2-person ULM aircraft DW series

piston engine

FLIGHT INSTRUMENTS: Winter Airspeed EBF 0/300 km/h Winter Altimeter EBH (0-10 000 feet, triple pointer) Winter Variometer EBV (+/- 10 m/sec) Winter slip Indicator QMIII Magnetic Compass ENGINE INSTRUMENTS: Analogue Left and Right Fuel Gauges 52mm MGL VEGA EMS2 80mm (RPM; Oil temperature, Oil pressure; Voltage; Hobbs; Manifold Pressure) INTERIOR: Adjustable Seats Conopy Protection Cover Tinted Canopy Luggage Compartment Behind the Seats Adjustable fresh Air System Ignition Key and Magneto Switches Start Button EXTERIOR: Painted in one non metallic colour, based on clients choice FLIGHT CONTROLS: Hydraulic Dual Brakes Rudder Pedals, Steereble Nose Wheel Electric Elevator Trim Electric Flap Control System Flaps And Trim System Indicator Ray Allen G205 Grip Stick on Pilot Side INTRODUCTION The purpose of this document is to provide an airplane basic technical specification (type design) with estimated performance for the purpose of applying for an aircraft type-approval pursuant to UL2 2019 [2]. This regulation is a binding technical document of the DW200 aircraft design. Defines the determination, basic characteristics and technical parameters of the airplane. 1. BRIEF TECHNICAL DESCRIPTION OF THE AIRPLANE The DW200 is a two-seat, self-supporting all-metal low-wing aircraft with side-by-side seats. The landing gear consists of a fixed three-wheel landing gear with a controlled nose wheel. The aircraft is fitted as standard with a four-cylinder four-stroke engine Rotax 912 ULS (100HP) and on the ground adjustable three-blade composite propeller. 1.1 FUSELAGE AND ITS EQUIPMENT The fuselage is a half-shell construction - duralumin cover and duralumin reinforcements.