The Savannah Aircraft model ‘S’ 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 36 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.

• Length – 6.60 m
• Vmax (5500 rpm) 115 mph
• Height – 2.58 m
• Vcruise (5000 rpm) – 100 mph
• Wing Span – 9.00m
• Vso (Stall – Flaps extended) – 30 mph
• Wing Cord – 1.43m
• Vne – 143 mph
• Wing Surface Area – 12.84 m²
• Climb Rate – 1100 ft/min
• Aspect Ratio – 6.3:1
• Glide Ratio – 11:1
• Cabin Width – 1.09 m
• Consumption (5000 rpm) – 18 l/hr
• Empty Mass – 300 kg
• Useful mass 300 kg
• Endurance – 8hr

• MTOW – 600 kg
• Take off distance – 35m MSL
• Landing distance 50m MSL
• Range (to empty) – 470 miles
• (Long range tanks 900 miles)
• Fuel Capacity – 152 litres

• Max operating Altitude – 14000 ft
• Structural load – (tested) – +6g / -4g
• Cross wind limitation – 30 mph

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

RUBBER BOOTS FOR PANEL SWITCHES.

GLOVE BOX AND AUX POWER POINT.

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.

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 – Lap and shoulder harness both seats.

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 & TUBES – Air Track Tyre 6.00-6 6 PR Certified.

FUEL TANKS – 2×36 Ltr tanks in each wing with 8 L accumulator behind the passenger seat in the rear fuselage for total of 152 Ltrs

(8 HR ENDURANCE)

ROOF – Aluminium.

LIGHTS – LED landing light on left wing and interior cabin light.

DECAL – Standard vinyl registration markings and

Savannah-S on wing tips.