Savannah
Savannah™ S
Savannah™ S is an ultralight aircraft with STOL capability (landing / take-offs on short distances), monoaripa above, the tricycle landing gear, two seats, “side-by-side” full metal (aluminum) .Sute apparatusSavannah ™They are already used worldwide thanks to safety and that confers resistance device structure. Takeoff and landing capabilities make theSavannah ™a plane suitable to use on undeveloped land, but comfort and stability and recommend. long-distance flights.
Savannah™ S innovation is the 2010 ICP company was born from the desire to make Savannah ™ more refined and elegant, thus augmenting aesthetic improvement process already started with Savannah ™ XL, whose front fuselage was completely changed. You add restyling the back of the unit by removing corners, yielding a sinuous curve that gives harmony and completeness whole structure without removing the known characteristics of solidity and sigurantei.Caracteristicile flight are surprising and exceptional combination of vortex generators and flaps offers a comprehensive range of 45-180 km / h. Takeoff and landing distances required simply stunning and unique to this type of ultralight.Aripile remained unchanged.
The new Savannah ™ S is joined to improve earlier:
- Gone with vortex generators, involving a cruising speed up to 180 km / h without compromising the very low employment rate;
- larger dimensions of the cabin, with 11cm wider and 15cm longer with;
- palonierului position adjustable standard or advanced by 10 cm;
- panoramic roof and doors with fully transparent;
- improved aerodynamic profile due to change in engine cowling and the windscreen angle with the fuselage;
- larger instrument panel, positioned above, leaving more space for knees
Specifications
Wing span |
9.00 Mts |
Wing area |
12.67 Sq mts |
Height |
2.58 Mts |
Lenght |
6.60 Mt |
Cockpit ‘A’idth |
1.18 KIE |
Empty weight |
286 Kg |
Maximum take-off weight |
450 Kg |
Maximum project …vieght |
560 Kg |
Load factor |
+6 I -3 g |
Flaps control |
manual/electric |
Luggage capacity |
20 Kg |
Maximum tanks capacity |
a x 36 Lts (+6 Its reserve) |
|
|
Performances
Maximum speed |
193 Km/ph |
Cruising speed |
179 Km/h |
UNE |
2a0 KmTh |
Rate of climb |
1200 ft.imin |
Maximum ceiling |
4000 mts |
Stalling speed with no flaps |
57 Kr/ph |
Stalling speed full flaps |
49 km/ph |
Efficiency |
1/11 |
Takeoff run |
55 mts |
Full flap landing |
70 mts |
Consumption at 75% |
13,5 L/ph |
SAVANNAH VARIANTS SOLD IN KITS READY TO FLY OR IN VARIOUS STAGES
This kit contains all the necessary materials of construction: fuselage, wings with flaperoane and shutters of leading edge, the horizontal tail assembly, the vertical mullions wings, landing gear (fixed) wheels with disc brakes independent tire rooms pedals palonier, leg, flap control lever, controls, control cables ready final loop cut to length and crimped with crimping machine certificate.
All components are produced in series with cutters coordinates (CNC) laser for the dramatic drop in costs and achieving superior quality and total interchangeability of parts without the need for further adjustments.
All cladding sheets are cut to size, bent or pressed, drilled and ready for riveting using rivets existing kit. Small operations deburring of holes may be sometimes necessary. To obtain excellent results, even pneumatic rivet gun is included in the kit, along with some “vices” (cleco) and pliers for this. For a fast and accurate building of approximately 1500 suggest the use of “cleco” that can be purchased individually in addition to the kit. We can repurchase them from you at the same price after completion of construction within 6 months.
Important parts such as pillars wings, parts of fuselage are ready made to facilitate construction.
The kit contains:
- all screws,
- two fuel tanks in the wings 36 liters each, reservoir with 6 liters of the book sensor, the condensation water drain purge, the fuel line to the firewall panel;
- 4-point seat belts;
- two throttle levers;
- plastic heads: wings, ailerons, shutters and tail assemblies;
- templates for setting ailerons, tail assemblies.
To complete the plane longer need:
Support engine / motor fairing / engine / propeller / radiator water and oil / hoses, pipes, fittings engine / tools board / cables / paint / upholstery cockpit.
Estimated time of construction (without paint and mochetare) + 100 hours for mounting the motor and installation labor.
In addition to the kit # 1:
– support Rotax 912 with pads and fixings;
– engine fairing;
– water radiator, oil cooler, spiral metal reinforced hoses, steel pipes for oil, NORMA and ABA clamps type;
– cabin heating system;
– the fuel line after the firewall panel with electric fuel pump, the fuel inlet pressure gauge and a return line, fuel hoses NBR, necklaces norms;
– navigation instruments and motor: speed air 80mm Altimeter 80mm vertical speed 80mm tachometer for Rotax 912 80mm slip indicator, compass, voltmeter, oil pressure, oil temperature, temperature cylinder heads right / left hourmetru temperature in the engine bonnet, fuel pressure;
– Full electrical installation with battery dry contact key “master”, two thermal fuses, switches for various consumers, battery charging bulb, lamp fuel reserve test button, landing light, cabin light, electric rudder trim;
– seat with upholstered.
To complete the plane longer need:
Rotax 912 / water and oil radiators, charge controller, exhaust and propeller.
Estimated time of construction (without paint and Trim) 250 hours.
In addition to the kit # 2: Rotax 912, charging regulator, oil tank, stainless steel exhaust muffler, propeller and propeller cone. Estimated time of construction (without paint and Trim) 250 hours.
Like Kit # 3 with: wings, fuselage, control surfaces ampenajele and ready built and adjusted.
No more than you did: painting, interior upholstery, engine and tools mounted positions.
Note: Other accessories and optional on request.
The Savannah S (Taildragger)
have the same flight characteristics as tricycle version, except that technical landing and takeoff should be adjusted for the rear wheel (skid).
SAVANNAH XL
has the largest cabin, highest instrument panel andperform better!
Savannah ™ XL is part of the group's aircraft fleet ICP in order to make the flight as pleasant as possible due to the generous dimensions of cockpituluiu new, wider than 11cm and panoramic windows that provide visibility and Vortex generators excelentă.Echipat improved aerodynamics line, this ultralight has a cruise speed of 180 km / h, a speed convenient to obtain maxim.Pentru line has been reviewed by tilting the front windshield and more completely redesigning the engine cowling.
Specifications
Wing span |
9.00 Mts |
Wing area |
12.87 Sq mts |
Height |
2.58 Mts |
Lenght |
6.60 Mt |
Cockpit ‘A’idth |
1.18 KIE |
Empty weight |
286 Kg |
Maximum take-off weight |
450 Kg |
Maximum project …vieght |
560 Kg |
Load factor |
+6 / -3 g |
Flaps control |
manual/electric |
Luggage capacity |
20 Kg |
Maximum tanks capacity |
a x 36 Lts (+6 Its reserve) |
|
|
Performances
Maximum speed |
193 Km !’ph |
Cruising speed |
177 Km/h |
VNE |
200 KmTh |
Rate of climb (90km/ph) |
1200 ft.imin |
Maximum ceiling |
4000 mts |
Stalling speed with no flaps |
57 Km/ph |
Stalling speed full flaps |
49 kmp/1-1 |
Efficiency |
1/11 |
Takeoff run |
55 mts |
Full flap landing |
70 mts |
Consumption at 75% |
18,5 L/ph |
Savannah ™ VG
(generator Vortex) was born from the need to have an aircraft with STOL qualities but with a substantial increase in cruise speed and maximum by removing slats-aircraft urilor.Savannah ™ VG is ideal for those who want to combine safety STOL flight with the ability to make longer flights with a cruising speed exceeding 170 km / h.
Specifications
Wing span |
9.00 Mts |
Wing area |
12.87 Sq mts |
Height |
1.58 Mts |
Lenght |
6.25 Mt |
Cockpit ‘A’idth |
1.05 KIE |
Empty weight |
282 Kg |
Maximum take-off weight |
450 Kg |
Maximum project …vieght |
560 Kg |
Load factor |
+6 / -3 g |
Flaps control |
manual/electric |
Luggage capacity |
20 Kg |
Maximum tanks capacity |
a x 36 Lts (+6 Its reserve) |
|
|
Performances
Maximum speed |
192 Km !’ph |
Cruising speed |
173 Km/h |
VNE |
200 Km 11-1 |
Rate of climb (90km/ph) |
1200 ft.imin |
Stalling speed with no flaps |
59 Km/ph |
Stalling speed full flaps |
55 km/h |
Efficiency |
1/11 |
Takeoff run |
55 mts |
Full flap landing |
70 mts |