1 ATTENT. FLIG. PER. EXAM. PREP.

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)

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)

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

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)

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)

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)

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)

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)

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)

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

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)

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)

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.

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.

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.

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.

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.

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.

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.

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).

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

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.

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.

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.

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.

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.