New Pipistrel Explorer SW121A Microlight Aircraft For Sale

The extraordinarily clean aircraft shapes enable flying with minimum power and noise, as well as the lowest fuel consumption, while keeping the performance on the same level or even better. Approved for intentional spins & Night VFR, the Explorer has the best flight characteristics in its category.

Type:
Aircraft (Microlight)
Manufacturer:
Pipistrel Aircraft
Model:
Explorer SW 121A
Year:
New
Serial Number:
TBA
Reg. Number:
TBA
Total Time:
Delivery Hours Only
Seats:
2
Price:
Price upon request

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Price:
Enquire
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 – 6.42 m (21.06 ft)
wingspan – 10.70 m (35.10 ft)
height – 1.90 m (6.23 ft)
wing area – 9.51 m² (102.4 ft²)
mean aerodynamic chord – 0.898 m (2.95 ft)
aspect ratio – 12.04
positive flaps – 0°, +9.5°, +20°; marked (0), (+1), (+2) respectively
negative flaps – -5°; marked as (-)
centre of gravity – 25% – 35% MAC

Weights
design empty weight – 371 kg (818 lb)
max take off weight (MTOW) – 600 kg (1323 lb)
design useful load – 229 kg (505 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 KIAS
stall without flaps – 53 KIAS
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-

Equipment
dual touch-screen glass cockpit
full-featured autopilot
dual radio
ADS-B In & Out
haptic stall-warning
full airframe ballistic parachute rescue system
certified engine capable of running on automotive fuel
certified hydraulic constant speed propeller
airbrakes for rapid descent
glider towing hook
approval for night VFR
approval for intentional spins
adjustable pedals and headrests