Given:Distance from departure to destination: 210 NM Endurance: 3,5 hTrue Track: 310 W/V: 270/30TAS: 120 kt What is the distance of the PSR from the departure point?4
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Given:Distance from departure to destination: 3750 NM Endurance: 9,5 hTrue Track: 360 W/V: 360/50TAS: 480 kt What is the distance of the PSR from the departure point?4
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Given:Distance from departure to destination: 330 NM Endurance: 5 hTrue Track:170 W/V: 140/25TAS: 125 kt What is the distance of the PSR from the departure point?4
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Which of the following statements is (are) correct with regard to the advantages of computer flight plans ?1. The computer can file the ATC flight plan.2. Wind data used by the computer is always more up-to-date than that available to the pilot.4
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Refer to CAP697 Section 4 - MRJT1 Page 19 Figure 4.5.1 En-route Climb 280/0.74 Given: brake release mass 57500 kgtemperature ISA -10°C head wind component 16 KT initial FL 280Find: still air distance (NAM) and ground distance (NGM) for the climb4
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'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is4
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Refer to CAP697 Section 4 - MRJT1 Page 21 Figure 4.5.1 En-route Climb 280/0.74 (continued)Find: Time, Fuel, Still Air Distance and TAS for an enroute climb 280/.74 to FL 350. Given: Brake release mass 64000 kg, ISA +10°C, airport elevation 3000'4
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On an instrument approach chart, a minimum sector altitude (MSA) is defined in relation to a radio navigation facility. Without any particular specification on distance, this altitude is valid to:4
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Given: true course (TC) 017 W/V 340/30TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS)4
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Refer to CAP 697 Section 2 SEP1 Page 3 Figure 2.1 Time, Fuel and Distance to Climb. Given: Take-off mass 3500 lbs, departure aerodrome pressure altitude 2500 ft,OAT +10°C,First cruising level: FL 140, OAT -5°CFind the time, fuel and still air distance to climb.4
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