A low wing variation of the Zenair CH 601.

Engine: Rotax 912, 80 hp
Wing span: 8.22 m
Wing area: 12.60 sq.m
MAUW: 450 kg
Empty weight: 280 kg
Fuel capacity: 120 lt
Max speed: 205 kph
Cruise speed: 175 kph
Minimum speed: 64 kph
Climb rate: 5 m/s
Seats: 2
Fuel consumption: 12 lt/hr
Price (1998): 78 000 000 L

Savannah is a modified copy of the Zenith Zodiac CH-701 STOL aircraft. I.C.P. srl was once a distributor of the Zenith STOL CH-701. I.C.P. was established in 1980 to produce accessories for the automotive sector. At the beginning of the 1990s, I.C.P. began production of UL aircraft, in collaboration with Agrocopteros of Colombia, including models such as the MXP-740, the MXP-740 Savannah, the MXP-640 Amigo and the MXP-650 Amigo. The Savannah has evolved into the Savannah Turbo, Hydro, ADV, VG (Vortex Generator) and the new Savannah XL which features a wider and more comfortable cabin. A light-weight Savannah is the Bingo, offered with different power units. On 12 September 2009, I.C.P. opened its new factory at Castelnuovo Don Bosco (Province of Asti) in Italy.

The Savannah is an evolved version of the Zenith/Zenair STOL CH701 built by the Italian ICP Company (a one time distributor of the CH701). Some differences include a raised cabin the CH701 has the tapered wing roots, the ICP does not and there are also changes to the tailplane. The NZ MCTOW is 544 kg, as against 520 kg in Australia and the US. It is fitted with two 40 litre wing fuel tanks and burns around 15 litres an hour. Power on stall (without flaps) occurs at about 13 kts and the Savannah will cruise at 85 kts. Newer models have progressive modifications including long-¬range tanks and manual slats, additional avionics, electrics and a Rotax 912ULS with a DUC three blade propeller.

The Savannah is an ultralight STOL aircraft (short takeoff and landing) with two side-by-side seats, single high wing, tricycle landing gear and full metal (alluminium) construction. It shares the same structure of the Bingo, differing just in some minor details, the engines mounted and the equipment.

The Savannah ADV tapered wing with reduced surface has a NACA 2315 profile. In substance, a fast wing that seems to clash with the squared and simple fuselage of the Savannah, and its STOL performance. The stall speed at a MTOW of 560 Kg, in clean configuration, is up to 49 kts and has achieved 44 kts during test. In front, the slats run on linear guides and perfectly re-enter in the leading edge profile, keeping it clean. At the trailing edge are two big flaps with high full deflection angle and another slotted winglet extending for the whole leading edge of the flap itself.

Activation of the flap is by a single electrical control, therefore, for every degree of flaps deflection there is a defined extension of the front slats. The pilot has just one switch to operate and the whole mechanism is automatic. This made it possible to establish the optimal settings during the testing phase, thus avoiding potentially dangerous “personal interpretations” by the pilots and making the airplane safe and simple to manage. So, a single switch activates the four moving surfaces and their position is indicated by a pin moving along an arch drawn out at the root of the right wing, where the electric motor and the mechanical activation system is embedded, but still in sight. The regulation is continuous and in case of emergency a little winch is provided to be connected to the electric motor shaft with a cotter pin. The production aircraft were to be fitted with a permanent winch connected to the motor shaft, in order to allow for immediate activation in case of electrical failure.

The Bingo is an ultralight STOL (short take off and landing) aircraft with side-by-side seats, single high wing, tricycle landing gear, metal construction. It has the same structure as the Savannah, differing just in some minor detials, the engine mounts, cowlings, and equipment.

All models are LSA.

Formerly known in the U.S. as the Skykits Savannah line, Italian maker I.C.P. became represented in the US by ICP Aviation in 2012 and included a tail-dragger version (model “T”) of the all-metal Savannah S-LSA. Twenty-nine of the tricycle-gear S model are registered in the U.S. in 2012. The STOL-capable S-LSA has a high-lift airfoil, Junkers-style flaperons, all-window doors and a true STOL stall speed of 26 knots. S model price 2012: $71,950; T model price 2012: $74,950.

Variation:
Agrocopteros MXP-740

Specifications:

Savannah
Stall: 24 kt / 28 mph / 45 kmh
Cruise: 76 kt / 87 mph / 140 kmh
VNE: 86 kt / 99 mph / 160 kmh
Empty Weight: 272 kg / 600 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 1000 ft/min / 5 m/s
Glide Ratio: 12:1
Take-off distance (50ft obstacle): 330 ft / 100 m
Landing distance (50ft obstacle): 440 ft / 135 m

Savannah (jabiru)
Stall: 23 kt / 26 mph / 43 kmh
Cruise: 70 kt / 81 mph / 130 kmh
VNE: 109 kt / 125 mph / 202 kmh
Empty Weight: 278 kg / 613 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 750 ft/min / 4 m/s
Take-off distance (50ft obstacle): 260 ft / 80 m
Landing distance (50ft obstacle): 260 ft / 80 m
2009 Price: 25000 EURO

Savannah
Engine: Rotax 912S, 100 hp
HP range: 80-120
Length: 21.3 ft / 6.1 m
Height: 2.10 m
Wing span: 29.3 ft / 9m
Wing area: 142 sq.ft / 12,96 sq.m
Wing chord: 144 cm
Aspect ratio: 6,3
Empty weight: 635 lb / 272 Kg
Gross weight: 1234 lb / 560 Kg
Fuel capacity: 21 USG / 80 lt
Wing load: 35 kg/sq.m
Max. speed: 87 – 95 kt
Vne: 108 kt
Cruising speed: 78 – 84 kt
Stall: 28 mph / 23 kt
Approach speed: 31 kt
Manoeuvre speed: 74 kt
Range: 460 sm / 800 km
Rate of climb: 1300 fpm
Takeoff dist: 90 ft
Landing dist: 160 ft
Cockpit width: 41 in
Undercarriage: nose wheel
Wheels: 4×8″
Loading factor: +6/-4g
Fuel consumption 75%: 12 – 14 lt/h
Seating: 2, side by side
Flaperons 0-20-40°

Savannah ADV
Engine: Rotax 912S, 100 hp
HP range: 80-120
Length: 21.3 ft
Wing span: 26.3 ft / 8 m
Wing area: 102 sq.ft / 9.4 sq/m
Wing cord at root: 1.5m
Wing cord at tip: 0.75m
Empty weight: 654 lb
Gross weight: 1234 lb
Fuel capacity: 21 USG
Maximum speed: 112 kts
Cruise: 115 mph / 100 kts
Stall speed clean: 43 kts
Stall speed flaps: 30 kts
Range: 510 sm
Climb rate: 1200 fpm at 52 kts
Takeoff dist: 110 ft / 35 m
Landing dist: 160 ft
Cockpit width: 41 in
Seats: 2
Cockpit width: 41 in
Load factor: +6 -3 g

Savannah Bingo 4S
Engine: HKS 700E, 60 hp
Length: 21.3 ft / 6.1 m
Height: 2.45m
Wing span: 29.5 ft
Wing area: 140 sq.ft
Empty weight: 610 lb / 255 kg
Gross weight: 1234 lb
Fuel capacity: 21 USG
Cruise: 75 mph / 65 kt
Stall: 28 mph / 25 kt
Max speed: 73 kt
Range: 460 sm
Range with reserve: 880 km
Rate of climb: 680 fpm
Takeoff dist: 160 ft / 50 m
Landing dist: 230 ft / 70 m
Cockpit width: 41 in
Landing gear: Nose fixed
Wheel track: 1.7m
Seats: 2
Fuel consumption: 10 lt/hr

Savannah Bingo 4S
Engine: Rotax 503
Wing span: 9m
Wheel track: 1.7m
Empty weight: 245 kg
Stall speed: 25 kt
Cruise speed: 60 kt
Max speed: 70 kt
Take off run: 50 m
Landing roll: 70 m
Climb rate: 480 fpm
Fuel consumption: 15 lt/hr
Range with res: 520 km
MTOW: 450kg
Wing span: 9m
Wheel track: 1.7m
Length: 6.1m
Height: 2.45m

Savannah Bingo 4S
Engine: Rotax 582
Wing span: 9m
Wheel track: 1.7m
Empty weight: 250 kg
Stall speed: 25 kt
Cruise speed: 65 kt
Max speed: 73 kt
Take off run: 50 m
Landing roll: 70 m
Climb rate: 840 fpm
Fuel consumption: 20 lt/hr
Range with res: 410 km
MTOW: 450kg
Wing span: 9m
Wheel track: 1.7m
Length: 6.1m
Height: 2.45m

Savannah Bingo 4S
Engine: Victor 2
Empty weight: 250 kg
Stall speed: 25 kt
Cruise speed: 70 kt
Max speed: 70 kt
Take off run: 50 m
Landing roll: 70 m
Climb rate: 840 fpm
Fuel consumption: 18 lt/hr
Range with res: 500 km
MTOW: 450kg
Wing span: 9m
Wheel track: 1.7m
Length: 6.1m
Height: 2.45m

Savannah Bingo 4S
Engine: HKS Turbo
Wing span: 9m
Wheel track: 1.7m
Length: 6.1m
Height: 2.45m
Empty weight: 265 kg
Stall speed: 25 kt
Cruise speed: 73 kt
Max speed: 84 kt
Take off run: 35 m
Landing roll: 70 m
Climb rate: 960 fpm
Fuel consumption: 12 lt/hr
Range with res: 810 km
MTOW: 450kg

Savannah VG
Cruise: 100 mph
Stall: 30 mph
Range: 460 sm
Rate of climb: 1300 fpm
Takeoff dist: 90 ft
Landing dist: 160 ft
Engine: Rotax 912S, 100 hp
HP range: 80-120
Fuel capacity: 21 USG
Empty weight: 645 lb
Gross weight: 1234 lb
Length: 21.3 ft
Wing span: 29.3 ft
Wing area: 132 sq.ft
Cockpit width: 41 in
Landing gear: fixed nose wheel

The Rambo is of aluminum construction, steel tube cabin, 118 cm wide. It is fitted with an electric elevator trim, carburator deicing, and cabin vent as standard
2009 Price: 33000 EURO
The F99 LSA is a high wing LSA legal craft.

F99 Rambo
Stall: 32 kt / 37 mph / 60 kmh
Cruise: 108 kt / 124 mph / 200 kmh
VNE: 124 kt / 143 mph / 230 kmh
Empty Weight: 285 kg / 628 lbs
MTOW Weight: 475 kg / 1047 lbs
Climb Ratio: 1200 ft/min / 6 m/s
Glide Ratio: 13
Take-off distance (50ft obstacle): 490 ft / 150 m
Landing distance (50ft obstacle): 820 ft / 250 m

F99 LSA
Stall: 50 kt / 58 mph / 93 kmh
Cruise: 125 kt / 144 mph / 232 kmh
VNE: 138 kt / 159 mph / 256 kmh
Empty Weight: 308 kg / 680 lbs
MTOW Weight: 594 kg / 1310 lbs
Climb Ratio: 1100 ft/min / 6 m/s
Glide Ratio: 12
Take-off distance (50ft obstacle): 610 ft / 186 m
Landing distance (50ft obstacle): 700 ft / 213 m

Option 1; kit completely assembled; Option. 2 ready to fly. 2009 Price: US$25900

Engine: Rotax 912 ULS
Propeller: Bolly 3 Blade ground adjustable
Empty Weight: 320 kg / 705 lbs
MTOW Weight: 569 kg / 1254 lbs
Fuel cap: 140 lt
Stall: 42 kt / 48 mph / 77 kmh
Cruise: 100 kt / 115 mph / 185 kmh
VNE: 113 kt / 130 mph / 209 kmh
Fuel burn: 16 lt/hr
Climb Ratio: 1000 ft/min / 5 m/s
Take-off distance (50ft obstacle): 262 ft / 80 m
Landing distance (50ft obstacle): 328 ft / 100 m

The IBIS GS240 is an all-metal, high-wing aircraft manufactured by the IBIS Aircraft company in Colombia. The GS240 has specifications and performance that are within the limitations of the new Light Sport Aircraft category. The GS240 is available for the U.S. market as a “quick-build kit” that will still meet the requirements of the FAA “51% rule” and allow the GS 240 to be put into the Experimental (Amateur-Built) Category. The GS240 kit is intended to provide as short a building time as reasonably possible for the builder, with all difficult aspects of fabrication and assembly having been done at the factory to minimize complications and delay for the first-time builder.
The IBIS GS-240 has specifications and performance that allow it to fit within the new “Light Sport Aircraft” rules. With the GS240 in this category, it can be flown by existing Private and Recreational pilots (without them having to maintain an FAA Medical Certificate), but also by people holding the new “Sport Pilot” license.

Stall: 35 kt / 40 mph / 64 kmh
Cruise: 104 kt / 120 mph / 193 kmh
VNE: 122 kt / 140 mph / 225 kmh
Empty Weight: 341 kg / 752 lbs
MTOW Weight: 599 kg / 1320 lbs
Climb Ratio: 700 ft/min / 4 m/s
Glide Ratio: 14:1
Take-off distance (50ft obstacle): 300 ft / 91 m

Designed for up to 300 lbs and 6.5 ft pilot. Strengthen undercarriage and 30% longer cockpit.

Speed max: 85 mph.
Cruise: 63 mph.
Range: 100 sm.
Stall: 35 mph.
ROC: 800 fpm.
Take-off dist: 200 ft.
Landing dist: 150 ft.
Service ceiling: 12,000 ft.
Engine: Rotax 503, 52 hp.
HP range: 40-65.
Fuel cap: 10 USG.
Weight empty: 600 lbs.
Height: 8.17 ft.
Length: 16.83 ft.
Wing span: 28 ft.
Wing area: 142 sq.ft.
Seats: 1.
Landing gear: nose wheel.