Jeppesen Private Pilot Stage III Exam with 100% Correct
Answers (2024/2025)
What combination of conditions is most detrimental to takeoff and climb performance? - -
High temperature, high humidity, and high altitude
Q2 - -8900ft
Q3 - -1732ft
Q4 - -1470ft
Q5 - -765fpm
What is the difference between the range and the endurance of an aircraft? - -With a given
amount of fuel, range is the distance that the aircraft can fly, and endurance is the amount of time
that the aircraft can remain in the air.
Center of gravity is defined as the theoretical point... - -where all of the aircraft's weight is
considered to be concentrated
One of the items included in the airplanes basic empty weight is... - -unusable fuel
What is the CG location after the airplane is loaded with full fuel? ****** - -42.66 inches
(SUM Weight x Arm)/(SUM Weight)
, How much fuel can be carried in the aircraft without exceeding a maximum takeoff weight of 2700
lbs? - -19.6 gallons (1 gallon = 6lbs)
Total moment - -113876.4 pound-inches
Assume an aircraft has a total weight of 2,950 pounds and a total moment of 210,700 pound-
inches. If the CG range is from 82.1 to 86.7 inches, what action, if any, should you take before you
fly the aircraft? - -Move some load aft in the aircraft
Q13 - -96.8 lb-inches
Q14 - -Within normal category limits but outside utility category limits
The time-speed-distance function of your flight computer can be used to solve for - -
groundspeed and fuel consumption
If your aircraft's fuel consumption rate is 5.6 g.p.h., how much fuel will it use on a flight of 230 n.m.
with an average groundspeed of 93 knots? - -13.8 gallons (Use E6-B)
Determine the density altitude using the listed conditions - -4097ft
Answers (2024/2025)
What combination of conditions is most detrimental to takeoff and climb performance? - -
High temperature, high humidity, and high altitude
Q2 - -8900ft
Q3 - -1732ft
Q4 - -1470ft
Q5 - -765fpm
What is the difference between the range and the endurance of an aircraft? - -With a given
amount of fuel, range is the distance that the aircraft can fly, and endurance is the amount of time
that the aircraft can remain in the air.
Center of gravity is defined as the theoretical point... - -where all of the aircraft's weight is
considered to be concentrated
One of the items included in the airplanes basic empty weight is... - -unusable fuel
What is the CG location after the airplane is loaded with full fuel? ****** - -42.66 inches
(SUM Weight x Arm)/(SUM Weight)
, How much fuel can be carried in the aircraft without exceeding a maximum takeoff weight of 2700
lbs? - -19.6 gallons (1 gallon = 6lbs)
Total moment - -113876.4 pound-inches
Assume an aircraft has a total weight of 2,950 pounds and a total moment of 210,700 pound-
inches. If the CG range is from 82.1 to 86.7 inches, what action, if any, should you take before you
fly the aircraft? - -Move some load aft in the aircraft
Q13 - -96.8 lb-inches
Q14 - -Within normal category limits but outside utility category limits
The time-speed-distance function of your flight computer can be used to solve for - -
groundspeed and fuel consumption
If your aircraft's fuel consumption rate is 5.6 g.p.h., how much fuel will it use on a flight of 230 n.m.
with an average groundspeed of 93 knots? - -13.8 gallons (Use E6-B)
Determine the density altitude using the listed conditions - -4097ft
