TECHNICAL SPECIFICATIONS |
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IBIS MAGIC GS-700 |
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DIMENSIONS |
PERFORMANCE |
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Wing Span |
29.03‘ |
Top Speed |
120 mph |
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Wing Area |
133.4 SQ FT |
Cruise Speed |
115 mph. |
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Wing Chord |
4.6' |
V. N. E. |
130 mph |
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Aspect Ratio |
6.2 |
Stall Speed No Flaps |
48 mph |
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Overall Height |
7.1‘ |
Stall Speed W. Flaps |
35 mph. |
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Overall Length |
22.5' |
Rate Of Climb |
1000 fpm. |
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Horizon Tail Span |
8.2' |
Take-Off Roll |
262 ft. |
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Horizon Tail Area |
22.6 SQ FT |
Landing Roll |
328 ft |
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Horizon Tail Chord |
2.8' |
Service Ceiling |
´+12.000 ft |
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Standard Range |
350 millas |
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WEIGHTS AND CAPACITIES |
Standard Endurance |
3 h. 30 min. |
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Empty Weight |
705 Lbs |
Fuel Consumption 70% Power |
4.6 G.P.H. |
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Useful Load |
550 Lbs |
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Gross Weight |
1254 Lbs |
DRIVING PLANT |
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Design Load Factor |
+5/-3 G |
Engine Rotax |
80Hp - 100Hp - 115Hp |
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Cabin Width |
42" |
Propeller, 3 P. IVO PROP, 912 ULS |
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Cabin Height |
46" |
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Landing Gear |
Triciclo |
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Landing Gear Width |
6.2' |
Specifications and Performance figures are based on the factory prototype results. |
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Seats |
(2) side by side |
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Fuel Capacity Standard |
20 US gal. |
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STANDARD EQUIPMENT LIST AIRCRAFT KIT IBIS MAGIC GS-700
1. FUSELAGE:
1.A- ENGINE SECTION:
Rotax 912 100 hp engine mount complete.
Easily removable engine cowling 2 inpection covers (superior and inferior).
Cover inspection
1.B- CABIN SECTION:
Dual control wheel
Cabin windows in ceiling, cabin windows in rear and laterals window of polycarbonate plastic.
Dual doors (open system up) with polycarbonate plastic and locks with gas spring assisted opening
Firewall super soundproofing.
2. CABIN FEATURES:
Two (2) thick padded and folding seats side by side (adjustable forward and back)
Seats side by side thick padded and upholstered with leather and synthetic material.
Super plush interior floor
Complete carpeting
Cargo tie downs
Windshield of polycarbonate plastic, highly resistant to impacts.
Carpeted interior
Dual adjustable fresh air vents
Rear cabin baggage compartment completely carpeted.
Lap belts three points (pilot & passenger)
Padded and upholstered seats
Rear cabin windows
3. CONTROL SYSTEM FEATURES:
Wings profile naca 650-18m
Wings with fiberglass wing tips (vortelator).
Dual pilot yoke grips control
Wings with flaps and ailerons
Dual aluminum pedals (rudder and nose wheel control)
Wing one stainless steel (chromium-molybdenum )strut with aluminum fairing
Central throttle controls
Left wing landing light
Wing with electrical flaps.
Wing-floor hook in both wings
Left wing pitot tube
In wing light
Wing tip for nav and strobe lights
Fiberglass instrumental panel with 3 section
4. CONTROL SYSTEM:
Horizontal stabilizer (tips)
Small wing for trim tab elevator
Elevator
Rudder
Vertical stabilizer
Dorsal fairing
Differentials wing flaps and ailerons
All moving tail
Removable wings
Landing light
5. LANDING GEAR:
Rugged fixed tricycle gear and nose gear with suspension system with steering nose wheel
Aerodynamic wheel fairings (wheel pants)
Hydraulic disk brakes system pilot side with independent master cylinders
600 x 6" wheels and tires (3)
Dual articulating hydraulic pilot brakes
6. FUEL SYSTEM:
Long range wing fuel tanks (2 units x 9 gl) us gallons
Fuel shut off valve
Visual fuel low level indication system
Low level alert light
7. PAINT:
Dupont polyurethane white lacquer.
Complete frame zinc chromate protection painting
8. MATERIALS:
Ibis ultra light aircrafts are made with aeronautical materials: aluminum alloy 6061–t6, 2024-t3 and 4130 chromium-molybdenum steel; hardware aircraft an; pop rivets avex (avdel-textron), solid aluminum rivets and polycarbonate plastic.