Savannah S
The Savannah™ S is the 2010 novelty from I.C.P., born from the desire to make the Savannah™ more refined and elegant and therefore complete the process of aesthetic improvement.
This version put the focus the rear part of the aircraft, leaving the wings unchanged, which have always proven to be the Savannah’s strong point, especially in the version with vortex generators, thanks to the combination of the high wing surface area with the profile high lift.
SAVANNAH S
Detailed Specs
Precision-engineered performance, broken down into the details that matter.
- The Savannah™ S is a monoplane type, with two side-by-side seats, fitted with a high wing supported by struts.
- The airframe structure is a full-metal one with load-resisting panels.
- The wing presents a “high lift” NACA 650-18 modified airfoil with Junkers type flaperon (aileron + flap) with manual or electrical (optional) control.
- Trim with electrical control on the elevator and with manual control on the rudder.
- It’s possible to install a parachute “Junkers 500” type.
- The tanks are installed into the wings and have 36 litres capacity each. They are communicating and flow into a collection sump, placed in the fuselage, provided with drain valve and with fuel reserve indicator connected to a push-to-test light.
- The two large lateral doors allow an easy independent access to the cabin and they may be removed for flying in hot regions or to take pictures.
- The cockpit is completely sound insulated and covered with upholstery or fitted carpet.
- For a better visibility, the doors and the roof are fully transparent.
- The cabin arrangement features two canvas or upholstery covered side-by-side seats.
- The luggage van, situated behind the seats and accessible during the flight, may contain up to 45 lbs (20 kilograms)
- The cabin’s ventilation is provided by an opening between the doors and the upper part of the cabin door frame. A dynamic air scoop intended to extract the cabin air is fitted at the bottom of the baggage compartment. It’s possible to improve the cabin ventilation by using two rotating air scoops in the doors windows.
- Heating system can be orientated on feet or on windshield with control on the dashboard.
- Cabin light.
- Anemometer D. 3 1/8” with coloured arcs
- Altimeter D. 3 1/8” with setting window
- Variometer D. 3 1/8”
- Compass
- Slip and skid indicator
- Tachometer
- Fuel pressure
- Oil pressure
- Oil temperature
- Hourmeter
- Voltmeter
- External temperature indicator + airbox (for Rotax 912 ULS only)
- Water temperature in front left engine head
- Water temperature in back right engine head
- Anemometer D. 3 1/8” with coloured arcs
- Altimeter D. 3 1/8” with setting window
- Variometer D. 3 1/8”
- Compass
- Slip and skid indicator
- Tachometer
- Fuel pressure
- Oil pressure
- Oil temperature
- Hourmeter
- Voltmeter
- External temperature indicator + airbox (for Rotax 912 ULS only)
- Water temperature in front left engine head
- Water temperature in back right engine head
- Wing span: 9.0 Mts
- Wing area: 12.87 Sq mts
- Height: 2.58 Mts
- Length: 6.60 Mts
- Cockpit width 1.18 Mts
- Empty weight: 286 Kg
- Maximum take-off weight: 450 Kg
- Maximum project weight: 560 Kg
- Load factor: +6 / -3 g
- Flaps control: manual/electric
- Luggage capacity: 20 Kg
- Maximum tanks capacity: 2 x 36 Lts (+6 lts reserve)
- PROPELLER – 3 blade Durandal E-PROP composite with built in leading edge protection – 2000hrs TBO OR DUC Swirl – 3 blade carbon fibre
- ENGINE – Rotax 912 ULS 100 hp with mechanical and backup electric fuel pumps and dual ignition. OR Rotax 912IS – 100hp Fuel Injected
- STANDARD INSTRUMENT PANEL – Airspeed indicator, Vertical speed indicator, magnetic compass, skid and slip indicator, tachometer, fuel pressure, oil pressure, oil temperature, hour meter, volt meter, external and airbox temperature, 2 x water temperature for left and right cylinder heads, 2 x throttle control, choke and carb heat.
- RADIO – TQ KRT2
- TRANSPONDER – TQKTX2S
- RUBBER BOOTS FOR PANEL SWITCHES.
- DUAL USB CHARGING PORT.
- CONTROL COLUMN – Centre Y stick with Ray Allen G101 stick grip (PTT button only)
- RUDDER PEDALS – Both sides with toe brakes on pilot side only.
- PARK BRAKE
- FLAP CONTROL – Manual with half and full flap settings.
- ELEVATOR TRIM – Electric elevator trim operated via toggle on panel.
- THROTTLE FRICTION – Wicks A820
- INTERIOR – Charcoal upholstered with black floor carpets and black upholstered high-density foam seats.
- EXTERIOR AND INTERIOR PRIME AND PAINT – Spray painted with exterior primer, painted with a standard two-tone design.
- SEAT BELTS – 4 Point quick release harness.
- LUGGAGE COMPARTMENT – Extended luggage compartment behind seats with 20 kg capacity.
- BAGGAGE NET – Keeps bags securely in the baggage compartment.
- DOORS – Gull wing type with snap vents in the windows.
- TYRES – Air Track 16″
- FUEL TANKS – 2×36 Ltr tanks in each wing with 6 L accumulator behind the passenger seat in the rear fuselage for total of 152 Ltrs
- (8 HR ENDURANCE)
- ROOF – Aluminium with viewing window.
- LIGHTS – LED landing light on left wing and interior cabin light.
- DECAL – Standard vinyl registration markings and
- Savannah S on wing tips.
UPGRADES/OPTIONAL EXTRAS
- Auto Pilot servos(Garmin or MGL)
- EFIS (Garmin or MGL)
- Dual Brakes
- Dual Controls (Between knees)
- G205 Stick grips (5 switch)
- Electric flaps.
- Custom paint and decals
- High intensity LED landing light for night VFR.
- Wing tip strobes and nav lights
- Tail strobe
- 21″ aero classic tubeless tyres
Savannah S also available in kit form for home-builders.
Compare Engine Options
Side-by-side specifications to help you choose the right engine
DESCRIPTION:
- 4-cylinder.
- 4-stroke liquid/air-cooled engine with opposed cylinders.
- Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet.
- 2 carburetors.
- Mechanical fuel pump.
- Dual-electronic ignition.
- Electric starter.
- Propeller speed reduction unit.
- Air intake system.
PERFORMANCE:
- 73.5 Kw @ 5800rpm.
- Torque – 128 nm @ 5100 rpm.
- Max Rpm – 5800.
- Bore – 81 mm.
- Stroke – 61mm.
- Displacement – 1351cm3.
- Weight – 69.4 kg-Engine with prop speed reduction unit.
- Overload clutch, Exhaust system, external alternator, engine suspension frame, air guide hood, and oil cooler.
- Fuel – min. MON 85 RON 95* min. AKI.
DESCRIPTION:
- 4-cylinder.
- 4-stroke liquid/air-cooled engine with opposed cylinders.
- Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet.
- Fuel Injected.
- Dual-electronic ignition.
- Electric starter.
- Propeller speed reduction unit.
- Air intake system.
PERFORMANCE:
- 73.5 Kw @ 5800rpm.
- Torque – 128 nm @ 5100 rpm.
- Max Rpm – 5800.
- Bore – 84 mm.
- Stroke – 61mm.
- Displacement – 1352cm3.
- Weight – 63.6 kg-Engine with prop speed reduction unit.
- Overload clutch, Exhaust system, external alternator, engine suspension frame, air guide hood, and oil cooler.
- Fuel – min. MON 85 RON 95* min. AKI.
USE CASES
We are the go-to aviation company for conservation, anti-poaching, flight schools, and private pilots – providing affordable, easy to maintain, and high quality solutions for all these use cases.
Ready for the Savannah “SR” experience? Let us help you choose – because we aim to provide a certified experience in a non-certified world ™
Speak to our team to configure your aircraft and place your order.