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DESCRIPTION

CONFIGURATION

KIT IBIS MAGIC GS-700 (S-LSA/VLA)

STANDARD EQUIPMENT LIST AIRCRAFT

DESCRIPTION

1.FUSELAGE:

Metallic monocoque aluminum alloy

1.A- ENGINE SECTION:

Rotax 80-100-115 hp  engine mount complete

Firewall super soundproofing

Cowling – easily removable  2 inspection covers (superior and inferior) in fiberglass

Engine inspections caps  in fiberglass -superior cover – side by side

1.B- CABIN SECTION:

Windshield of polycarbonate plastic, highly resistant to impacts (lexan 2mm)

Dual adjustable fresh air vents (snap vents)

Cabin windows in ceiling and rear of polycarbonate plastic (lexan 2mm)

Cabin laterals window  of polycarbonate plastic (lexan 2mm)

Dual Doors (open system up) with gas spring assisted opening

Dual doors:

Two (2) points closed, front and rear with security and luxury lock

Each door open with the same key on both sides, pilot and copilot, with handles for Easy opening from the inside and outside

Windows of polycarbonate plastic (lexan 2mm)

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 with head rest

Super plush interior cabin floor and baggage floor

Cargo tie downs in baggage

Rear cabin baggage compartment completely carpeted
Lap belts three points (pilot & passenger)

Internal cabin windows in ceiling

Seats and rails completely galvanized, a better and safer sliding in the point of the rails.

Fiberglass instrument panel with 3 section in aluminum sheet

Dual pilot yoke grips control in fiber glass for pilot and copilot

Central  throttle controls

Dual aluminum pedals  for pilot and copilot (rudder and nose wheel control)

Pedals system totally galvanized

Internal yokes and throttle system totally galvanized

3. CONTROL SYSTEM FEATURES:

Wings profile NACA 650-18m

Wings with differential flaps and ailerons and system flaps pipes, galvanized

Fiber glass fairing for root of wings

Fiber glass fairing for aileron tube

Aileron hinged

Wing one steel (chromium-molybdenum )strut with aluminum fairing

Removable wings

Left wing landing light cover with polycarbonate lexan

Wing with electrical flaps with top microswitch

Smaller flaps motor with lid inspection

Wing-floor  hook in both wings and tail

Left wing  pitot tube

Wings with fiberglass wing tips (vortelator) with provision for nav and strobe lights

4. CONTROL SYSTEM:

Horizontal stabilizer with  fiberglass tips

Elevator

Vertical stabilizer with  fiberglass tips
Rudder with  fiberglass tips

Fin for install trim tab elevator (trim tab elevator no included)

Dorsal fairing and

Fiber glass fairing for rudder control cable

Inspection lids in the wings

Inspection lid on the tail of the fuselage

Inspection lid on the vertical stabilizer

Inspection lid on the basis of the horizontal stabilizer

Inspection lid under the fuselage

5. LANDING GEAR:

Rugged fixed tricycle gear and nose gear with suspension system with steering nose wheel

Nose gear and rods pedals totally galvanized

Aerodynamic wheel fairings (wheel pants)

Landing gear legs of aluminum plate 7075-T6

Landing gear with Matco hydraulic brakes system, with wheels, discs, brakes and with independent master cylinders

Three (3) certified wheels and tires 500 x 5″

Dual articulating hydraulic pilot brakes

Springs in the pedals to return to neutral point. (This automatically compensate and assist in focusing the wheel nose gear and rudder).

6. FUEL SYSTEM:

Long range wing fuel tanks (2 units x 9 us gallons each wing) and Reserve tank 2 us gallons with warning sender. Total capacity 20 us gallons

Fuel shut off valve pilot side

Visual fuel low level indication system

7. PAINT:

Internal and external wash primer protection anticorrosive painting

Dupont polyurethane white color

Ibis identification´s logo in pedals, throttle, baggage, safety belts and identification´s plate

The packing  is an steel structure wich making sure that all boxes are insured and are well off inside

8.MATERIALS:

The Ibis aircrafts are made with aeronautical materials: Aluminum alloy 6061–T6, 2024-T3, 7075-T6 and 4130N chromium-molybdenum steel; hardware aircraft AN and MS; pop rivets Avex (Avex-Textron), solid aluminum rivets, polycarbonate plastic lexan UV, carbon fiber, fiberglass volan 150-180-125, electrical cable MIL-W-22758/16,electric terminal 3M, flex stainless steel control cable MIL-W-83420, Matco brakes system, teflon, aeroquip hoses of fuel, stainless stell tridon clamp and dupont paint.

SPECIFICATIONS

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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 ç3 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.        
             

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VIDEOS