New Pipistrel Velis Club Microlight Airplane For Sale

Glider towing capability, constant-speed propeller, heavy-duty landing gear, exceptional outside visibility, and reliable avionics. Ideal for all-round pilot training as a complement of the Velis Training System, but can be enjoyed separately as well.

Type:
Aircraft (Microlight)
Manufacturer:
Pipistrel Aircraft
Model:
Velis Club
Year:
New
Serial Number:
TBA
Reg. Number:
TBA
Total Time:
Delivery Hours Only
Seats:
2
Price:
Price upon request

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Price:
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Aircraft Model & Manufacturer:
Year:
2023
Total Time:
1
Registration Number:
TBA
Serial Number:
TBA
Seats:
2
Aircraft Location:
Contact Name:
Taja Boscarol
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Description

Engine
Rotax 912 S3, EASA certified engine
Max Power – 100 hp, 73.5 kW

Propeller
2-blade Hydraulic CS MTV-33-1-A/170-200 EASA certified

Dimensions
length – 6.40 m (21.0 ft)
wingspan – 10.70 m (35.10 ft)
height – 2.06 m (6.75 ft)
wing area – 9.51 m² (102.4 ft²)
positive flaps – 0°, +9.5°, +20°; marked (0), (+1), (+2) respectively
negative flaps – -5°; marked as (-)

Weights
design empty weight – 340 kg (750 lb)
max take-off weight (MTOW) – 600 kg (1323 lb)
design useful load – 260 kg (573 lb)
max baggage weight – 25 kg (55 lb)
fuel tanks capacity – 2 x 50 l
useful fuel – 2 x 49.5 l

Performance
never exceed speed, VNE – 163 KTAS
max structural cruising speed, except in smooth air, VNO – 120 KIAS
max operating manoeuvring speed, VA – 100 KIAS
max flaps extended speed, VFE – 81 KIAS
max airbrakes extended speed, VAE – 100 KIAS
stall speed with flaps, VS0 – 47 KCAS
stall speed without flaps, VS – 53 KTAS
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 – 5.33 m/s (1050 ft/min)
take off distance at SL – 160 m (525 ft)
take off distance over 15 m obstacle at SL – 320 m (1,050 ft)
maximum take-off altitude – 3048 m (10,000 ft) MSL
maximum operating altitude – 5486 m (18,000 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 (4.86 gal/h)
endurance @4000 ft., 65 % power) – 5 h 33 min (+30 min reserve)
range distance (+ 30 min reserve, @4000 ft., 65 % power) – 1189 km (642 nmi)
noise level – (ICAO Annex 16, Chapter 10) 70 dB(A) (measured)
flight load factor limits – +4.0 g, -2.0 g