Performance Charts Quiz CPL
(Refer to figure 13.) Using a maximum rate of climb under the given conditions, how much fuel would be used from engine start to a pressure altitude of 16,000 feet?
GIVEN:
Aircraft weight: 3,400 lb
Airport pressure altitude: 6,000 ft
Temperature at 6,000 feet
10 °C
Aircraft weight: 3,400 lb
Airport pressure altitude: 6,000 ft
Temperature at 6,000 feet
10 °C
43 pounds.
49 pounds.
45 pounds.
(Refer to figure 12) Given the following conditions, how much fuel is needed to fly 500 NM with a 25-knot tailwind?
GIVEN:
Pressure altitude: 18,000 ft
Temperature: -21° C
Power: 2,400 RPM / 28 inches MP
Pressure altitude: 18,000 ft
Temperature: -21° C
Power: 2,400 RPM / 28 inches MP
39 gallons
52 gallons
37 gallons
(Refer to figure 2) You're flying power off at 68 KTS with the gear and flaps retracted. What would happen if you initiate a turn and bank to 30° while maintaining 68 KTS?
The airplane will stall.
The airplane will continue flying normally.
The increased lift created by banking the airplane will cause the airplane to climb.
(Refer to figure 2) While flying power-off at a weight of 2,750 pounds with the gear and flaps down in a 30° bank turn, at which speed would you expect the airplane to stall?
70 KTS
62 KTS
62 MPH
(Refer to Figure 3A.) At an altitude of 3,000 feet AGL, how far would you expect to glide?
27,342 feet.
4.5 statute miles.
1,400 feet.
(Refer to Figure 3A.) How far would you expect to glide at an altitude of 7,000 feet height above terrain?
10.5 nautical miles.
9 nautical miles.
55,440 feet.
(Refer to figure 2.) Select the correct statement regarding stall speeds.
Power-off stalls occur at higher airspeeds with the gear and flaps down.
In a 60° bank the airplane stalls at a lower airspeed with the gear up.
Power-on stalls occur at lower airspeeds in shallower banks.
(Refer to figure 2.) Select the correct statement regarding stall speeds. The airplane will stall
10 knots higher in a power-on, 60° bank, with gear and flaps up, than with gear and flaps down.
25 knots lower in a power-off, flaps-up, 60° bank, than in a power-off, flaps-down, wings-level configuration.
10 knots higher in a 45° bank, power-on stall, than in a wings-level stall with flaps up.
(Refer to figure 33) An IFR departure procedure out of a high-altitude airport requires a minimum rate of climb of 750 FPM. What is the maximum temperature you can depart and maintain the IFR climb requirements given the following conditions?
GIVEN:
Weight: 4,000 lbs
Pressure altitude: 8,000 ft
0° C.
20° C.
-20° C.
Which maximum range factor decreases as weight decreases?
Altitude.
Airspeed.
Angle of attack.
An airplane is located at an airport with an elevation of 5,000 feet MSL and a temperature of 90 degrees F. The altimeter is set to airport elevation. Later that night the temperature plummets to 50 degrees F. Unless the altimeter setting is changed, it will read
4,800 feet
5,000 feet
5,200 feet
What effect does a downsloping runway have on takeoff performance?
Increased takeoff distance.
Runway slope does not affect takeoff distance.
Decreased takeoff distance.
(Refer to figure 15.) What is your distance from climb to cruise altitude with the following:
GIVEN:
| Airport pressure altitude | 4,000 feet |
| Airport temperature | 0 °C |
| Cruise pressure altitude | 8,000 feet |
| Cruise temperature | -10 °C |
11.5 NM.
17 NM.
6 NM.
Your airplane is equipped with an air conditioner that has a limitation stating it must be used on the ground only. If you forget to turn it off prior to takeoff, what can you expect?
The alternator will become overloaded.
Your takeoff roll distance will increase.
Your takeoff roll distance will decrease.
As fuel quantity decreases, and in turn the aircraft weight decreases, what is one adjustment you could make during a flight to achieve maximum range?
Descend to a lower altitude.
Increase fuel flow with the mixture to generate more power.
Reduce the throttle as the flight progresses to maintain a constant airspeed.
Approaching the destination airport, you are issued a land and hold short (LAHSO) clearance and determine the available landing distance to be 2,500 feet. Your preflight landing calculations show that you need 2,955 feet to land. Can you accept the LAHSO clearance?
Yes, as long as use a short field landing technique and know you can still stop in the available landing distance.
Yes, as long as you determine there will not be a conflict with the aircraft operating on the crossing runway.
No.
While flying at a pressure altitude of 5,000', your OAT gauge reads 22°C. You know that the density altitude is:
5,000'.
Lower than 5,000'.
Higher than 5,000'.
(Refer to figure 32) What is the total takeoff distance required to clear a 50-foot obstacle with the following conditions:
GIVEN:
| Temperature | 50 °F |
| Pressure altitude | 4,000 feet |
| Weight | 3,200 lb |
| Headwind | 15 kts. |
1,200 feet.
880 feet.
700 feet.
(Refer to figure 33) If your airplane weighs 3,700 lbs. and the pressure altitude is 8,000', how much would the maximum rate of climb decline if the temperature were to increase from 0 °C to 20 °C?
150 FPM.
140 FPM.
145 FPM.
(Refer to figure 8.) Using the line for Best Power Level Flight, what is the fuel flow at 71% power?
16.8 gallons per hour.
16 gallons per hour.
14.8 gallons per hour.
(Refer to figure 34.) What is the maximum available flight time under the conditions stated? (Allow for VFR night reserves.)
GIVEN:
| Pressure altitude | 6,000 ft |
| Temperature | -7° C |
| Power | 2,400 RPM - 24 inches MP |
| Usable fuel available | 342 lb |
3 hours and 49 minutes.
3 hours and 4 minutes.
3 hours.
(Refer to figure 12.) Using the conditions listed in the chart, what is the aircraft's endurance at cruise altitude with no reserve?
GIVEN:
Engine start, taxi, takeoff and climb: 115 pounds and 19 minutes
Descent, Landing and taxi: 50 pounds and 12 minutes
| RPM | 2,200 |
| Temperature | -1 °C |
| Manifold Pressure | 22 inches |
| Usable fuel available | 375 lb |
3 hours and 2 minutes.
3 hours and 11 minutes.
2 hours and 48 minutes.
The performance tables of an aircraft for takeoff and climb are based on
pressure/density altitude.
cabin altitude.
true altitude.
GIVEN:
Pressure altitude 12,000 ft
True air temperature +50 °F
From the conditions given, the approximate density altitude is11,900 feet.
14,130 feet.
18,150 feet
GIVEN:
Pressure altitude 5,000 ft
True air temperature +30 °C
From the conditions given, the approximate density altitude is7,800 feet.
8,100 feet.
8,800 feet.
GIVEN:
Pressure altitude 6,000 ft
True air temperature +30 °F
From the conditions given, the approximate density altitude is9,000 feet.
5,500 feet.
5,000 feet.
GIVEN:
Pressure altitude 7,000 ft
True air temperature +15 °C
From the conditions given, the approximate density altitude is
5,000 feet.
8,500 feet.
9,500 feet.
(Refer to figure 8.) GIVEN:
Fuel quantity 47 gal
Power-cruise (lean) 55 percent
Approximately how much flight time would be available with a night VFR fuel reserve remaining?
3 hours 8 minutes
3 hours 22 minutes
3 hours 43 minutes
(Refer to figure 9.) Using a normal climb, how much fuel would be used from engine start to 10,000 feet pressure altitude?
Aircraft weight 3,500lb
Airport pressure altitude 4,000 ft
Airport pressure altitude 4,000 ft
Temperature 21 °C
23 pounds.
31 pounds.
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?
Aircraft weight 3,200lb
Airport pressure altitude 2,000 ft Temperature 27 °C
10 pounds.
14 pounds.
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?
Aircraft weight 3,800lb
Airport pressure altitude 4,000 ft Temperature 30 °C
Airport pressure altitude 4,000 ft Temperature 30 °C
28 pounds.
35 pounds.
40 pounds.
(Refer to figure 11.) If the cruise altitude is 7,500 feet, using 64 percent power at 2,500 RPM, what would be the range with 48 gallons of usable fuel?
635 miles.
645 miles.
810 miles.
(Refer to figure 11.) What should be the endurance at an altitude of 7,500 feet, using 52 percent power? NOTE: (With 48 Gallons fuel-no reserve)
6.1 Hours
7.7 Hours
8.0 Hours
(Refer to figure 8.) GIVEN:
Fuel quantity 65 gal
Best power (level flight) 55 percent
Approximately how much flight time would be available with a day VFR fuel reserve remaining?
4 hours 17 minutes.
4 hours 30 minutes.
5 hours 4 minutes.
(Refer to figure 8.) Approximately how much fuel would be consumed when climbing at 75 percent power for 7 minutes?
1.82 gallons.
1.97 gallons.
2.15 gallons.
(Refer to figure 8.) Determine the amount of fuel consumed during takeoff and climb at 70 percent power for 10 minutes.
2.66 gallons.
2.88 gallons.
3.2 gallons.
(Refer to figure 8.) With 38 gallons of fuel aboard at cruise power (55 percent), how much flight time is available with night VFR fuel reserve still remaining?
2 hours 34 minutes.
2 hours 49 minutes.
3 hours 18 minutes.
(Refer to figure 9.) Using a normal climb, how much fuel would be used from engine start to 12,000 feet pressure altitude?
Aircraft weight 3,800 lb
Airport pressure altitude 4,000 ft
Airport pressure altitude 4,000 ft
Temperature 26 °C
46 pounds.
51 pounds.
58 pounds.
(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?
103 MPH TAS, 7.7 GPH.
105 MPH TAS, 6.1 GPH.
105 MPH TAS, 6.2 GPH.
(Refer to figure 12.) GIVEN:
Pressure altitude 18,000 ft
Temperature -21 °C
Power 2,400 RPM - 28” MP
Recommended lean mixture
Usable fuel 425 lb
3 hours 46 minutes.
4 hours 1 minute.
4 hours 31 minutes.
(Refer to figure 12.) GIVEN:
Pressure altitude 18,000 ft
Temperature -41 °C
Power 2,500 RPM - 26” MP
Power 2,500 RPM - 26” MP
Recommended lean mixture
Usable fuel 318 lb
What is the approximate flight time available under the given conditions? (Allow for VFR night fuel reserve.)
2 hours 27 minutes.
3 hours 12 minutes.
3 hours 42 minutes.
(Refer to figure 12.) GIVEN:
Pressure altitude 18,000 ft
Temperature - 1 °C
Power 2,200 RPM - 20” MP
Best fuel economy
Usable fuel 344 lb
Usable fuel 344 lb
What is the approximate flight time available under the given conditions? (Allow for VFR day fuel reserve.)
4 hours 50 minutes.
5 hours 20 minutes.
5 hours 59 minutes.
(Refer to figure 13.) GIVEN:
Aircraft weight 3,400 lb
Airport pressure altitude 6,000 ft
Airport pressure altitude 6,000 ft
Temperature at 6,000 feet 10 °C
Using a maximum rate of climb under the given conditions, how much fuel would be used from engine start to a pressure altitude of 16,000 feet?
43 pounds.
45 pounds.
49 pounds.
(Refer to figure 13.) GIVEN
Aircraft weight 4,000 lb
Airport pressure altitude 2,000 ft
Airport pressure altitude 2,000 ft
Temperature. at 2,000 feet 32 °C
Using a maximum rate of climb under the given conditions, how much time would be required to climb to a pressure altitude of 8,000 feet?
7 Minutes
8.4 Minutes
11.2 Minutes
(Refer to figure 13.) GIVEN
Aircraft weight 3,700 lb
Airport pressure altitude 4,000 ft
Airport pressure altitude 4,000 ft
Temperature at 4,000 feet 21 ºC
Using a normal climb under the given conditions, how much fuel would be used from engine start to a pressure altitude of 12,000 feet?
30 pounds.
37 pounds.
46 pounds.
(Refer to figure 14.) GIVEN:
Weight 3,400 lb
Airport pressure altitude 4,000 ft
Airport pressure altitude 4,000 ft
Temperature at 4,000 feet 14 ºC
Using a normal climb under the given conditions, how much time would be required to climb to a pressure altitude of 8,000 feet?
4.8 minutes.
5 minutes.
5.5 minutes.
(Refer to figure 15.) GIVEN
Airport pressure altitude 4,000 ft
Airport temperature 12 °C
Cruise pressure altitude 9,000 ft
Cruise temperature -4 °C
What will be the distance required to climb to cruise altitude under the given conditions?
6 miles.
8.5 miles.
11 miles.
(Refer to figure 31.) What is the headwind component for a Rwy 13 takeoff if the surface wind is 190° at 15 knots?
7 knots.
13 knots.
15 knots.
(Refer to figure 32.) GIVEN:
Temperature 75 °F
Pressure altitude 6,000 ft
Weight 2,900 lb
Headwind 20 kts
To safely take off over a 50-foot obstacle in 1,000 feet, what weight reduction is necessary?
50 pounds.
100 pounds.
300 pounds.
(Refer to figure 32.) GIVEN:
Temperature 50 °F
Pressure altitude 2,000 feet
Weight 2,700 lb
Wind Calm
What is the total takeoff distance over a 50-foot obstacle?
650 feet.
1050 feet.
800 feet.
(Refer to figure 32.) GIVEN:
Temperature 100 °F
Pressure altitude 4,000 ft
Weight 3,200 lb
Wind Calm
What is the ground roll required for takeoff over a 50-foot obstacle?
1,180 feet.
1,350 feet.
1,850 feet.
(Refer to figure 32.) GIVEN
Temperature 30 °F
Pressure altitude 6,000 ft
Weight 3,300 lb
Headwind 20 kts
What is the total takeoff distance over a 50-foot obstacle?
1,100 feet.
1,300 feet.
1,500 feet.
(Refer to figure 15.) GIVEN
Airport pressure altitude 2,000 ft
Airport temperature 20 °C
Cruise pressure altitude 10,000 ft
Cruise pressure altitude 10,000 ft
Cruise temperature 0 °C
What will be the fuel, time, and distance required to climb to cruise altitude under the given conditions?
5 gallons, 9 minutes, 13 NM.
6 gallons, 11 minutes, 16 NM.
7 gallons, 12 minutes, 18 NM.
What effect does an uphill runway slope have on takeoff performance?
Increases takeoff speed.
Increases takeoff distance.
Decreases takeoff distance.
(Refer to figure 31.) Rwy 30 is being used for landing. Which surface wind would exceed the airplane's crosswind capability of 0.2 VSO, if VSO is 60 knots?
260° at 20 knots.
275° at 25 knots.
315° at 35 knots.
(Refer to figure 31.) If the tower-reported surface wind is 010° at 18 knots, what is the crosswind component for a Rwy 08 landing?
7 knots.
15 knots.
17 knots.
(Refer to figure 31.) The surface wind is 180° at 25 knots. What is the crosswind component for a Rwy 13 landing?
19 knots.
21 knots.
23 knots.
(Refer to figure 33.) GIVEN:
Weight 4,000 lb
Pressure altitude 5,000 ft
Temperature 30 °C
What is the maximum rate of climb under the given conditions?
655 ft/min.
702 ft/min.
774 ft/min.
(Refer to figure 33.) GIVEN:
Weight 3,700 lb
Pressure altitude 22,000 ft
Temperature -10 °C
What is the maximum rate of climb under the given conditions?
305 ft/min.
320 ft/min.
384 ft/min.
(Refer to figure 34.) GIVEN:
Pressure altitude 6,000 ft
Temperature +3 °C
Power 2,200 RPM - 22 inches MP
Usable fuel available 465 lb
What is the maximum available flight time under the conditions stated?
6 hours 27 minutes.
6 hours 39 minutes.
6 hours 56 minutes.
(Refer to figure 34.) GIVEN:
Pressure altitude 6,000 ft
Temperature -17 °C
Power 2,300 RPM - 23 inches MP
Usable fuel available 370 lb
What is the maximum available flight time under the conditions stated?
4 hours 20 minutes.
4 hours 30 minutes.
4 hours 50 minutes.
(Refer to figure 34.) GIVEN:
Pressure altitude 6,000 ft
Temperature .+13 °C
Power 2,500 RPM - 23 inches MP
Usable fuel available 460 lb
What is the maximum available flight time under the conditions stated?
4 hours 58 minutes.
5 hours 7 minutes.
5 hours 12 minutes.
(Refer to figure 35.) GIVEN:
Temperature 70 °F
Pressure altitude Sea level
Weight. 3,400 lb
Headwind 16 kts
Determine the approximate ground roll.
689 feet.
716 feet.
1,275 feet.
(Refer to figure 35.) GIVEN:
Temperature 85 °F
Pressure altitude 6,000 ft
Weight 2,800 lb
Headwind 14 kts
Determine the approximate ground roll.
742 feet.
1,280 feet.
1,480 feet.
(Refer to figure 35.) GIVEN:
Temperature 50 °F
Pressure altitude Sea level
Weight 3,000 lb
Headwind 10 kts
Determine the approximate ground roll.
425 feet.
636 feet.
836 feet.
(Refer to figure 35.) GIVEN:
Temperature 80 °F
Pressure altitude 4,000 ft
Weight 2,800 lb
Headwind 24 kts
What is the total landing distance over a 50-foot obstacle?
1,125 feet.
1,250 feet.
1,325 feet.
To determine pressure altitude prior to takeoff, the altimeter should be set to
the current altimeter setting.
29.92 inches Hg and the altimeter indication noted.
the field elevation and the pressure reading in the altimeter setting window noted.
(Refer to Figure 32.) Determine the approximate runway length necessary for takeoff.
GIVEN:
Temperature 40°F
Pressure altitude 4,000 ft
Weight 3,200 lbs
Headwind 15 kts
1,300 feet.
850 feet.
950 feet.
{"name":"Performance Charts Quiz CPL", "url":"https://www.quiz-maker.com/Q171C4IBI","txt":"(Refer to figure 13.) Using a maximum rate of climb under the given conditions, how much fuel would be used from engine start to a pressure altitude of 16,000 feet? GIVEN:Aircraft weight: 3,400 lbAirport pressure altitude: 6,000 ftTemperature at 6,000 feet10 °C, (Refer to figure 12) Given the following conditions, how much fuel is needed to fly 500 NM with a 25-knot tailwind? GIVEN:Pressure altitude: 18,000 ftTemperature: -21° CPower: 2,400 RPM \/ 28 inches MP, (Refer to figure 2) You're flying power off at 68 KTS with the gear and flaps retracted. What would happen if you initiate a turn and bank to 30° while maintaining 68 KTS?","img":"https://www.quiz-maker.com/3012/CDN/105-5137080/figure-13.png?sz=1200"}
