FAA GLIDER PILOT LICENSE EXAMINATION
COMPLETE QUESTIONS AND DETAILED SOLUTIONS
LATEST UPDATE THIS YEAR JUST RELEASED
Examination Coverage Areas
1. Glider aerodynamics and principles of flight — lift, drag, stability, stalls, spins, and energy management.
2. Glider performance and limitations — best glide, minimum sink, maneuvering speed, VNE, loading, and
performance effects.
3. Flight controls and instruments — primary controls, trim, airspeed, variometer, altimeter, compass, and
yaw coordination.
4. Preflight and ground operations — inspection, assembly, control connections, tow equipment, launch
preparation, and taxiing.
5. Launch procedures — aerotow, ground tow, winch launches, signals, tow emergencies, and release
procedures.
6. Traffic patterns, approaches, and landings — pattern planning, spoilers/airbrakes, wind correction, slips,
and accuracy landings.
7. Soaring meteorology — thermals, ridge lift, wave lift, wind, clouds, fronts, turbulence, and convective
hazards.
8. Soaring techniques and cross-country flight — thermalling, ridge soaring, navigation, route planning,
altitude management, and outlandings.
9. Emergency procedures and risk management — rope breaks, off-field landings, spins, equipment failures,
collision avoidance, and ADM.
10.FAA regulations and pilot responsibilities — certification, aeronautical experience, towing rules, airspace,
right-of-way, weather minimums, and operating limitations. Current FAA practical-test material includes a
Private Pilot Practical Test Standard for Glider Category, FAA-S-8081-22A. (
1.
A glider pilot notices that increasing airspeed during a straight glide requires
substantially more altitude loss per unit of horizontal distance. Which
aerodynamic change best explains this observation?
A. Induced drag has disappeared completely
B. Parasite drag has increased significantly
C. Lift has become completely independent of airspeed
D. The glider has entered a stalled condition
Answer: B. Parasite drag has increased significantly
,Rationale: Parasite drag increases with airspeed, so flying substantially faster than
the optimum glide speed increases total drag and reduces glide efficiency.
2.
Why does a glider normally require a continuous exchange of altitude for forward
motion when atmospheric lift is unavailable?
A. Gliders have no wings capable of producing lift
B. Gliders require engine thrust to maintain aerodynamic stability
C. Gliders use gravitational potential energy to overcome aerodynamic drag
D. Gliders cannot maintain airspeed without increasing their altitude
Answer: C. Gliders use gravitational potential energy to overcome aerodynamic
drag
Rationale: A glider converts potential energy from altitude into kinetic energy and
aerodynamic work while descending through still air.
3.
During a coordinated turn, what primary aerodynamic effect must the pilot
account for when increasing bank angle while maintaining altitude?
A. The vertical component of lift decreases
B. The horizontal component of lift disappears
C. Total lift requirement decreases dramatically
D. Induced drag becomes completely negligible
,Answer: A. The vertical component of lift decreases
Rationale: Banking tilts the lift vector, reducing its vertical component, so
additional total lift is required to maintain altitude.
4.
A glider pilot increases bank angle while attempting to maintain altitude without
increasing angle of attack or airspeed. What is the most likely result?
A. The glider climbs because lift increases automatically
B. The glider maintains altitude because bank angle does not affect lift
C. The glider descends because insufficient vertical lift remains
D. The glider accelerates vertically upward because induced drag decreases
Answer: C. The glider descends because insufficient vertical lift remains
Rationale: Increased bank reduces the vertical component of lift, requiring
additional lift production to maintain altitude during a level turn.
5.
Which statement most accurately describes induced drag on a glider operating at
relatively low airspeeds?
A. Induced drag generally increases as airspeed decreases
B. Induced drag disappears whenever the wings produce lift
C. Induced drag remains constant regardless of loading
D. Induced drag increases only when spoilers are extended
, Answer: A. Induced drag generally increases as airspeed decreases
Rationale: At lower airspeeds, greater angles of attack are generally required to
produce lift, increasing induced drag associated with wingtip vortices.
6.
What aerodynamic condition exists when the wing exceeds its critical angle of
attack, regardless of the indicated airspeed?
A. Best glide condition
B. Stall condition
C. Maximum range condition
D. Minimum sink condition
Answer: B. Stall condition
Rationale: A stall occurs when the wing exceeds its critical angle of attack, not
simply because the aircraft reaches one particular indicated airspeed.
7.
Why can a glider stall at an airspeed significantly higher than its published
straight-and-level stall speed?
A. Stall speed never changes with aircraft loading
B. Bank angle and load factor can increase the stall speed
C. Wind always increases indicated airspeed during turns
D. The variometer directly changes the critical angle of attack
COMPLETE QUESTIONS AND DETAILED SOLUTIONS
LATEST UPDATE THIS YEAR JUST RELEASED
Examination Coverage Areas
1. Glider aerodynamics and principles of flight — lift, drag, stability, stalls, spins, and energy management.
2. Glider performance and limitations — best glide, minimum sink, maneuvering speed, VNE, loading, and
performance effects.
3. Flight controls and instruments — primary controls, trim, airspeed, variometer, altimeter, compass, and
yaw coordination.
4. Preflight and ground operations — inspection, assembly, control connections, tow equipment, launch
preparation, and taxiing.
5. Launch procedures — aerotow, ground tow, winch launches, signals, tow emergencies, and release
procedures.
6. Traffic patterns, approaches, and landings — pattern planning, spoilers/airbrakes, wind correction, slips,
and accuracy landings.
7. Soaring meteorology — thermals, ridge lift, wave lift, wind, clouds, fronts, turbulence, and convective
hazards.
8. Soaring techniques and cross-country flight — thermalling, ridge soaring, navigation, route planning,
altitude management, and outlandings.
9. Emergency procedures and risk management — rope breaks, off-field landings, spins, equipment failures,
collision avoidance, and ADM.
10.FAA regulations and pilot responsibilities — certification, aeronautical experience, towing rules, airspace,
right-of-way, weather minimums, and operating limitations. Current FAA practical-test material includes a
Private Pilot Practical Test Standard for Glider Category, FAA-S-8081-22A. (
1.
A glider pilot notices that increasing airspeed during a straight glide requires
substantially more altitude loss per unit of horizontal distance. Which
aerodynamic change best explains this observation?
A. Induced drag has disappeared completely
B. Parasite drag has increased significantly
C. Lift has become completely independent of airspeed
D. The glider has entered a stalled condition
Answer: B. Parasite drag has increased significantly
,Rationale: Parasite drag increases with airspeed, so flying substantially faster than
the optimum glide speed increases total drag and reduces glide efficiency.
2.
Why does a glider normally require a continuous exchange of altitude for forward
motion when atmospheric lift is unavailable?
A. Gliders have no wings capable of producing lift
B. Gliders require engine thrust to maintain aerodynamic stability
C. Gliders use gravitational potential energy to overcome aerodynamic drag
D. Gliders cannot maintain airspeed without increasing their altitude
Answer: C. Gliders use gravitational potential energy to overcome aerodynamic
drag
Rationale: A glider converts potential energy from altitude into kinetic energy and
aerodynamic work while descending through still air.
3.
During a coordinated turn, what primary aerodynamic effect must the pilot
account for when increasing bank angle while maintaining altitude?
A. The vertical component of lift decreases
B. The horizontal component of lift disappears
C. Total lift requirement decreases dramatically
D. Induced drag becomes completely negligible
,Answer: A. The vertical component of lift decreases
Rationale: Banking tilts the lift vector, reducing its vertical component, so
additional total lift is required to maintain altitude.
4.
A glider pilot increases bank angle while attempting to maintain altitude without
increasing angle of attack or airspeed. What is the most likely result?
A. The glider climbs because lift increases automatically
B. The glider maintains altitude because bank angle does not affect lift
C. The glider descends because insufficient vertical lift remains
D. The glider accelerates vertically upward because induced drag decreases
Answer: C. The glider descends because insufficient vertical lift remains
Rationale: Increased bank reduces the vertical component of lift, requiring
additional lift production to maintain altitude during a level turn.
5.
Which statement most accurately describes induced drag on a glider operating at
relatively low airspeeds?
A. Induced drag generally increases as airspeed decreases
B. Induced drag disappears whenever the wings produce lift
C. Induced drag remains constant regardless of loading
D. Induced drag increases only when spoilers are extended
, Answer: A. Induced drag generally increases as airspeed decreases
Rationale: At lower airspeeds, greater angles of attack are generally required to
produce lift, increasing induced drag associated with wingtip vortices.
6.
What aerodynamic condition exists when the wing exceeds its critical angle of
attack, regardless of the indicated airspeed?
A. Best glide condition
B. Stall condition
C. Maximum range condition
D. Minimum sink condition
Answer: B. Stall condition
Rationale: A stall occurs when the wing exceeds its critical angle of attack, not
simply because the aircraft reaches one particular indicated airspeed.
7.
Why can a glider stall at an airspeed significantly higher than its published
straight-and-level stall speed?
A. Stall speed never changes with aircraft loading
B. Bank angle and load factor can increase the stall speed
C. Wind always increases indicated airspeed during turns
D. The variometer directly changes the critical angle of attack
