Given: CAS 120 kt, FL 80, OAT +20°C. What is the TAS?4
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Given: True Heading = 180° TAS = 500 kt, W/V 225° / 100 kt Calculate the GS?4
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The following information is displayed on an Inertial Navigation System: GS 520 kt,True HDG 090°, Drift angle 5° right, TAS 480 kt. SAT (static air temperature) -51°C. The W/V being experienced is:4
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Given: Compass Heading 090 Deviation 2W Variation 12E, TAS 160 KT Whilst maintaining a radial 070 from a VOR station, the aircraft flies a ground distance of 14 NM in 6 MIN. What is the W/V (T)?4
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Given: TAS = 470 kt, True HDG = 317°, W/V = 045°(T)/45kt. Calculate the drift angle and GS?4
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Given: TAS = 125 kt, True HDG = 355°, W/V = 320°(T)/30kt. Calculate the true track and GS?4
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Given: TAS = 225 kt, HDG (°T) = 123°, W/V = 090/60kt. Calculate the Track (°T) and GS?4
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Given: course required = 085° (T), Forecast W/V 030/100kt, TAS = 470 kt, Distance = 265 NM. Calculate the true HDG and flight time?4
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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 KT. Calculate the effective headwind component?4
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Other exam subjects ATPL - Airline Transport Pilot license