PPL(A) PL060 Navigation and radio aids

The aircraft flies with the heading of 330 degrees in windless conditions and crosses the 120 radial from the VOR / DME LIN within 30 NM from DME. The aircraft will be flying:

The aircraft plans to descent at a constant GS. Within 5 minutes the pilot plans to descend from FL 100 to FL050. What should be the descent rate on the VSI? 

The aircraft is moving at a speed of 120 km/h. Wind speed is 30 km/h. The maximum value of drift angle in these conditions is:

The aircraft is moving at a speed of 150 km/h. Wind speed is 30 km/h. The maximum value of the drift angle in these conditions is: 

The aircraft is moving at a ground speed of 150 km / h. In 14 minutes it will cover the distance of: 

The aircraft is moving at a ground speed of 180 km/h. In 18 minutes it will cover the distance of:

The aircraft takes off from the airport located at 1500 ft MSL and climbs vertically at a speed of 600 ft / min. Its average GS is 90 knots and the pressure = 1013.2 hPa QNH. How far from the airport will FL 75 be reached?

The aircraft takes off from the airport elevation 500 ft MSL and rises vertically at a speed of 500 ft / min. Its average cruising speed of 100 knots, and the pressure = 1013.2 hPa QNH. How far from the airport FL 80 is reached?

The aircraft maintains the magnetic heading of 060 degrees. The declination is 8°W, the drift angle is +4°. What is the true track heading of the aircraft?

The GPS system operates in the band ... on the basis of:

The average GS of the aircraft is 150 km/h. In 18 minutes it will fly the distance of:

Sunrise and sunset tables in AIP Poland are provided in chapter:

The on-board device cooperating with the NDB beacon is: 

The on-board device cooperating with VDF direction finder is:

VOR is radionavigation system:

VOR provides the bearing angle for the beacon: 

What is the use of the squawk IDENT?

In what mode is the altitude query sent?: 

In case where the transmitter and receiver move relative to each other (relative motion) there occurs a phenomenon of: 

In the event of COMMUNICATION FAILURE The pilot sets the transponder A mode, code: 

In the event of EMERGENCY The pilot sets the transponder A mode, code:

In the event of HIJACK The pilot sets the transponder A mode, code: 

The standard pressure value is:

The pressure standard is:

The cooperation between the on-board DME with the ground beacons requires:

Assuming that air is incompressible and the location of pressure transmitters on the airplane cause no errors in speedometer indication, TAS is equal to:

The frequency range of the DME radio range-finder is:

The range from which one can receive signals from an NDB ground station is:

Breaking of the wave on the shore (sea/land): 

The descent is planned from the altitude of 7,000 ft so as to reach 1,000 ft AMSL within 6 NM away from the VOR / DME. GS is 180kt and the rate of descent is 1,000ft/min. The distance from the station at the start of descent is:

Time source in the GPS are: