ATPL - FLIGHT PERFORMANCE &
PLANNING 3/3 Exam Questions and
Answers with Verified Solutions | Latest
Updated 2026
15. (Refer to Figure 11) What c. 105 MPH TAS, 6.2 GPH
would be the approximate true
airspeed and fuel consumption
per hour at an altitude of
7,500 feet, using 52 percent
power? a. 103 MPH TAS, 6.3
GPH b. 105 MPH TAS, 6.6 GPH
c. 105 MPH TAS, 6.2 GPH
20. (Refer to Figure 8) With 38 a. 2 hours 34 minutes
gallons of fuel aboard at cruise
power (55 percent), how much
flight time is available with
night VFR fuel reserve still
remaining? a. 2 hours 34
minutes b. 2 hours 49 minutes
c. 3 hours 18 minutes
25. When computing weight a. The unusable fuel, fuel operating
and balance, the basic empty fluids, and full oil
weight includes the weight of
the airframe, engine(s), and all
installed optional equipment.
Basic empty weight also
includes: a. The unusable fuel,
fuel operating fluids, and full
, oil b. All usable fuel, full oil,
hydraulic fluid, but does not
include the weight of the pilot,
passengers, or baggage c. All
usable fuel and oil, but does
not include any radio
equipment or instruments that
were installed by someone
other than the manufacturer.
23. (Refer to Figure 35) Given: a. 689 feet
Temperature................................................
70°F Pressure
altitude...........................................
Sea level
Weight.........................................................
3,400 lb
Headwind......................................................
16 kts Determine the
approximate ground roll. a.
689 feet b. 716 feet c. 1,275
feet
3. If all index units are positive b. Nose, or out in front of the
when computing weight and airplane
balance, the location of the
datum would be at the: a.
Centreline of the main wheels
b. Nose, or out in front of the
airplane c. Centreline of the
nose or tailwheel, depending
on the type of airplane
PLANNING 3/3 Exam Questions and
Answers with Verified Solutions | Latest
Updated 2026
15. (Refer to Figure 11) What c. 105 MPH TAS, 6.2 GPH
would be the approximate true
airspeed and fuel consumption
per hour at an altitude of
7,500 feet, using 52 percent
power? a. 103 MPH TAS, 6.3
GPH b. 105 MPH TAS, 6.6 GPH
c. 105 MPH TAS, 6.2 GPH
20. (Refer to Figure 8) With 38 a. 2 hours 34 minutes
gallons of fuel aboard at cruise
power (55 percent), how much
flight time is available with
night VFR fuel reserve still
remaining? a. 2 hours 34
minutes b. 2 hours 49 minutes
c. 3 hours 18 minutes
25. When computing weight a. The unusable fuel, fuel operating
and balance, the basic empty fluids, and full oil
weight includes the weight of
the airframe, engine(s), and all
installed optional equipment.
Basic empty weight also
includes: a. The unusable fuel,
fuel operating fluids, and full
, oil b. All usable fuel, full oil,
hydraulic fluid, but does not
include the weight of the pilot,
passengers, or baggage c. All
usable fuel and oil, but does
not include any radio
equipment or instruments that
were installed by someone
other than the manufacturer.
23. (Refer to Figure 35) Given: a. 689 feet
Temperature................................................
70°F Pressure
altitude...........................................
Sea level
Weight.........................................................
3,400 lb
Headwind......................................................
16 kts Determine the
approximate ground roll. a.
689 feet b. 716 feet c. 1,275
feet
3. If all index units are positive b. Nose, or out in front of the
when computing weight and airplane
balance, the location of the
datum would be at the: a.
Centreline of the main wheels
b. Nose, or out in front of the
airplane c. Centreline of the
nose or tailwheel, depending
on the type of airplane
