問題一覧
1
Which statement is correct with regards to polar Axis of the Earth
The polar axis of the Earth causes the geographic South Pole and geographic north pole and is perpendicular to the plane of equator
2
An aeroplane flies from Hanover (52°28'n 009°59'E) to Kiel (5423'N, 009°59'E) on a northerly heading. What is the distance between Hanover and Kiel?
115nm
3
What is the distance between two parallels of longitude 9° east and 10° east on the parallel of the latitude 50° north?
60km
4
1700 central European time equals
1600utc
5
Determine sunrise defined as
The point in time when the observer of the first time on the particular day is able to see the upper edge of the sun disc
6
The term Civil Twilight is defined
The period of time before sunrise or after sunset where the midpoint of the sun disc is 6° or less below the true horizon
7
Which formula is correct to calculate the magnetic course?
Mc =tc-var
8
Tc 184 wac 011 mh 198 ch 200 what is the th and dev
th=194 dev=-002
9
The term agonic line is defined as the line on earth or an aeronautical chart connecting all points with
Variation of 0
10
How are the rhumb lines and great circles did depicted on the direct Mercator chart
rhumb lines straight lines great circles curved lines
11
Which answer states the correct correlation between number and Chart symbols
1 vor 2 vor/dme 3 vortac 4 nbd
12
An elk travels 100 nautical miles in 56 minutes the ground speed equals
198kmh
13
Calibrated airspeed 155 kt flight level 80 outside air temperature -15°C the true airspeed equals
170kts
14
Ground speed 160 KT true course 177° wind vector 140°/20 KT true heading equals
173
15
An aircraft is following a true head of 290° at the true or speed of 150 KT the wind vector is 260°/20 KT true course equal
294
16
What is the meaning of the 1:60 rule?
1NM latte offset at 1° drift after 60 NM
17
Radio waves within the VHF range EG VOR travel as
Quasi optical wave
18
QDM 279 var 5w dev 5e the QDR equals
099°
19
The term QTE means
True bearing from the station to the aircraft
20
The range of a VOR is highly affected by
Transmitter and receiver altitude