Diagnostic Test For The Air Force Qualifying Page 20
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27DIAGNOSTIC TEST FOR THE AIR FORCE QUALIFYING TEST
PRACTICE TEST THREE
39. 3, 0
a.
98
4.
The _________ is a fireproof partition between
b.
6
the engine block and the cockpit.
c.
2
a.
Steel wall
d.
36
b.
Firewall
e.
12
c.
Blockade
d.
Smoke wall
40. -3, -1
e.
Coolant system
a.
20
b.
14
5.
What is the normal method for losing altitude?
c.
73
a.
A descent at minimum safe airspeed
d.
37
b.
A glide
e.
4
c.
A partial power descent
d.
All of the above
Subtest 8: Aviation Information
e.
None of the above
Directions: The Aviation Information subtest
6.
What is an adverse yaw?
measures your knowledge of aviation. This subtest is
a.
A yaw in the direction of the banked wing
common to all three service selection tests, although
b.
A yaw in the direction of the raised wing
the number of questions varies from one service to
c.
A yaw in the direction of airflow
another. Each of the questions or incomplete
d.
A yaw in the direction of the sun
statements is followed by five choices. You must
e.
None of the above
decide which one of the choices best completes the
statement or answers the question. Eliminating any
7.
Aircraft rudder effectiveness increases with
obviously incorrect choices first will increase your
_________.
chances of selecting the correct answer. You have
a.
Temperature
eight (8) minutes to complete this subtest.
b.
Altitude
c.
Headwind
Questions: 20
d.
Speed
Time: 8 minutes
e.
Tailwind
1.
Straight wings are ideal for ___________, but
8.
Which of the following is not one of the four
are not ideal for _____________.
traditional types of airspeed?
a.
Sonic flight, low speeds
a.
Indicated airspeed
b.
High speeds, low altitudes
b.
Calibrated airspeed
c.
Fighter aircraft, commercial aircraft
c.
Equivalent airspeed
d.
Low speeds, high speeds
d.
Pressurized airspeed
e.
None of the above
e.
True airspeed
2.
Which of the following are considered cargo
9.
Which of the following are considered attack
aircraft?
aircraft?
a.
C-2A Greyhound
a.
F-117A Nighthawk
b.
C-17 Globemaster III
b.
AC-130 H/U Gunship Spectre/Spooky
c.
C-21A Learjet
c.
A10 Thunderbolt II (“Warthog”)
d.
C-130 Hercules
d.
None of the above
e.
All of the above
e.
All of the above
3.
The primary flight control systems are:
a.
Wing flaps and landing gear
b.
Trim control systems
c.
Control wheel, instruments
d.
Throttle, altimeter
e.
Ailerons, elevator/stabilizer, rudder
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