Ibis Magic GS-700

	IBIS MAGIC GS-700 All Metal Construction
	DIMENSIONS			PERFORMANCE
	Wing Span	29.03‘		Top Speed	120 mph
	Wing Area	133.4 SQ FT		Cruise Speed	115 mph.
	Wing Chord	4.6'		V. N. E.	130 mph
	Aspect Ratio	6.2		Stall Speed No Flaps	48 mph
	Overall Height	7.1‘		Stall Speed W. Flaps	35 mph.
	Overall Length	22.5'		Rate Of Climb	1000 fpm.
	Horizon Tail Span	8.2'		Take-Off Roll	262 ft.
	Horizon Tail Area	22.6 SQ FT		Landing Roll	328 ft
	Horizon Tail Chord	2.8'		Service Ceiling	´+12.000 ft
				Standard Range	350 millas
	WEIGHTS AND CAPACITIES			Standard Endurance	3 h. 30 min.
	Empty Weight	705 Lbs		Fuel Consumption 70% Power	4.6  G.P.H.
	Useful Load	550 Lbs
	Gross Weight	1254 Lbs		DRIVING PLANT
	Design Load Factor	+5/-3 G		Engine Rotax	80Hp - 100Hp - 115Hp
	Cabin Width	42"		Propeller, 3 P. IVO PROP, 912 ULS
	Cabin Height	46"
	Landing Gear	Triciclo
	Landing Gear Width	6.2'		Specifications and Performance figures are based on the factory prototype results.
	Seats	(2) side by side
	Fuel Capacity Standard	20 US gal.

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.