Planning Leave a reply0% Planning 1 / 201. Q82 Up to which altitude is an overflight prohibited according to the NOTAM? See figure (PFP-024)Siehe Anlage 18 A) Altitude 9500 m MSL B) Flight Level 95 C) Altitude 9500 ft MSL D) Height 9500 ft 2 / 202. Q54 A pilot wants to take off on runway 36, the reported wind is 240 degrees, 12 knots. What is the value of the wind components acting on the aircraft on take-off and landing? A) Crosswind from the left 6 kt. Tailwind 10.4 kt. B) Crosswind from the right 10.4 kt. Tailwind 6 kt. C) Crosswind from the left 10.4 kt. Tailwind 6 kt. D) Crosswind from the right 6 kt. Headwind 10.4 kt. 3 / 203. Q94 (For this questions, use attachment or CAP697 SEP1 Fig. 2.2 Table 2.2.3) Planning a flight from EDWH (Oldenburg Hatten) to EDWF (Leer Papenburg), the following conditions apply: Cruise level = FL 65 Temperature = ISA+20 Cruise weight = 3400 lbs Power setting = 23.0 in. HG @ 2300 RPM What Indicated Airspeed (IAS) and Fuel Flow (FF) can be expected? (2,00 P.) Siehe Anlage 21 A) IAS = 142 kt FF = 11.5 GPH B) IAS = 158kt FF = 11.5 GPH C) IAS = 145 kt FF = 11.9 GPH D) IAS = 150 kt FF = 12.3 GPH 4 / 204. Q84 What is the nature of the flight shown in the given ATC flight plan? See annex (PFP-051a)Siehe Anlage 19 A) Flight under instrument flight rules. B) Traffic pattern under visual flight rules. C) Night flight under visual flight rules. D) Border crossing flight. 5 / 205. Q74 What is the purpose of “interception lines” in visual navigation? A) They are used as easily recognizable guidance upon a possible loss of orientation B) To visualize the range limitation from the departure aerodrome C) They help to continue the flight when flight visibility drops below VFR minima D) To mark the next available en-route airport during the flight 6 / 206. Q15 The term “center of gravity” is defined as… A) the point at which the total mass of the aeroplane is considered to act. B) the heaviest point on an aeroplane. C) half the distance between the neutral point and the datum line. D) another designation for the neutral point. 7 / 207. Q24 When preparing to carry out the weighing procedure on an aircraft, which of the following is required? A) Drain all engine tank oil B) Remove the batteries C) Remove service equipment D) Drain all useable fuel 8 / 208. Q35 Which is the most recently determined empty mass and the associated center of gravity (CG) arm from the aircraft documentation? See annex (PFP-006)Siehe Anlage 6 A) 512 kg; 285.39 m B) 498 kg; 280.59 m C) 5 kg; 1.3 m D) 4 kg; 1.1 m 9 / 209. Q79 How much taxi fuel must be consumed before take-off to reduce the aircraft mass to the maximum take-off mass? Maximum ramp mass (MRM): 1150 kg Actual ramp mass: 1148 kg Maximum take-off mass (MTOM): 1145 kg A) 4 L B) 3 L C) 5 L D) 2 L 10 / 2010. Q16 The center of gravity (CG) defines… A) the product of mass and balance arm. B) the point on the longitudinal axis or its extension from which the centers of gravity of all masses are referenced. C) the point through which the force of gravity is said to act on a mass. D) the distance from the datum to the position of a mass. 11 / 2011. The result of a front C.G. position is: Increase in stability. Increase in fuel consumption. Increase in stall speed. Increase in range. (1,00 P.) A) 1, 2 B) 1, 2, 3 C) 2, 4 D) 2, 3, 4 12 / 2012. Q9 The empty weight and the corresponding center of gravity (CG) of an aircraft are initially determined… A) for one aircraft of a type only, since all aircraft of the same type have the same mass and CG position. B) by weighing. C) through data provided by the aircraft manufacturer. D) by calculation. 13 / 2013. Q30 Calculated take-off mass = 1082 kg, calculated CG = 0.254 m, fuel burn = 55 l on station 0.40 m. Where is the CG situated after the landing? A) 25.4 cm B) 25.2 cm C) 24.6 cm D) 24.8 cm 14 / 2014. Q39 It is possible that the surface wind speed at an airport is reduced due to friction. When a surface area with a minor tailwind condition is left during the initial climb, the pilot might expect… A) a decrease in airspeed and rate of climb due to increasing tailwind. B) an increase in airspeed and rate of climb due to increasing tailwind. C) an increase in airspeed and rate of climb due to decreasing tailwind. D) a deacrease in airspeed and climb performance due to decreasing tailwind. 15 / 2015. Q22 The balance arm is the horizontal distance between… A) the C.G. of a mass and the datum line. B) the front C.G. limit and the datum line. C) the C.G. of a mass and the rear C.G. limit. D) the front C.G. limit and the rear C.G. limit. 16 / 2016. Q27 What mass equals 102 litres of Avgas 100LL? A) 74 kg B) 142 lbs C) 74 lbs D) 142 kg 17 / 2017. Q19 The term “moment” with regard to a mass and balance calculation is referred to as… A) quotient of a mass and a balance arm. B) product of a mass and a balance arm. C) sum of a mass and a balance arm. D) difference of a mass and a balance arm. 18 / 2018. Q26 The position of the center of gravity equals… See figure (PFP-052e)Siehe Anlage 1 A) 142 in. B) 147.5 in. C) 137.5 in. D) 145.7 in. 19 / 2019. Q57 A pilot wants to take off on runway 36, the reported wind is 240 degrees 12 knots. What are the wind components acting on the aircraft on take-off and landing? A) Crosswind from the right 6 kt. Headwind 10.4 kt. B) Crosswind from the right 10.4 kt. Tailwind 6 kt. C) Crosswind from the left 10.4 kt. Tailwind 6 kt. D) Crosswind from the left 6 kt. Tailwind 10.4 kt. 20 / 2020. Q101 (For this question, please use annex PFP-063) According ICAO, what symbol indicates a general spot elevation? (2,00 P.) Siehe Anlage 24 A) C B) A C) B D) D Your score is 0%