CAX performance section
(Refer to figure 2.) An airplane weighing 2,750 pounds - correct answer ✔✔be below stall speed
(Refer to figure 2.) You are flying an airplane that weighs 2,750 pounds - correct answer ✔✔The airplane
should stall under these conditions.
(Refer to figure 3.) If an airplane glides at an angle of attack of 10 degrees, how much altitude will it lose
in 6 miles? - correct answer ✔✔2,830 feet.
(Refer to figure 3.) If an airplane glides at an angle of attack of 10 degrees, how much altitude will it lose
in 1 miles? - correct answer ✔✔480 feet.
(Refer to figure 3.) How much altitude will this airplane lose in 3 statute miles of gliding at an angle of
attack of 8 degrees - correct answer ✔✔1,320 feet.
(Refer to figure 3.) The L/D ratio at a 2 degree angle of attack is approximately the same as - correct
answer ✔✔16.5 degrees angle of attack
(Refer to figure 4.) What is the stall speed of an airplane under a load factor of 2 G's - correct answer
✔✔91 knots
(Refer to figure 4.) What increase in load factor would take place if the angle of bank - correct answer
✔✔4 G's.
(Refer to figure 4.) You are descending at a constant rate of descent. - correct answer ✔✔40 percent.
The performance tables of an aircraft for takeoff and climb are based on - correct answer ✔✔pressure/
density altitude
,(Refer to figure 8.)
GIVEN:
Fuel quantity 47 gal - correct answer ✔✔3 hours 22 minutes.
(Refer to figure 8.)
GIVEN:
Fuel quantity 65 gal - correct answer ✔✔4 hours 30 minutes.
(Refer to figure 8.) Approximately how much fuel would be consumed when climbing at 75 percent
power for 7 minutes? - correct answer ✔✔2.15 gallons
(Refer to figure 8.) Approximately how much fuel would be consumed when climbing at 75 percent
power for 20 minutes? - correct answer ✔✔6 gallons.
(Refer to figure 8.) Determine the amount of fuel consumed during takeoff and climb at 70 percent
power for 10 minutes. - correct answer ✔✔2.88 gallons
(Refer to figure 8.) With 38 gallons of fuel aboard at cruise power (55 percent) - correct answer ✔✔2
hours 34 minutes.
(Refer to figure 8.) Using the line for Best Power Level Flight - correct answer ✔✔17 gallons per hour.
(Refer to figure 9.) Using a normal climb, how much fuel would be used from engine start to 12,000 feet
pressure altitude? - correct answer ✔✔58 pounds.
(Refer to figure 9.) Using a normal climb, how much fuel would be used from engine start to 10,000 feet
pressure altitude? - correct answer ✔✔35 pounds.
(Refer to figure 10.) Using a maximum rate of climb, how much fuel would be used from engine start to
6,000 feet pressure altitude? - correct answer ✔✔24 pounds.
, (Refer to figure 10.) Using a maximum rate of climb, how much fuel would be used from engine start to
10,000 feet pressure altitude? - correct answer ✔✔40 pounds.
(Refer to figure 11.) If the cruise altitude is 7,500 feet, using 64 percent power - correct answer ✔✔810
miles.
(Refer to figure 11.) What would be the endurance at an altitude of 7,500 feet, using 52 percent power?
NOTE: (With 48 - correct answer ✔✔7.7 hours.
(Refer to figure 11.) What would be the approximate true airspeed and fuel consumption per hour at an
altitude of 7,500 feet, using 52 percent power? - correct answer ✔✔105 MPH TAS, 6.2 GPH
(Refer to figure 11.) With 38 gallons - correct answer ✔✔600 miles.
(Refer to figure 11.) With 48 gallons - correct answer ✔✔760 miles.
(Refer to figure 12.)
GIVEN:
Pressure altitude: 18,000 ft
Temperature -21 degrees C - correct answer ✔✔4 hours 1 minute
(Refer to figure 12.)
GIVEN:
Pressure altitude: 18,000 ft
Temperature -41 degrees C - correct answer ✔✔2 hours 27 minutes
(Refer to figure 12.)
GIVEN:
Pressure altitude: 18,000 ft
Temperature -1 degrees C - correct answer ✔✔5 hours 59 minutes
(Refer to figure 2.) An airplane weighing 2,750 pounds - correct answer ✔✔be below stall speed
(Refer to figure 2.) You are flying an airplane that weighs 2,750 pounds - correct answer ✔✔The airplane
should stall under these conditions.
(Refer to figure 3.) If an airplane glides at an angle of attack of 10 degrees, how much altitude will it lose
in 6 miles? - correct answer ✔✔2,830 feet.
(Refer to figure 3.) If an airplane glides at an angle of attack of 10 degrees, how much altitude will it lose
in 1 miles? - correct answer ✔✔480 feet.
(Refer to figure 3.) How much altitude will this airplane lose in 3 statute miles of gliding at an angle of
attack of 8 degrees - correct answer ✔✔1,320 feet.
(Refer to figure 3.) The L/D ratio at a 2 degree angle of attack is approximately the same as - correct
answer ✔✔16.5 degrees angle of attack
(Refer to figure 4.) What is the stall speed of an airplane under a load factor of 2 G's - correct answer
✔✔91 knots
(Refer to figure 4.) What increase in load factor would take place if the angle of bank - correct answer
✔✔4 G's.
(Refer to figure 4.) You are descending at a constant rate of descent. - correct answer ✔✔40 percent.
The performance tables of an aircraft for takeoff and climb are based on - correct answer ✔✔pressure/
density altitude
,(Refer to figure 8.)
GIVEN:
Fuel quantity 47 gal - correct answer ✔✔3 hours 22 minutes.
(Refer to figure 8.)
GIVEN:
Fuel quantity 65 gal - correct answer ✔✔4 hours 30 minutes.
(Refer to figure 8.) Approximately how much fuel would be consumed when climbing at 75 percent
power for 7 minutes? - correct answer ✔✔2.15 gallons
(Refer to figure 8.) Approximately how much fuel would be consumed when climbing at 75 percent
power for 20 minutes? - correct answer ✔✔6 gallons.
(Refer to figure 8.) Determine the amount of fuel consumed during takeoff and climb at 70 percent
power for 10 minutes. - correct answer ✔✔2.88 gallons
(Refer to figure 8.) With 38 gallons of fuel aboard at cruise power (55 percent) - correct answer ✔✔2
hours 34 minutes.
(Refer to figure 8.) Using the line for Best Power Level Flight - correct answer ✔✔17 gallons per hour.
(Refer to figure 9.) Using a normal climb, how much fuel would be used from engine start to 12,000 feet
pressure altitude? - correct answer ✔✔58 pounds.
(Refer to figure 9.) Using a normal climb, how much fuel would be used from engine start to 10,000 feet
pressure altitude? - correct answer ✔✔35 pounds.
(Refer to figure 10.) Using a maximum rate of climb, how much fuel would be used from engine start to
6,000 feet pressure altitude? - correct answer ✔✔24 pounds.
, (Refer to figure 10.) Using a maximum rate of climb, how much fuel would be used from engine start to
10,000 feet pressure altitude? - correct answer ✔✔40 pounds.
(Refer to figure 11.) If the cruise altitude is 7,500 feet, using 64 percent power - correct answer ✔✔810
miles.
(Refer to figure 11.) What would be the endurance at an altitude of 7,500 feet, using 52 percent power?
NOTE: (With 48 - correct answer ✔✔7.7 hours.
(Refer to figure 11.) What would be the approximate true airspeed and fuel consumption per hour at an
altitude of 7,500 feet, using 52 percent power? - correct answer ✔✔105 MPH TAS, 6.2 GPH
(Refer to figure 11.) With 38 gallons - correct answer ✔✔600 miles.
(Refer to figure 11.) With 48 gallons - correct answer ✔✔760 miles.
(Refer to figure 12.)
GIVEN:
Pressure altitude: 18,000 ft
Temperature -21 degrees C - correct answer ✔✔4 hours 1 minute
(Refer to figure 12.)
GIVEN:
Pressure altitude: 18,000 ft
Temperature -41 degrees C - correct answer ✔✔2 hours 27 minutes
(Refer to figure 12.)
GIVEN:
Pressure altitude: 18,000 ft
Temperature -1 degrees C - correct answer ✔✔5 hours 59 minutes
