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Manufacturer | Robin Aircraft |
---|---|
Model | DR400/140B |
Type | Light aircraft |
Engine | Lycoming O-320-D2A |
Wingspan | 8.72 m (28 ft 7 in) |
Length | 6.96 m (22 ft 10 in) |
Seating Capacity | 4 |
Max Takeoff Weight | 1, 000 kg |
Stall Speed | 95 km/h |
Fuel Capacity | 110 liters |
Horsepower | 160 hp (119 kW) |
Height | 2.23 m (7 ft 4 in) |
Describes the engine manufacturer, models, displacement, cooling, and FADEC system.
Lists airspeed limitations for never exceed, normal operation, maneuvering, and flaps extended conditions.
Defines the allowable flight load factors at maximum weight with flaps up and down for different categories.
Specifies the maximum allowed takeoff and landing weights for categories "U" and "N".
Specifies engine manufacturer, model, power output, and RPM limits for takeoff and continuous operation.
Provides procedures for engine failure during takeoff roll and flight, and landing without power.
Details the steps to attempt an engine restart after a failure, considering altitude and conditions.
Details procedures for FADEC malfunctions, distinguishing between single and dual FADEC lamp warnings.
Covers procedures for engine fires on the ground and in flight, including extinguishing methods.
Outlines steps to take in case of an electrical fire, including equipment shutdown and landing preparation.
Explains actions for electrical power supply malfunctions, including alternator failure and FADEC backup battery operation.
Details the procedure to recover from an inadvertent spin by adjusting controls and rudder.
Describes the pre-flight inspection procedure to be performed before each flight.
Provides a step-by-step guide for starting the aircraft engine, including checks and warnings.
Lists essential checks and settings to be completed before takeoff.
Covers normal, short, and crosswind takeoff procedures, including speeds and flap settings.
Details normal climb speeds (best rate and angle) and actions for high temperatures.
Covers short landing, overshoot procedure, and actions after landing.
Presents takeoff distances at maximum weight under different pressure altitudes and temperature conditions.
Provides landing distances based on altitude, temperature, and runway conditions.