Technical Specific — Sample Paper 1

The centre of gravity is calculated as:

The yellow arc (caution range) on the ASI covers:

Engine indications are available on the display only when:

The pressure accumulator used for unfeathering is charged to approximately:

The maximum take-off mass of the standard aircraft is:

The wheel brakes are:

The autopilot fitted is:

Which of the following will cause the autopilot to disconnect automatically?

The main battery is rated at:

When towing with a tow vehicle, the nose wheel must not be turned more than:

The correct order for an emergency gear extension is:

The operating manoeuvring speed VO above 1800 kg is:

The caution L/R ALTN FAIL indicates:

With a fuel selector set to CROSSFEED, that engine draws fuel from:

On the flight display, an autopilot mode shown in green indicates it is:

The overall height of the aircraft is:

The total usable fuel in the two main tanks is approximately:

With flaps in the APPROACH or LANDING position, the load factor limits are:

The blue radial line on the airspeed indicator represents:

During single-engine flight, the correct technique is to:

The avionic bus is connected to the right main bus through:

Take-off power may be used for a maximum of:

The maximum coolant temperature is:

The number of propeller blades fitted to each engine is:

The red gear warning light illuminates when the landing gear is:

The negative manoeuvring load factor at VO is:

The datum plane is located:

The maximum demonstrated crosswind component is:

The engines are started using:

Take-off is not permitted with a fuel selector in which position(s)?

The engines fitted to the DA-42 NG are:

Exceeding the maximum take-off mass results in:

The maximum oil pressure is:

After an engine failure the aircraft should be flown at:

The aural gear warning horn sounds when the landing gear is retracted and a power lever is brought below approximately:

The caution L/R COOL LVL indicates:

Which bus is connected directly to the main battery and cannot be switched off?

The maximum load in the nose baggage compartment is:

Maximum take-off power is:

The L/R FUEL LOW caution appears when the usable fuel in that tank falls to about:

The maximum gearbox temperature is:

Intentional negative-g manoeuvres are:

The maximum landing mass of the standard aircraft is:

The maximum continuous RPM is:

The standby attitude module is powered for at least 1.5 hours by:

The maximum permitted alternator load (amperage) is:

The mean aerodynamic chord (MAC) is:

The fuselage of the DA-42 NG is of which construction?

The leading edge sweep of the wing is:

A fire warning for an engine is triggered when the engine compartment temperature exceeds approximately: