at altitude 2000 ft ISA | |||||||
| Engine speed | rpm | 4300 | 4500 | 4800 | 5000 | 5500 | |
| Fuel consumption | l/h | 14.5 | 15.5 | 17.2 | 18.5 | 21.3 | |
| IAS | km/h | 165 | 175 | 190 | 200 | 223 | |
| KIAS | knots | 89 | 94 | 103 | 108 | 120 | |
| CAS | km/h | 163 | 172 | 185 | 194 | 215 | |
| KCAS | knots | 88 | 93 | 100 | 105 | 116 | |
| TAS | km/h | 172 | 183 | 196 | 206 | 228 | |
| KTAS | knots | 93 | 99 | 106 | 111 | 123 | |
| Usable fuel (l) | 119 | hh:mm | 8:12 | 7:40 | 6:55 | 6:25 | 5:35 |
| km | 1411 | 1404 | 1356 | 1325 | 1273 | ||
| 100 | hh:mm | 6:53 | 6:27 | 5:48 | 5:24 | 4:41 | |
| km | 1186 | 1180 | 1139 | 1113 | 1070 | ||
| 80 | hh:mm | 5:31 | 5:09 | 4:39 | 4:19 | 3:45 | |
| km | 948 | 944 | 911 | 890 | 856 | ||
| 60 | hh:mm | 4:08 | 3:52 | 3:29 | 3:14 | 2:49 | |
| km | 711 | 708 | 683 | 668 | 642 | ||
| 40 | hh:mm | 2:45 | 2:34 | 2:19 | 2:09 | 1:52 | |
| km | 474 | 472 | 455 | 445 | 428 | ||
| 20 | hh:mm | 1:22 | 1:17 | 1:09 | 1:04 | 0:56 | |
| km | 237 | 236 | 227 | 222 | 214 | ||
Fuel Operating Ranges (TOW version)
| Endurances and ranges at altitude 2000 ft ISA | |||||||
| Engine speed | rpm | 5500 | 5500 | 5500 | 5500 | 5500 | |
| MAP | inHg | 27.1 | 26.1 | 25.1 | 24.1 | 23.1 | |
| IAS | km/h | 229 | 218 | 207 | 195 | 184 | |
| KIAS | knots | 124 | 118 | 112 | 105 | 99 | |
| CAS | km/h | 221 | 211 | 201 | 190 | 180 | |
| KCAS | knots | 119 | 114 | 109 | 103 | 97 | |
| TAS | km/h | 228 | 217 | 207 | 196 | 185 | |
| KTAS | knots | 123 | 117 | 112 | 106 | 100 | |
| Fuel consumption | l/h | 27.8 | 22.8 | 20.9 | 18.9 | 17.9 | |
| Usable fuel (l) | 119 | hh:mm | 4:16 | 5:12 | 5:42 | 6:18 | 6:39 |
| km | 974 | 1132 | 1181 | 1234 | 1234 | ||
| 100 | hh:mm | 3:35 | 4:22 | 4:47 | 518 | 5:35 | |
| km | 819 | 952 | 993 | 1037 | 1037 | ||
| 80 | hh:mm | 2:52 | 3:30 | 3:50 | 4:14 | 4:28 | |
| km | 354 | 761 | 794 | 830 | 830 | ||
| 60 | hh:mm | 2:09 | 2:37 | 2:52 | 3:10 | 3:21 | |
| km | 491 | 571 | 596 | 622 | 622 | ||
| 40 | hh:mm | 1:26 | 1:45 | 1:55 | 2:07 | 2:14 | |
| km | 327 | 381 | 397 | 415 | 415 | ||
| 20 | hh:mm | 0:43 | 0:52 | 0:57 | 1:03 | 1:07 | |
| km | 164 | 190 | 199 | 207 | 207 | ||
Rate of Climb (Non TOW version)
| IAS | KIAS | |
| Best angle of climb airspeed VX (at SL) | 100 IAS | 54 KIAS |
| Rate of climb at VX (at SL) | 985 fpm | |
| Best rate of climb airspeed VY (at SL) | 127 IAS | 69 KIAS |
| Rate of climb at VY (at SL) | 1085 fpm | |
Rate of Climb (TOW version)
| IAS | KIAS | |
| Best angle of climb airspeed VX (at SL) | 104 IAS | 57 KIAS |
| Rate of climb at VX (at SL) | 1127 fpm | |
| Best rate of climb airspeed VY (at SL) | 127 IAS | 69 KIAS |
| Rate of climb at VY (at SL) | 1190 fpm | |
Stall Speeds
| IAS | KIAS | |
| Cruise, FLAPS 0 (0°) | 78 | 42 |
| Takeoff, FLAPS 1 (15°) | 68 | 37 |
| Landing – normal, FLAPS 2 (24°) | 64 | 35 |
| Landing – emergency, FLAPS 3 (35°) | 61 | 33 |
Specification
Dimensions
| Wing area | 10.500 m2 | 112.98 ft2 |
| Wing span | 8.926 m | 29.28 ft |
| Overall length | 6.460 m | 21.19 ft |
| Maximum height | 1.850 m | 6.07 ft |
| Wheel base | 1.400 m | 4.59 ft |
| Main landing gear track | 2.240 m | 7.35 ft |
| Maximum propeller diameter | 1.750 m | 68.90 in |
| Mean aerodynamic chord (MAC) | 1.172 m | 3.84 ft |
Engine
| Number of engines | 1 |
| Number of cylinders | 4 |
| Engine manufacturer | BRP-Rotax GmbH & Co KG |
| Engine model number | Rotax 912 ULS2 |
| Engine type | Horizontally opposed, geared, normally aspirated, spark ignition |
| Cooling | Combined liquid and air |
| Maximum takeoff power at 5800 rpm (max. 5 min.) | 73.5 kW / 100 hp |
| Maximum continuous power at 5500 rpm | 69.0 kW / 92.5 hp Propeller |
Propeller (Non TOW version)
| Number of propellers | 1 |
| Propeller manufacturer | PRODUCTION EVRA, Creil, France |
| Propeller model number | EVRA PerformanceLine 175/xxx/805.5 |
| Number of blades | 3 |
| Propeller diameter | 1.750 m (68.90 in) |
| Propeller type | Fixed pitch, ground adjustable |
| Pitch setting (measured 200 mm from blade tip) | 23° |
Propeller (TOW version)
| Number of propellers | 1 |
| Propeller manufacturer | WOODCOMP s. r. o., Odolená Voda, Czech republic |
| Propeller model number | KW-31 |
| Number of blades | 3 |
| Propeller diameter | 1.726 m (67.95 in) |
| Propeller type | In-flight electrically adjustable, constant speed |
| Pitch range | 17° - 30° |
Three View Drawing (Non TOW version)
Three View Drawing (TOW version)
