AFOQT ACTUAL FINAL EXAM QUESTIONS AND
ANSWERS SURE A+
✔✔The amount of lift generated is dependent on the difference between the camber
line and the____ - ✔✔Chord line
✔✔If an engine produces 3500 pounds of thrust and travels at 500 mph, what is the
thp? - ✔✔4666.67
✔✔This functional landing gear style is helpful when landing on non paved runways -
✔✔Tail wheel
✔✔The main and tail portions of this landing gear style are positioned along the
longitudinal axis - ✔✔Tandem
✔✔This landing gear style includes a nose gesr - ✔✔Tricycle
✔✔This landing gear style is required when the main landing gear is positioned forward
of the aircrafts CG - ✔✔Tail wheel
✔✔What component is designed to relieve pressure on the controls - ✔✔The trim tabs
, ✔✔Which components help optimize the performance of an aircraft as part of the
secondary flight control system - ✔✔The leading edge devices and the spoilers
✔✔Which is not considered necessary to achieve straight and level flight - ✔✔Moving
the flight controls
✔✔What action must a pilot perform when flying out of a steep turn that is not usually
required during shallow and medium turns - ✔✔Input opposite pressure on the controls
✔✔Which statement is correct regarding the best rate of climb - ✔✔The most altitude in
a given amount of time can be obtained
✔✔What is the standard rate of descent for a partial power descent - ✔✔500 fpm
✔✔Which rotary wing aircraft component allows the rotor hub blades to flap - ✔✔The
teeter hinge
✔✔Which direction will a rotary wing aircraft roll due to the transverse flow effect -
✔✔Laterally
✔✔Which primary rotary wing flight control increases the pitch angle of the blades
simultaneously - ✔✔The collective
✔✔Air pressure decreases 1 inch of mercury for each ____ feet of altitude - ✔✔1000
✔✔An increase in the static pressure, as measured around the diaphragm inside the
VSI, indicates an aircraft is in which of the following maneuvers - ✔✔A climb
✔✔Which type of airspeed is displayed on the airspeed indicator - ✔✔Indicated
airspeed
✔✔What is the purpose of the turn and slip indicator - ✔✔To indicate if the pilot is
making a coordinated left or right standard turn
✔✔The lateral axis of an aircraft controls what - ✔✔Pitch
✔✔If the variation between magnetic North Pole and the true North Pole is greater than
+12 degrees west, how does a pilot adjust for the compass heading - ✔✔By adding 12
degrees to the compass heading displayed
✔✔What are the different types of marked runways - ✔✔Precision instrument, non
precision instrument, and visual
ANSWERS SURE A+
✔✔The amount of lift generated is dependent on the difference between the camber
line and the____ - ✔✔Chord line
✔✔If an engine produces 3500 pounds of thrust and travels at 500 mph, what is the
thp? - ✔✔4666.67
✔✔This functional landing gear style is helpful when landing on non paved runways -
✔✔Tail wheel
✔✔The main and tail portions of this landing gear style are positioned along the
longitudinal axis - ✔✔Tandem
✔✔This landing gear style includes a nose gesr - ✔✔Tricycle
✔✔This landing gear style is required when the main landing gear is positioned forward
of the aircrafts CG - ✔✔Tail wheel
✔✔What component is designed to relieve pressure on the controls - ✔✔The trim tabs
, ✔✔Which components help optimize the performance of an aircraft as part of the
secondary flight control system - ✔✔The leading edge devices and the spoilers
✔✔Which is not considered necessary to achieve straight and level flight - ✔✔Moving
the flight controls
✔✔What action must a pilot perform when flying out of a steep turn that is not usually
required during shallow and medium turns - ✔✔Input opposite pressure on the controls
✔✔Which statement is correct regarding the best rate of climb - ✔✔The most altitude in
a given amount of time can be obtained
✔✔What is the standard rate of descent for a partial power descent - ✔✔500 fpm
✔✔Which rotary wing aircraft component allows the rotor hub blades to flap - ✔✔The
teeter hinge
✔✔Which direction will a rotary wing aircraft roll due to the transverse flow effect -
✔✔Laterally
✔✔Which primary rotary wing flight control increases the pitch angle of the blades
simultaneously - ✔✔The collective
✔✔Air pressure decreases 1 inch of mercury for each ____ feet of altitude - ✔✔1000
✔✔An increase in the static pressure, as measured around the diaphragm inside the
VSI, indicates an aircraft is in which of the following maneuvers - ✔✔A climb
✔✔Which type of airspeed is displayed on the airspeed indicator - ✔✔Indicated
airspeed
✔✔What is the purpose of the turn and slip indicator - ✔✔To indicate if the pilot is
making a coordinated left or right standard turn
✔✔The lateral axis of an aircraft controls what - ✔✔Pitch
✔✔If the variation between magnetic North Pole and the true North Pole is greater than
+12 degrees west, how does a pilot adjust for the compass heading - ✔✔By adding 12
degrees to the compass heading displayed
✔✔What are the different types of marked runways - ✔✔Precision instrument, non
precision instrument, and visual
