2 FLIG. PER. EXAM PREP

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.