• The Ventura 4 is a monoplane type, with 4 seats, fitted with a high wing supported by struts.
• All metal structure with load resisting panels.
• High lift GA 35 418 Aerofoil with Junkers type flaperon (aileron + flap) with electrical control.
• Trim with electrical control on the elevator and with manual control on the rudder.
• Wing fuel tanks with 2×36 litres capacity in each wing. The tanks are connected and flow into a 16ltr 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.  
• The cockpit is insulated, has upholstery covered seats and a fitted carpet.
• Doors are fully transparent allowing good visibility.
• The cabin arrangement features two upholstery adjustable front seats and 2 rear upholstered seats.
• The luggage compartment situated behind the rear seats is accessible during the flight and can hold up to 45 lbs (20 kilograms).
• The cabin’s ventilation is provided by cabin adjustable air scoops on the side of the forward fuselage.  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 – 7.3m
• HEIGHT – 2.7m
• VCRUISE – 120mph
• WING SPAN – 9M
• VSO STALL CLEAN – 40MPH
• STALL FULL FLAP – 38MPH
• WING CHORD – 1.5M
• VNE – 162MPH
• WING SURFACE- 13.5M2
• CLIMB RATE – 1500fpm (Rotax 915is/Airmaster Propeller)
• ASPECT RATIO- 6
• CABIN WIDTH – 1.16M
• FUEL CONSUMPTION –  @5000RPM = 25LTR P/H (ROTAX 915is)
• EMPTY MASS – 400KG
• USEFULL LOAD = 400KG
• ENDURANCE – 6.4 HR TO EMPTY
• MTOW – 800KG
• TAKE OFF DISTANCE GRASS MSL – 150M
• LANDING DISTANCE GRASS MSL – 100M
• RANGE TO EMPTY – 768MILES
• FUEL CAPACITY 156LTRS
• MAX OP ALT – 23,000FT
• STRUCTURAL LOAD – +3.8/-1.5
• CROSS WIND LIMITATION – 30MPH

PROPELLER – Airmaster 3 blade AP430CTF-WWR72B Electric Variable pitch, Constant Speed Feathering with panel mount controller OR Eprop Glorieuse hydraulic variable pitch, constant speed with panel mount electronic controller.

ENGINE –

1. Rotax 915is 140hp (Turbo charged) with redundant electronic fuel injection and ignition or Rotax 916is 160hp.

INSTRUMENT PANEL DESIGNED AS PER CUSTOMER REQUIREMENT– Options include Garmin G3X 10 or 7″ screens with GSA28 Auto pilot servos, GTR200 Com radio, GTX335 mode S transponder, GMC307/507 audio panel.

RUBBER BOOTS – For easy switch identification.

CONTROL COLUMN – Centre Y stick with Ray Allen G205 stick grip (PTT and elevator trim)

RUDDER PEDALS – Both sides with toe brakes.

FLAP CONTROL – Electric operated via panel toggle switch.

ELEVATOR TRIM – Electric operated via G205 stick grip.

THROTTLE FRICTION – Wicks A820 on both throttles.

PARK BRAKE – Panel mounted.

INTERIOR – Grey epoxy coated with upholstered baggage compartment and floor carpets or rubberised floor.

EXTERIOR AND INTERIOR PRIME AND PAINT – Design as per customer requirement. 

SEAT BELTS – Lap and shoulder harness for rear seats and car type belts for front seats.

LUGGAGE COMPARTMENT – Luggage compartment behind rear seats with 20kgs capacity.

BAGGAGE NET – Covers bag compartment opening.

DOORS – Gull wing type with snap vents in the windows.

TYRES & TUBES – 16×6-6 with or without  spats.

FUEL TANKS – 2x36Ltr tank in each wing with with 16Ltr accumulator behind the passenger seat in the rear fuselage for total of 160Ltr (6 hr endurance)

LEATHER BOOT – For centre control Y stick.

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

• The main landing gear is made up of a single piece aluminium alloy leaf leg.
• The nose landing gear is fitted with a high density rubber ring shock absorber and is steerable during taxiing.
• The Ventura is fitted with disc brakes, with independent left/right toe brakes for the pilot and co-pilot (optional).