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Alternative Image(s) :
Ekolot JK-05L Junior
Note:
No notes for this product
Product Number:
LSA
Country/Territory:
South Africa
Contact Person:
Richard Stubbs
Telephone Number:
083 655 0355
e-Mail Address:
richardstubbs@mweb.co.za
Website Address:
www.aircraftafrica.co.za
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Description
Specification
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The
Ekolot JK-05L Junior
is a
Polish
ultralight aircraft
, designed and produced by
Ekolot
of
Krosno
. It was certified in Poland in February 2010. The aircraft is supplied as a kit for
amateur construction
or as a complete ready-to-fly aircraft.
Design and development
The JK-05L was designed to comply with the
Fédération Aéronautique Internationale
microlight rules. It features a
strut-braced
high wing
, an enclosed cockpit with two seats in
side-by-side configuration
, fixed
tricycle landing gear
and a single engine in
tractor configuration
.
The aircraft is made from composites. Its 10.68 m (35.0 ft) span wing employs an NN-1817
airfoil
, has an area of 10.24 m
2
(110.2 sq ft) and employs
carbon fibre
flaperons
. The twin 35 litres (7.7 imp gal; 9.2 US gal) fuel tanks are located behind the seats. A
ballistic parachute
is available. The controls include a single, centrally-mounted
centre stick
and electric trim. The standard engine is the 80 hp (60 kW)
Rotax 912UL
four-stroke
powerplant.
The JK-05L was later developed into the
Ekolot KR-030 Topaz
.
General characteristics
Crew:
one
Capacity:
one passenger
Length:
5.7 m (18 ft 8 in)
Wingspan:
10.76 m (35 ft 4 in)
Height:
2.25 m (7 ft 5 in)
Wing area:
10.2 m
2
(110 sq ft)
Airfoil
:
NN-1817
Empty weight:
290 kg (639 lb)
Gross weight:
450 kg (992 lb)
Fuel capacity:
70 litres (15 imp gal; 18 US gal)
Powerplant:
1 ×
Rotax 912UL
four cylinder, liquid and air-cooled,
four stroke
aircraft engine
, 60 kW (80 hp)
Performance
Maximum speed:
200 km/h (124 mph; 108 kn)
Cruising speed:
180 km/h (112 mph; 97 kn) at 75% power
Stall speed:
55 km/h (34 mph; 30 kn) flaps down
Range:
1,000 km (621 mi; 540 nmi)
Rate of climb:
6 m/s (1,200 ft/min)
Wing loading:
41 kg/m
2
(8.4 lb/sq ft)
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