Private Pilot Stage 3 Exam/ Private Pilot Stage III Exam –
Jeppeson With complete solu on RATED A+ NEW
EDITION
What combina on of condi ons is most detrimental to takeoff and climb performance? - Ans
High temperature, high humidity, and high al tude
According to the accompanying chart, pressure al tude of 5,000 feet with a temperature of
+40C will result in a density al tude of approximately - Ans 8,900 feet
According to the accompanying takeoff distance chart and the following condi ons, what is the
total distance necessary to clear a 50-foot obstacle? - Ans 1,732 feet
Using the listed condi ons and the accompanying landing distance chart, determine the
distance required to land over a 50-foot barrier - Ans 1,470 feet
Use the accompanying maximum rate-of-climb chart and the listed condi ons to determine the
rate of climb - Ans 765 f.p.m.
What is the difference between the range and the endurance of an aircra0? - Ans With a given
amount of fuel, range is the distance that the aircra0 can fly, and endurance is the amount of
me that the aircra0 can remain in the air.
Center of gravity is defined as the theore cal point - Ans where all of the aircra0's weight is
considered to be concentrated
One of the items included in an aircra0's basic empty weight is - Ans unusable fuel
, What is the CG loca on a0er the airplane is loaded with full fuel? - Ans 42.66 inches
How much fuel can be carried in the aircra0 without exceeding a maximum takeoff weight of
2,700 pounds? - Ans 19.6 gallons
Using the loading specifica ons from the previous problem, the total moment is - Ans
113,8976.4 pound-inches
Assume an aircra0 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 ac on, if any, should you take before
you fly the aircra0? - Ans Move some load a0 in the aircra0
Based on the following condi ons, what is the total moment/1000 pound-inches? - Ans 96.8
According to the center of gravity moment envelope, the aircra0's CG is - Ans within normal
category limits but outside u lity category limits
The me-speed-distance func on of your flight computer can be used to solve for - Ans
groundspeed and fuel consump on
If your aircra0's fuel consump on 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? - Ans 13.8 gallons
Determine the density al tude using the listed condi ons - Ans 4097 feet
When you are flying an aircra0 into a le0-quartering headwind, what is the effect on
groundspeed and wind correc on angle if the wind velocity increases? - Ans Groundspeed
decreases, and wind correc on increases.
Jeppeson With complete solu on RATED A+ NEW
EDITION
What combina on of condi ons is most detrimental to takeoff and climb performance? - Ans
High temperature, high humidity, and high al tude
According to the accompanying chart, pressure al tude of 5,000 feet with a temperature of
+40C will result in a density al tude of approximately - Ans 8,900 feet
According to the accompanying takeoff distance chart and the following condi ons, what is the
total distance necessary to clear a 50-foot obstacle? - Ans 1,732 feet
Using the listed condi ons and the accompanying landing distance chart, determine the
distance required to land over a 50-foot barrier - Ans 1,470 feet
Use the accompanying maximum rate-of-climb chart and the listed condi ons to determine the
rate of climb - Ans 765 f.p.m.
What is the difference between the range and the endurance of an aircra0? - Ans With a given
amount of fuel, range is the distance that the aircra0 can fly, and endurance is the amount of
me that the aircra0 can remain in the air.
Center of gravity is defined as the theore cal point - Ans where all of the aircra0's weight is
considered to be concentrated
One of the items included in an aircra0's basic empty weight is - Ans unusable fuel
, What is the CG loca on a0er the airplane is loaded with full fuel? - Ans 42.66 inches
How much fuel can be carried in the aircra0 without exceeding a maximum takeoff weight of
2,700 pounds? - Ans 19.6 gallons
Using the loading specifica ons from the previous problem, the total moment is - Ans
113,8976.4 pound-inches
Assume an aircra0 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 ac on, if any, should you take before
you fly the aircra0? - Ans Move some load a0 in the aircra0
Based on the following condi ons, what is the total moment/1000 pound-inches? - Ans 96.8
According to the center of gravity moment envelope, the aircra0's CG is - Ans within normal
category limits but outside u lity category limits
The me-speed-distance func on of your flight computer can be used to solve for - Ans
groundspeed and fuel consump on
If your aircra0's fuel consump on 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? - Ans 13.8 gallons
Determine the density al tude using the listed condi ons - Ans 4097 feet
When you are flying an aircra0 into a le0-quartering headwind, what is the effect on
groundspeed and wind correc on angle if the wind velocity increases? - Ans Groundspeed
decreases, and wind correc on increases.
