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Type | Sailplane |
---|---|
Manufacturer | DG Flugzeugbau |
Max Takeoff Weight | 750 kg |
Stall Speed | 65 km/h (40 mph, 35 kts) |
Cockpit | Tandem seating |
Max Glide Ratio | 50:1 |
Introduces the flight manual and its purpose for pilots and instructors.
Details the EASA approval and airworthiness requirements for the motorglider.
Provides technical specifications, dimensions, and features of the DG-1000T.
Defines critical airspeed limitations (VNE, VPE, VRA, VA) and their operational significance.
Specifies maximum take-off and landing masses for different categories and ballast configurations.
Lists approved aerobatic manoeuvres for Utility and Aerobatic categories.
Outlines the maximum g-loads that must not be exceeded during flight manoeuvres.
Provides instructions for safely jettisoning the canopy in emergency situations.
Details the procedure for recovering the motorglider from a stall condition.
Explains the steps required to recover from a spin, including rudder and stick control.
Outlines procedures for handling fires in the engine, fuselage, or electrical systems.
Describes actions to take when electrical power is lost during flight.
Covers the process of assembling, disassembling, and filling ballast tanks.
Lists essential checks to be performed before each flight for safety and airworthiness.
Details procedures for aerotow and winch launches, including recommended speeds.
Provides instructions for normal landing procedures, including crosswind and soft field landings.
Outlines approved aerobatic manoeuvres and required entry speeds and g-loads.
Lists stall speeds for various configurations (airbrakes, wing spans) in level flight.
Presents data on minimum sink rate and best glide ratio for different wing loadings and spans.
Details rate of climb, cruising speed, maximum range, and operational altitude.