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General| Manufacturer | Diamond Aircraft Industries |
|---|---|
| Crew | 1 |
| Capacity | 3 passengers |
| Type | Light twin-engine aircraft |
| Length | 8.56 m (28 ft 1 in) |
| Height | 2.49 m (8 ft 2 in) |
| Maximum speed | 356 km/h (221 mph, 192 kn) |
| Service ceiling | 5, 486 m (18, 000 ft) |
| Wingspan | 13.42 m |
| Max takeoff weight | 1, 999 kg |
| Engines | 2 × Austro Engine AE300 diesel engines |
| Range | 1, 693 km |
Describes the integrated G1000 avionics system and its functionalities.
Details critical airspeeds for various flight conditions and configurations.
Lists limitations for the engines, including RPM, power, and temperature ranges.
Shows engine instrument markings and their color code significance for TAE 125 engines.
Describes the color and significance of alerts displayed on the G1000 system.
Specifies the aircraft's mass and weight limitations for safe operation.
Defines the Datum Plane and provides limitations for the center of gravity position.
Specifies approved fuel grades and limitations for Jet Fuel and Diesel Fuel.
Explains warnings related to engine parameters displayed on the G1000.
Details various warnings displayed by the G1000 system and their meanings.
Provides procedures for detecting, troubleshooting, and handling one engine inoperative situations.
Details procedures for landing gear unsafe warnings and manual extension.
Provides procedures for handling smoke and fire emergencies on the ground and in flight.
Lists critical airspeeds for various normal operating phases and configurations.
Provides detailed checklists for pre-flight, engine start, taxiing, take-off, and landing.
Comprehensive checklist for cabin, center console, and instrument panel checks before flight.
Checklist for pre-starting engine procedures, including cabin, canopy, and system checks.
Step-by-step procedure for starting the engine, including safety warnings and cautions.
Checklist for pre-take-off procedures, including airplane positioning, restraints, and systems.
Procedure for take-off, including transponder, power lever, elevator, rudder, and airspeeds.
Checklist for approach and landing, covering backrests, harnesses, controls, lights, gear, and trim.
Procedures and cautions for refueling the airplane, including grounding and fuel types.
Procedure for conducting a precautionary landing due to operational factors.
Addresses engine instrument readings outside the normal range (RPM, Coolant, Oil, Gearbox, Fuel Temp, Voltage).
Presents tables and diagrams for various performance aspects of the airplane.
Provides calculated stalling speeds at various flight masses and bank angles.
Presents take-off distances over obstacles and ground roll for various conditions.
Charts showing rate of climb for take-off climb performance.
Performance data for climb with one engine inoperative.
Presents landing distances over obstacles and ground roll for various conditions.
Provides information and methods for calculating flight mass and CG position.
Explains how to calculate loading conditions, including examples and de-icing fluid considerations.
Graphical representation of the permissible center of gravity range for the DA 42.
Provides general specifications and descriptions of the engine, propeller, and related systems.
General specifications for the TAE125 engines, including displacement and power ratings.
Explains the operation of key controls like the power lever, elect. master, and engine master.
Details the engine instruments displayed on the Garmin G1000 MFD.
Describes the fuel system, including main and auxiliary tanks, fuel selector valves, and pumps.
Overview of the aircraft's electrical system, including power generation, storage, and distribution.
Explains the function and operation of the Engine Control Unit (ECU).
Overview of the G1000 integrated avionics system components and features.
Detailed procedures and warnings for refueling the airplane safely.
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