For a landing on runway 23 (227° magnetic) surface W/V reported by the ATIS is 180/30kt.VAR is 13°E.Calculate the cross wind component?4
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Given:Runway direction 083°(M) Surface W/V 035/35 KTCalculate the effective headwind component?4
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A useful method of a pilot resolving, during a visual flight, any uncertainty in the aircraft's position is to maintain visual contact with the ground and:4
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An aircraft at FL330 is required to commence descent when 65 NM from a VOR and to cross the VOR at FL100. The mean GS during the descent is 330 kt.What is the minimum rate of descent required?4
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An aircraft at FL290 is required to commence descent when 50 NM from a VOR and to cross that VOR at FL80. Mean GS during descent is 271kt.What is the minimum rate of descent required?4
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An aircraft is flying with the aid of an inertial navigation system (INS) connected to the autopilot. The following two points have been entered in the INS computer:WPT 1: 60°N 030°W WPT 2: 60°N 020°WWhen 025°W is passed the latitude shown on the display unit of the inertial navigation system will be:4
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The ICAO definition of ETA is the:4
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(Refer to figure)Complete line 5 of the FLIGHT NAVIGATION LOG, positions "J" to "K". What is the HDG° (M) and ETA?4
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The time difference in Local Mean time between sunset at position A (50°N 120°E) and B (50°S, 120°E) on the 21st of November is:4
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For 1st February the Air Almanac lists the following data: Latitude: 66°00'NMorning civil twilight: 07:56Sunrise: 09:00Sunset: 15:28Evening civil twilight: 16:32The duration of morning twilight at 66°00'N is:4
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