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Exam simulation Flight Performance and Planning - PPL(H) - Private Pilot Licence (Helicopter)

Exam simulation PPL(H) Helicopter Theory Exam Questions in English Flight Performance and Planning 120 questions on 120 minutes

1 - Why is fuel burn monitoring important for a PPL(H) flight?
2 - What is the nature of the flight shown in the given ATC flight plan? Use figure (PFP-051a)
question PFP-051a.webp
3 - The term "FATO" is defined as...
4 - The required data for a mass and balance calculation including masses and balance arms can be found in the...
5 - The maximum endurance with a helicopter is achieved by flying at...
6 - Why must an aircraft be loaded so that the centre of gravity (CG) remains within the approved limits during all phases of flight?
7 - Which statement about fuel planning is correct?
8 - The centre of gravity has to be located...
9 - Which action best supports safe management of temperature correction?
10 - The term "datum" with regard to a mass and balance calculation defines...
11 - A helicopter burns 33 l/h. Planned flight time is 75 minutes and required reserve is 20 l. What minimum fuel should be planned?
12 - Which statement about centre of gravity forward of limit is correct?
13 - A helicopter burns 34 l/h. Planned flight time is 50 minutes and required reserve is 20 l. What minimum fuel should be planned?
14 - The planned distance is 100 NM and groundspeed is 120 kt. What is the approximate flight time?
15 - The total weight of an aircraft is acting vertically through the...
16 - Which factor has a positive effect on the power required?
17 - During a flight, a flight plan can be filed at the...
18 - (For this question, please use annex PFP-063) According to ICAO, what symbol indicates a general spot elevation?
question PFP-063.webp
19 - Why does the VNE decrease with increasing pressure altitude?
20 - The basic empty mass of an aircraft includes...
21 - The upper limit of LO R 4 equals... Use figure (PFP-030)
question PFP-030.webp
22 - What is the maximum helicopter mass to conduct a hover in ground effect at 9000 feet pressure altitude and an outside air temperature of +10° C? Use figure (PFP-045)
question PFP-045.webp
23 - Why is temperature correction important for a PPL(H) flight?
24 - Basic empty mass is 720 kg, occupants are 80 kg and 65 kg, usable fuel for departure is 35 kg and MTOM is 920 kg. Is the mass within limits?
25 - 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
26 - The planned distance is 45 NM and groundspeed is 90 kt. What is the approximate flight time?
27 - According to the aeronautical chart, Friesach/Hirt (LOKH) has a 707 m grass runway. The preferred runway is 17 due to a surface wind of 180°/10 kt. The required landing distance for your aircraft under the present conditions is 550 m. Considering the NOTAM below, is it safe to plan LOKH as an alternate aerodrome? Use figure (PFP-026)
question PFP-026.webp
28 - Which action best supports safe management of pressure altitude?
29 - Basic empty mass is 810 kg, occupants are 85 kg and 60 kg, usable fuel for departure is 45 kg and MTOM is 980 kg. Is the mass within limits?
30 - Why is baggage location important for a PPL(H) flight?
31 - Which statement about slope operations is correct?
32 - The position of the centre of gravity equals... Use figure (PFP-052e)
question PFP-052e.webp
33 - The term "moment" with regard to a mass and balance calculation is referred to as...
34 - Which actions should be taken if the orientation is lost during helicopter flight operations?
35 - Which action best supports safe management of take-off power margin?
36 - The conversion factor from kilogram [kg] into pounds [lb] is...
37 - What is the never-exceed speed at 4000 feet pressure altitude, +10° C outside air temperature and a helicopter mass of 2300 lbs? Use figure (PFP-046)
question PFP-046.webp
38 - Why is obstacle clearance important for a PPL(H) flight?
39 - Which statement about headwind for take-off is correct?
40 - What is the message of the NOTAM shown below? B7938/25 NOTAMN Q) LECB/QMRLC/IV/NBO/A /000/999/3933N00244E005 A) LEPA B) 2511212200 C) 2511220500 E) RWY 24L/06R CLOSED
41 - Which statement about hover out of ground effect is correct?
42 - A helicopter burns 28 l/h. Planned flight time is 80 minutes and required reserve is 25 l. What minimum fuel should be planned?
43 - (For this question, please use annex PFP-061) According to ICAO, what symbol indicates a group of unlighted obstacles?
question PFP-061.webp
44 - The calculated take-off mass is 750 kg and the total moment is 625 000 kg mm (equivalent to 625 kg m). Which numbered cross represents this loading? Use figure (PFP-003); its metric horizontal scale is moment divided by 1 000.
question PFP-003.webp
45 - Which statement about tailwind for landing is correct?
46 - The term "balance arm" in the context of a mass and balance calculation defines the...
47 - Increasing a helicopter's mass will...
48 - How should tailwind be considered during helicopter performance planning?
49 - Considering the following fuel data, how much trip fuel is required? Fuel for start-up and taxi: 5 L Fuel for take-off and climb: 12 L Fuel for cruise flight: 25 L Fuel for descent, approach and landing: 7 L Fuel for taxi and parking: 3 L Fuel to alternate: 13 L Final reserve fuel: 10 L
50 - Given values: Calculated take-off mass = 746 kg calculated CG = 37.1 cm fuel burn = 30.5 l on station 45 cm. Where is the CG situated after the landing?
51 - The centre of gravity (CG) defines...
52 - The planned distance is 54 NM and groundspeed is 108 kt. What is the approximate flight time?
53 - When landing, if the TAS is significantly less than the ground speed, you will have...
54 - What factor is affected by headwind during a departure?
55 - Which action best supports safe management of alternate planning?
56 - Baggage and cargo must be properly stowed and fastened, otherwise a shift of the cargo may cause...
57 - Which statement about centre of gravity aft of limit is correct?
58 - Why is alternate planning important for a PPL(H) flight?
59 - The empty weight and the corresponding centre of gravity (CG) of an aircraft are initially determined...
60 - Which action best supports safe management of landing performance margin?
61 - How should crosswind be considered during helicopter performance planning?
62 - Why is pressure altitude important for a PPL(H) flight?
63 - 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?
64 - The planned distance is 84 NM and groundspeed is 84 kt. What is the approximate flight time?
65 - Which statement about density altitude is correct?
66 - The planned distance is 60 NM and groundspeed is 80 kt. What is the approximate flight time?
67 - Basic empty mass is 700 kg, occupants are 65 kg and 72 kg, usable fuel for departure is 40 kg and MTOM is 880 kg. Is the mass within limits?
68 - The VFR semicircular rules are based on the...
69 - Calculated take-off mass = 2300 lbs, calculated CG = 95.75 in, fuel burn = 170 lbs on station 87.00 in. Where is the CG situated after the landing?
70 - (For this question, please use annex PFP-062) According to ICAO, what symbol indicates a civil airport (not international airport) with paved runway?
question PFP-062.webp
71 - What mass equals 102 litres of Avgas 100LL?
72 - The balance arm is the horizontal distance between...
73 - A helicopter burns 48 l/h. Planned flight time is 25 minutes and required reserve is 20 l. What minimum fuel should be planned?
74 - The planned distance is 30 NM and groundspeed is 60 kt. What is the approximate flight time?
75 - What needs to be observed if the carburettor heat is applied in a hover?
76 - Why is wind component important for a PPL(H) flight?
77 - A helicopter burns 45 l/h. Planned flight time is 30 minutes and required reserve is 15 l. What minimum fuel should be planned?
78 - Which statement about a NOTAM affecting the destination is correct?
79 - Loads must be adequately secured in order to...
80 - Which statement about lateral centre of gravity is correct?
81 - A helicopter burns 32 l/h. Planned flight time is 45 minutes and required reserve is 15 l. What minimum fuel should be planned?
82 - Which statement about useful load is correct?
83 - Why is fuel reserve important for a PPL(H) flight?
84 - The planned distance is 72 NM and groundspeed is 96 kt. What is the approximate flight time?
85 - When preparing to carry out the weighing procedure on an aircraft, which of the following is required?
86 - During a flight with a flight plan submitted, landing is conducted at an aerodrome other than the destination stated in the filed flight plan. Who has to be contacted by the pilot immediately?
87 - How should gusty wind be considered during helicopter performance planning?
88 - Exceeding the maximum allowed aircraft mass is...
89 - What is the purpose of "interception lines" in visual navigation?
90 - The density of AVGAS 100LL at 15° C is...
91 - The specified speed in the ATS flight plan equals: Use figure (PFP-051)
question PFP-051.webp
92 - What should be considered regarding ice formation during flight?
93 - What is the maximum helicopter mass to conduct a departure at 8000 feet pressure altitude and an outside air temperature of +20° C? Max. gross mass: 2500 lbs. Min. gross mass: 1600 lbs. Use figure (PFP-045)
question PFP-045.webp
94 - Which action best supports safe management of surface condition?
95 - Basic empty mass is 640 kg, occupants are 90 kg and 78 kg, usable fuel for departure is 50 kg and MTOM is 890 kg. Is the mass within limits?
96 - Which statement about maximum take-off mass is correct?
97 - Using figure (PFP-006), calculate the empty mass and centre-of-gravity arm after all three equipment changes. Round the CG arm to three decimal places.
question pfp-006-corrected-20261005.webp
98 - Which point indicates the speed for maximum endurance? Use figure (PFP-044)
question PFP-044.webp
99 - A helicopter burns 38 l/h. Planned flight time is 55 minutes and required reserve is 20 l. What minimum fuel should be planned?
100 - The position of the centre of gravity (including fuel) equals... Use figure (PFP-053e)
question PFP-053e.webp
101 - The distance between the centre of gravity and the datum is called...
102 - During an unaccelerated flight...
103 - Which action best supports safe management of wind component?
104 - What are the variable physical properties of the atmosphere that affect the helicopter performance?
105 - The upper limit of LO R 16 equals... Use figure (PFP-056)
question PFP-056.webp
106 - The EOBT (estimated off-block time) is specified in the ATS flight plan as...
107 - Why is passenger mass accuracy important for a PPL(H) flight?
108 - A helicopter burns 35 l/h. Planned flight time is 90 minutes and required reserve is 30 l. What minimum fuel should be planned?
109 - The term "maximum elevation figure" (MEF) is defined as...
110 - A helicopter burns 42 l/h. Planned flight time is 60 minutes and required reserve is 20 l. What minimum fuel should be planned?
111 - A helicopter approach is conducted into the wind because...
112 - Which statement about hover in ground effect is correct?
113 - Which action best supports safe management of passenger mass accuracy?
114 - A helicopter burns 30 l/h. Planned flight time is 70 minutes and required reserve is 20 l. What minimum fuel should be planned?
115 - Basic empty mass is 760 kg, occupants are 70 kg and 70 kg, usable fuel for departure is 28 kg and MTOM is 930 kg. Is the mass within limits?
116 - Why is landing performance margin important for a PPL(H) flight?
117 - How should headwind be considered during helicopter performance planning?
118 - What is the lowest possible VFR flight level if a true course of 181° is selected and a variation of 3° east exists?
119 - What must be considered for cross-border flights?
120 - The calculated take-off mass is 725 kg and the total moment is 650 000 kg mm (equivalent to 650 kg m). Which numbered cross represents this loading? Use figure (PFP-004); its metric horizontal scale is moment divided by 1 000.
question PFP-004.webp