5861260
Question 1
Question
26 What is the crosswind component for a landing on runway 18,if the wind is 220 degrees 30 knots?(Fig FPP02)
Answer
-
O '19 kts
-
O '16 kts
-
O '22 kts.
-
O '24 kts
Question 2
Question
27 If the wind direction is forming a 45 degree angle with the runway, what is the maximum wind speed during landing so as not to exceed a maximum demonstrated crosswind component of 25 kts? (Fig FPP02)
Answer
-
O '35 kts
-
O '27 kts
-
O '30 kts
-
O '40 kts
Question 3
Question
28 If the wind direction is forming a 30 degree angle with the runway,what is the maximum wind speed during landing so as not to exceed a max demonstrated crosswind component of 12 kts?(Fig FPP02)
Answer
-
O '24 kts.
-
O '17 kts..
-
O '21 Kts.
-
O '28 kts..
Question 4
Question
29 If the wind is from 180 degrees 20 kts which runway should be used by an aircraft with a max demonstrated crosswind component of 13 kts? (Fig FPP02)
Answer
-
O Runway 14.
-
O Runway 32.
-
O Runway 24.
-
O Runway 06.
Question 5
Question
30 How much fuel is required for a flight of 1.000 NM under the following conditions: Pressure altitude 8.000 ft,outside air temperature -19 C,manifold pressure 19.5 inHg, wind calm. (Fuel reserves are not included) (Fig FPP03)
Answer
-
O '73.2 USG.
-
O '63,5 USG
-
O '70.1 USG.
-
O '78.2 USG.
Question 6
Question
31 How much fuel required for a flight of 1.000 NM under the following conditions: Pressure altitude 8.000ft.outside air temperature +22 C,manifold pressure 20.8 inHg,wind calm.(Fuel reserves are not included) (Fig FPP03)
Answer
-
O '70.1 USG.
-
O '73.2 USG.
-
O '60,2 USG.
-
O '78,2 USG.
Question 7
Question
32 What is the estimated fuel consumption for a 500 NM flight under the following conditions: Pressure altitude 4.000 ft,outside air temperature +29 C,manifold pressure 21.3 inHg,wind calm. (Fig FPP03)
Answer
-
O '36.1 USG.
-
O '31.4 USG.
-
O '40,1 USG.
-
O '43,2 USG.
Question 8
Question
33 What is the fuel flow of an aircraft which flies at 11.000 ft,in standard atmosphere,with 65% power? (Fig FPP03)
Answer
-
O '11,2 USG/hr.
-
O '11,8 USG/hr
-
O '12,1 USG/hr.
-
O '10,9 USG/hr
Question 9
Question
34 What manifold pressure will you use at 6.500 ft ,2.450 RPM ,with 65% power and a temperature of 20C above standard? (Fig FPP03)
Answer
-
O '21,0 inHg.
-
O '19,8 inHg.
-
O '20,8 inHg.
-
O '20,4 inHg.
Question 10
Question
35 What will the true air speed be if you are flying at 9.500 ft,with 65% power and a temperature of 20 C (36 F) below standard? (Fig FPP03)
Answer
-
O '159 kts.
-
O '157 kts
-
O '154 kts.
-
O '162 kts.
Question 11
Question
36 Calculate the landing distance (ground roll) of the aircraft under the following conditions (Fig FPP04): Temperature standard ,Pressure altitude 2.000 ft ,weight 2.300 lbs,wind calm.
Answer
-
O '900 ft.
-
O '1.250 ft.
-
O '1.450 ft.
-
O '700 ft..
Question 12
Question
37 Calculate the landing distance (ground roll) of the aircraft under the following conditions (Fig FPP04):Temperature 32 C (90 F) ,pressure altitude 4.000 ft ,weight 2.800 lbs ,headwind 10 kts.
Answer
-
O '1.100 ft.
-
O '1.350 ft.
-
O '1.500 ft.
-
O '900 ft.
Question 13
Question
38 Calculate the total landing distance over 50 ft obstacle under the following conditions (Fig FPP04):Temperature 32 C (90 F), pressure altitude 3.000 ft ,Weight 2.900 lbs ,tailwind 10 kts.
Answer
-
O '2.850 ft.
-
O '2.500 ft.
-
O '1.900 ft.
-
O '3.200 ft.
Question 14
Question
39 Calculate the landing distance (ground roll) of the aircraft under the following conditions (Fig 5):Pressure altitude sea level ,headwind 4 kts ,temperature standard.
Answer
-
O '401 ft.
-
O '356 ft.
-
O '490 ft.
-
O '534 ft.
Question 15
Question
40 Calculate the landing distance (ground roll) of the aircraft under the following conditions (Fig FPP04):Pressure altitude 7.500 ft ,headwind 4 kts ,temperature standard.
Answer
-
O '468 ft.
-
O '520 ft.
-
O '655 ft.
-
O '820 ft.
Question 16
Question
41 What is the landing distance (ground roll) of the aircraft under the following conditions (Fig FPP05):Pressure altitude 3.750 ft ,headwind 12 kts ,temperature standard.
Answer
-
O '338 ft.
-
O '310 ft.
-
O '424 ft.
-
O '470 ft.
Question 17
Question
42 What is the landing distance over 50ft obstacle under the following conditions (Fig FPP05):Pressure altitude 5.000 ft ,headwind 8 kts ,temperature 5 C (41 F),asphalt runway.
Answer
-
O '956 ft.
-
O '830 ft.
-
O '1.076 ft.
-
O '1.554 ft.
Question 18
Question
43 What is the landing distance over 50 ft obstacle under the following conditions (Fig FPP05):Pressure altitude 5.000 ft ,wind calm ,temperature 41 C (101 F).
Answer
-
O '1.315 ft.
-
O '1.075 ft.
-
O '545 ft.
-
O '1.195 ft.
Question 19
Question
44 What is the landing distance (ground roll) under the following conditions (Fig FPP05):Pressure altitude 1.250 ft ,headwind 8 kts ,temperature standard.
Answer
-
O '366 ft.
-
O '275 ft..
-
O '470 ft.
-
O '549 ft.
Question 20
Question
45 What is the landing distance of the aircraft under the following conditions (Fig FPP05): Pressure altitude 7.500 ft, temperature 0 C (32 F), headwind component 20 kts ,obstacle 50 ft.
Answer
-
O '628 ft.
-
O '852 ft.
-
O '567 ft.
-
O '1.136 ft.
Question 21
Question
46 Calculate the total take off distance over 50 ft obstacle under the following conditions (Fig FPP06):Pressure altitude 4.000 ft temperature standard ,weight 2.600 lbs ,wind calm.
Answer
-
O '1.520 ft.
-
O '1.150 ft.
-
O '1.020 ft.
-
O '1.850 ft.
Question 22
Question
47 What is the take off distance under the following conditions (Fig FPP06):Pressure altitude 2.000 ft ,temperature 38 C ,take off weight 2.750 lbs .wind calm ,obstacle 0 ft.
Answer
-
O '1.100 ft.
-
O '900 ft.
-
O '1.350 ft.
-
O '1.600 ft.
Question 23
Question
48 Calculate the total take off distance over 50 ft obstacle under the following conditions (Fig FPP06):Temperature standard ,pressure altitude sea level ,weight 2.500 lbs ,wind calm.
Answer
-
O '1.130 ft.
-
O '1.500 ft.
-
O '880 ft.
-
O '700 ft.
Question 24
Question
49 What is the take off distance of the aircraft under the following conditions (Fig FPP06):temperature 32 C ,pressure altitude 2.000 ft ,take off weight 2.900 lbs headwind component 20 kts ,obstacle 0 ft.
Answer
-
O '910 ft.
-
O '1220 ft.
-
O '1.470 ft.
-
O '670 ft.
Question 25
Question
50 Which of the following are included in the term "basic empty weight"?
Answer
-
O unusable fuel and optional equipment.
-
O Hydraulic fluids and usable fuel.
-
O Only the airframe, the engine and the equipment, which have been installed by the manufacturer.
-
O full fuel and oil tanks.
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