1 ATTENT. FLIG. PER. EXAM. PREP.

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Question 1 of 30

11 In order for a propeller driven aircraft to achieve maximum range it should be flown at a speed:

Select one of the following:

O which gives the max L/D ratio.
O equal to V2.
O slightly higher than stalling speed.
O equal to V1.

Explanation

Question 2 of 30

20 How will the density altitude change by an increase in temperature from -4C to +10C if the pressure altitude remains the same.(Fig. FPP01)

Select one of the following:

O It will increase by 1.650 ft.]
O it will increase by 1.400 ft.]
O It will increase by 1.200 ft.]
O It will decrease by 1.000 ft.]

Explanation

Question 3 of 30

21 What will the density altitude be if the airport elevation is 5.250 ft ,temperature 27C and altimeter setting 29.25 inHg? (Fig FPP01)

Select one of the following:

O '8.500 ft.
O '5.850 ft.
O '4.900 ft.
O '7.700 ft.

Explanation

Question 4 of 30

25 How does high density altitude affect propeller efficiency?

Select one of the following:

O It decreases propeller efficiency.
O It improves propeller efficiency.
O It does not affect propeller efficiency.

Explanation

Question 5 of 30

26 What is the crosswind component for a landing on runway 18,if the wind is 220 degrees 30 knots?(Fig FPP02)

Select one of the following:

O '19 kts
O '16 kts
O '22 kts.
O '24 kts

Explanation

Question 6 of 30

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)

Select one of the following:

O '35 kts
O '27 kts
O '30 kts
O '40 kts

Explanation

Question 7 of 30

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)

Select one of the following:

O '24 kts.
O '17 kts.
O '21 Kts.
O '28 kts.

Explanation

Question 8 of 30

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)

Select one of the following:

O Runway 14.
O Runway 32.
O Runway 24.
O Runway 06.].

Explanation

Question 9 of 30

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)

Select one of the following:

O '73.2 USG.
O '63,5 USG
O '70.1 USG.
O '78.2 USG.

Explanation

Question 10 of 30

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)

Select one of the following:

O '70.1 USG.
O '73.2 USG.
O '60,2 USG.
O '78,2 USG.

Explanation

Question 11 of 30

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)

Select one of the following:

O '36.1 USG.
O '31.4 USG.
O '40,1 USG.
O '43,2 USG.

Explanation

Question 12 of 30

33 What is the fuel flow of an aircraft which flies at 11.000 ft,in standard atmosphere,with 65% power? (Fig FPP03)

Select one of the following:

O '11,2 USG/hr.
O '11,8 USG/hr
O '12,1 USG/hr.
O '10,9 USG/hr

Explanation

Question 13 of 30

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)

Select one of the following:

O '21,0 inHg.
O '19,8 inHg.
O '20,8 inHg.
O '20,4 inHg.

Explanation

Question 14 of 30

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)

Select one of the following:

O '159 kts.
O '157 kts
O '154 kts.
O '162 kts.

Explanation

Question 15 of 30

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.

Select one of the following:

O '900 ft.
O '1.250 ft.
O '1.450 ft.
O '700 ft..

Explanation

Question 16 of 30

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.

Select one of the following:

O '1.100 ft.
O '1.350 ft.
O '1.500 ft.
O '900 ft.

Explanation

Question 17 of 30

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.

Select one of the following:

O '2.850 ft.
O '2.500 ft.
O '1.900 ft.
O '3.200 ft.

Explanation

Question 18 of 30

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.

Select one of the following:

O '401 ft.
O '356 ft..
O '490 ft.
O '534 ft.

Explanation

Question 19 of 30

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.

Select one of the following:

O '468 ft.
O '520 ft.
O '655 ft.
O '820 ft.

Explanation

Question 20 of 30

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.

Select one of the following:

O '338 ft.
O '310 ft.
O '424 ft.
O '470 ft.

Explanation

Question 21 of 30

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.

Select one of the following:

O '956 ft.
O '830 ft.
O '1.076 ft.
O '1.554 ft.

Explanation

Question 22 of 30

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).

Select one of the following:

O '1.315 ft.
O '1.075 ft.
O '545 ft.
O '1.195 ft.

Explanation

Question 23 of 30

44 What is the landing distance (ground roll) under the following conditions (Fig FPP05):Pressure altitude 1.250 ft ,headwind 8 kts ,temperature standard.

Select one of the following:

O '366 ft.
O '275 ft.
O '470 ft.
O '549 ft.

Explanation

Question 24 of 30

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.

Select one of the following:

O '628 ft.
O '852 ft.
O '567 ft.
O '1.136 ft.

Explanation

Question 25 of 30

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.

Select one of the following:

O '1.520 ft.
O '1.150 ft.
O '1.020 ft.
O '1.850 ft.

Explanation

Question 26 of 30

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.

Select one of the following:

O '1.100 ft.
O '900 ft.
O '1.350 ft.
O '1.600 ft.

Explanation

Question 27 of 30

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.

Select one of the following:

O '1.130 ft.
O '1.500 ft.
O '880 ft.
O '700 ft.

Explanation

Question 28 of 30

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.

Select one of the following:

O '910 ft.
O '1220 ft.
O '1.470 ft.
O '670 ft.

Explanation

Question 29 of 30

50 Which of the following are included in the term "basic empty weight"?

Select one of the following:

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.

Explanation

Question 30 of 30

51 If an aircraft is overloaded by 110 lbs (55 kgs),how much fuel does the pilot have to remove so that the aircraft loading will be within limits?]

Select one of the following:

O '18,3 USG.
O '16,2 USG.
O '15,7 USG.
O '17,1 USG.

Explanation

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