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  • Aerospool Dynamic WT9 EASA LSA

  • Dynamic WT-9 OK Edition

  • Aeropro Eurofox

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  • Aerospool Dynamic WT9

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Aerospool Dynamic WT9 EASA LSA

  • The WT9 Dynamic LSA aircraft is certified according to EASA Certification Specification for Light Sport Aeroplanes
    CS-LSA, Amendment 1 dated 29th July 2013.

PERFORMANCE

Weights

Maximum takeoff weight 600.0 kg 1323 lb
Maximum landing weight 600.0 kg 1323 lb
Maximum empty weight 350 kg 772 lb
Minimum useful load 250 kg 552 lb
Minimum load per seat 55.0 kg 121 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

IAS KIAS
Top speeds at sea level At 5800 rpm 240 130
At 5500 rpm 230 124

Cruise Speeds at Altitudes and Power Setting

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

Fuel Operating Ranges

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 5:9 4:39 4:19 3:45
km 948 944 911 890 856
60 hh:mm 4:8 3:52 3:29 3:14 2:49
km 711 708 683 668 642
40 hh:mm 2:45 2:34 2:19 2:9 1:52
km 474 472 455 445 428
20 hh:mm 1:22 1:17 1:9 1:4 0:56
km 237 236 227 222 214

Rate of Climb

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

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

TECHNICAL 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

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°

Three View Drawing

Aerospool Dynamic WT9 EASA LSA 1

 

kijk voor meer informatie op LSA Aerospool

of neem contact met ons op.

Maastricht-Aachen Airport

Vliegveldweg 148
6199 AD Maastricht-Aachen airport

Contact gegevens

Email: info@cycloonholland.nl
Telefoon: +31 (0) 77 201 87 02
Maintenance: +31 (0) 6 51 68 53 95

Cycloon Holland B.V.

KVK: 52429695
BTW: NL850440919B01
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