SR 01 – MAGIC LSA ProTrainer
The SR-01 MAGIC is an all metal aircraft in the LSA (Light Sport Aircraft) category. The single engine low winged aircraft has two seats in tandem.
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Bombardier ROTAX 912 ULS
Woodcomp SR200 three-bladed ground adjustable
Dynon SkyView
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2012 © EURODISPLAY s.r.o. • • •
The SR-01 MAGIC is an all metal aircraft in the LSA (Light Sport Aircraft) category. The single engine low winged aircraft has two seats in tandem.
AIRFRAME
Fuselage with tail units
The fuselage is semi-monocoque and has a conventional formed sheet metal bulkhead, with stringers and metal skin. Major structural items are the front and rear carry-through spars,
to which the wings are attached. The all metal fuselage carries
a fixed steel rod nosewheel and has aluminium main landing gear fitted with differential hydraulic brakes.
The cockpit has two seats in tandem with 4-point seat belts.
The tail assembly consists of a conventional vertical fin, a rudder, and a horizontal stabilizer with an elevator fitted with a trim tab.
Wing
The internally braced wings are constructed with front and rear spars with formed sheet metal ribs, doublers and stringers.
The wings carry conventional hinged ailerons and single-slotted flaps attached to the trailing edges. The flaps have an electrical drive system for 20º and 40º deflections. Inside the wings
are two 70 litre integral fuel tanks.
Interior and exterior
Offered in two trim levels:
• Economy
• Luxury
Fuselage with tail units
The fuselage is semi-monocoque and has a conventional formed sheet metal bulkhead, with stringers and metal skin. Major structural items are the front and rear carry-through spars,
to which the wings are attached. The all metal fuselage carries
a fixed steel rod nosewheel and has aluminium main landing gear fitted with differential hydraulic brakes.
The cockpit has two seats in tandem with 4-point seat belts.
The tail assembly consists of a conventional vertical fin, a rudder, and a horizontal stabilizer with an elevator fitted with a trim tab.
Wing
The internally braced wings are constructed with front and rear spars with formed sheet metal ribs, doublers and stringers.
The wings carry conventional hinged ailerons and single-slotted flaps attached to the trailing edges. The flaps have an electrical drive system for 20º and 40º deflections. Inside the wings
are two 70 litre integral fuel tanks.
Interior and exterior
Offered in two trim levels:
• Economy
• Luxury
Flight controls
The aircraft´s flight control system consists of conventional, manually-operated ailerons, and a rudder and elevator, with the trim tab powered electrically.
Powerplant
The engine and propeller are installed to customer‘s requirements. We offer the aircraft equipped with the Rotax 912 UL (80hp),
the Rotax 912 ULS (100hp) or the Rotax 914 UL (115hp).
In all cases the propeller is ground adjustable.
Avionics and instruments
According to the customer‘s preferences we offer the cockpit
with either analogue or glass instrumentation.
Rescue system
The Stratos - Magnum 601 parachute system is installed
and activated manually from the cockpit.
Download Brochure
The aircraft´s flight control system consists of conventional, manually-operated ailerons, and a rudder and elevator, with the trim tab powered electrically.
Powerplant
The engine and propeller are installed to customer‘s requirements. We offer the aircraft equipped with the Rotax 912 UL (80hp),
the Rotax 912 ULS (100hp) or the Rotax 914 UL (115hp).
In all cases the propeller is ground adjustable.
Avionics and instruments
According to the customer‘s preferences we offer the cockpit
with either analogue or glass instrumentation.
Rescue system
The Stratos - Magnum 601 parachute system is installed
and activated manually from the cockpit.
Download Brochure
STANDARD EQUIPMENT
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Engine
Propeller
Avionics
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Engine
Propeller
Avionics
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Bombardier ROTAX 912 ULS
Woodcomp SR200 three-bladed ground adjustable
Dynon SkyView
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Specifications
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Maximum empty weight
Maximum take off weight (mtow)
(with parachute)
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Dimensions Wing span:
Height:
Length:
Wing area:
Cabin width:
Baggage capacity
Fuel capacity
Average fuel consumption
Load factors
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Performance
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Never exceed speed Vne
Maximum cruise speed Vh
Stall speed No Flaps
Stall speed Full Flaps
Climb rate
Service ceiling
Cruising range
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Take-off distance over 50ft obstacle
Landing distance over 50ft obstacle
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—
Maximum empty weight
Maximum take off weight (mtow)
(with parachute)
—
Dimensions Wing span:
Height:
Length:
Wing area:
Cabin width:
Baggage capacity
Fuel capacity
Average fuel consumption
Load factors
—
Performance
—
Never exceed speed Vne
Maximum cruise speed Vh
Stall speed No Flaps
Stall speed Full Flaps
Climb rate
Service ceiling
Cruising range
—
Take-off distance over 50ft obstacle
Landing distance over 50ft obstacle
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US / Imperial standard
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772 lbs
1,320 lbs
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31´2´´
7´3´´
22´7´´
126.5 sq/ft
2´3´´
22 lb
36.8 US gal (2× 18.4)
30.64 Imp gal (2× 15.32)
3.7 – 4.5 US gal/h
3.1 – 3.75 Imp gal/h
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138 kts / 157 mph
120 kts / 137 mph
42 kts / 26 mph
35 kts / 22 mph
1,100 feet/minute
14,750 ft
1,358 nm
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820 ft
920 ft
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772 lbs
1,320 lbs
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31´2´´
7´3´´
22´7´´
126.5 sq/ft
2´3´´
22 lb
36.8 US gal (2× 18.4)
30.64 Imp gal (2× 15.32)
3.7 – 4.5 US gal/h
3.1 – 3.75 Imp gal/h
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138 kts / 157 mph
120 kts / 137 mph
42 kts / 26 mph
35 kts / 22 mph
1,100 feet/minute
14,750 ft
1,358 nm
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820 ft
920 ft
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Metric
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350 kg
600 kg
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9 446 mm
2 400 mm
6 860 mm
11,732 m2
0,70 m
10 kg
140 litres (2×70 l)
14 – 17 l/h
+6 / -3
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252 km/h
220 km/h
82 km/h
64 km/h
5,5 m/s
4 500 m
2 200 km
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250 m
280 m
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350 kg
600 kg
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9 446 mm
2 400 mm
6 860 mm
11,732 m2
0,70 m
10 kg
140 litres (2×70 l)
14 – 17 l/h
+6 / -3
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252 km/h
220 km/h
82 km/h
64 km/h
5,5 m/s
4 500 m
2 200 km
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250 m
280 m
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2012 © EURODISPLAY s.r.o. • • •PROFESSIONAL DESIGN AND GA WORK QUALITY
