FAA-H-8083-25C · Source PDF page 477
Glossary
Glossary · PHAK page G-1
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Glossary
A ADC. See air data computer.
14 CFR. See Title 14 of the Code of Federal Regulations.
ADF. See automatic direction finder.
100-hour inspection. An inspection identical in scope to
ADI. See attitude director indicator.
an annual inspection. Conducted every 100 hours of flight
on aircraft of under 12,500 pounds that are used to carry
Adiabatic cooling. A process of cooling the air through
passengers for hire.
expansion. For example, as air moves up slope it expands with
the reduction of atmospheric pressure and cools as it expands.
Absolute accuracy. The ability to determine present position
in space independently, and is most often used by pilots.
Adiabatic heating. A process of heating dry air through
compression. For example, as air moves down a slope it is
Absolute altitude. The actual distance between an aircraft
compressed, which results in an increase in temperature.
and the terrain over which it is flying.
Adjustable-pitch propeller. A propeller with blades whose
Absolute pressure. Pressure measured from the reference
pitch can be adjusted on the ground with the engine not
of zero pressure, or a vacuum.
running, but which cannot be adjusted in flight. Also referred
to as a ground adjustable propeller. Sometimes also used to
A.C. Alternating current.
refer to constant-speed propellers that are adjustable in flight.
Acceleration. Force involved in overcoming inertia, and
Adjustable stabilizer. A stabilizer that can be adjusted in
which may be defined as a change in velocity per unit of time.
flight to trim the airplane, thereby allowing the airplane to
fly hands-off at any given airspeed.
Acceleration error. A magnetic compass error apparent when
the aircraft accelerates while flying on an easterly or westerly
ADM. See aeronautical decision-making.
heading, causing the compass card to rotate toward North.
ADS-B. See automatic dependent surveillance-broadcast.
Accelerate-go distance. The distance required to accelerate
to V with all engines at takeoff power, experience an engine
1 Advection fog. Fog resulting from the movement of warm,
failure at V , and continue the takeoff on the remaining
1 humid air over a cold surface.
engine(s). The runway required includes the distance required
to climb to 35 feet by which time V speed must be attained.
2 Adverse yaw. A condition of flight in which the nose of an
airplane tends to yaw toward the outside of the turn. This is
Accelerate-stop distance. The distance required to accelerate
caused by the higher induced drag on the outside wing, which
to V with all engines at takeoff power, experience an engine
1 is also producing more lift. Induced drag is a by-product of
failure at V , and abort the takeoff and bring the airplane to
1 the lift associated with the outside wing.
a stop using braking action only (use of thrust reversing is
not considered).
Aerodynamics. The science of the action of air on an object,
and with the motion of air on other gases. Aerodynamics
Accelerometer. A part of an inertial navigation system
deals with the production of lift by the aircraft, the relative
(INS) that accurately measures the force of acceleration in
wind, and the atmosphere.
one direction.
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