Savannah “SR”
One of the best known ultralights has taken evolution to a new level. Own the newest Savannah “SR” and conquer the third dimension.
With more than 3000 aircraft built in different models, the aviation pioneers behind the Savannah “SR” have taken the feedback of operators everywhere and have incorporated it into the ultimate version of the most loved ultralight by STOL pilots
SAVANNAH “SR”
Detailed Specs
Precision-engineered performance, broken down into the details that matter.
The Savannah Aircraft model ‘SR’ is a monoplane type, with two side-by-side seats, fitted with a high wing supported by struts.
All metal structure with load resisting panels.
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.
Wing fuel tanks with 72 litres capacity in each wing. The tanks are connected and flow into a collection sump placed in the fuselage. A single drain valve at the bottom of the fuselage is provided for fuel sampling.
- The two large removable lateral doors allow easy independent access to the cabin. Ideal for aerial photography.
- The cockpit is insulated, has upholstery covered seats and a fitted carpet.
- Doors are fully transparent allowing good visibility.
- The cabin arrangement features two canvas or upholstery covered side-by-side seats.
- The luggage compartment situated behind the seats is accessible during the flight and can hold up to 45 lbs (20 kilograms).
- The cabin’s ventilation is provided by rotating air scoops on the doors. A dynamic air scoop intended to extract the cabin air is fitted at the top of the baggage compartment.
- Heating system can be orientated on feet or on windshield with control on the dashboard.
- Cabin light.
- Air speed indicator, 3 1/8” with coloured arcs.
- Altimeter, 3 1/8” with setting window.
- Vertical speed indicator, 3 1/8”.
- Magnetic Compass
- Slip and skid indicator
- Tachometer
- Fuel pressure
- Oil pressure
- Oil temperature
- Hour meter
- Voltmeter
- External temperature indicator + airbox (for Rotax 912 ULS only)
- Water temperature for front left engine head.
- Water temperature for back right engine head.
- Length – 6.60m
- Height – 2.60m
- Vcruise (5000 rpm) – 100 knots
- Wing Span – 9.00m
- Vso (Stall – Flaps extended) – 34 knots
- Wing Cord – 1.32m
- Vne – 124 knots
- Wing Surface Area – 11.88 m²
- Climb Rate – 1100 ft/min
- Aspect Ratio – 6.3:1
- Glide Ratio – 11:1
- Cabin Width – 1.11m
- Consumption (5000 rpm) – 18 l/hr
- Empty Mass – 315 kg
- Useful mass 285 kg
- Endurance – 8hr
- MTOW – 600 kg
- Take off distance – 141m MSL
- Landing ground role 170m MSL
- Range (to empty) – 470 miles
- (Long range tanks 900 miles)
- Fuel Capacity – 152 litres
- Max operating Altitude – 14000 ft
- Structural load – (tested) – +4g / -2g
- Cross wind limitation – 26 knots
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 “SR” 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 SR 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?
Speak to our team to configure your aircraft and place your order.