FAA-H-8083-25C · Source PDF page 482
Glossary
Glossary · PHAK page G-6
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C Center of gravity limits. The specified forward and aft
points within which the CG must be located during flight.
Cabin altitude. Cabin pressure in terms of equivalent altitude
These limits are indicated on pertinent airplane specifications.
above sea level.
Center of gravity range. The distance between the forward
Cage. The black markings on the ball instrument indicating
and aft CG limits indicated on pertinent airplane specifications.
its neutral position.
Center of pressure. A point along the wing chord line where
Calibrated. The instrument indication compared with a
lift is considered to be concentrated. For this reason, the center
standard value to determine the accuracy of the instrument.
of pressure is commonly referred to as the center of lift.
Calibrated orifice. A hole of specific diameter used to delay
Centrifugal flow compressor. An impeller-shaped device
the pressure change in the case of a vertical speed indicator.
that receives air at its center and slings the air outward at high
velocity into a diffuser for increased pressure. Also referred
Calibrated airspeed. The speed at which the aircraft
to as a radial outflow compressor.
is moving through the air, found by correcting IAS for
instrument and position errors.
Centrifugal force. An outward force that opposes centripetal
force, resulting from the effect of inertia during a turn.
Camber. The camber of an airfoil is the characteristic curve
of its upper and lower surfaces. The upper camber is more
Centripetal force. A center-seeking force directed inward
pronounced, while the lower camber is comparatively flat.
toward the center of rotation created by the horizontal
This causes the velocity of the airflow immediately above the
component of lift in turning flight.
wing to be much higher than that below the wing.
CG. See center of gravity.
Canard. A horizontal surface mounted ahead of the main
wing to provide longitudinal stability and control. It may
Changeover point (COP). A point along the route or
be a fixed, movable, or variable geometry surface, with or
airway segment between two adjacent navigation facilities
without control surfaces.
or waypoints where changeover in navigation guidance
should occur.
Canard configuration. A configuration in which the span
of the forward wings is substantially less than that of the
Chart Supplement U.S. (formerly Airport/Facility
main wing.
Directory). An FAA publication containing information on
all airports, communications, and NAVAIDs.
Cantilever. A wing designed to carry loads without external
struts.
Checklist. A tool that is used as a human factors aid in
aviation safety. It is a systematic and sequential list of all
CAS. Calibrated airspeed.
operations that must be performed to properly accomplish
a task.
CDI. Course deviation indicator.
Chord line. An imaginary straight line drawn through an
Ceiling. The height above the earth’s surface of the lowest
airfoil from the leading edge to the trailing edge.
layer of clouds, which is reported as broken or overcast, or
the vertical visibility into an obscuration.
Circling approach. A maneuver initiated by the pilot to
align the aircraft with a runway for landing when a straight-
Center of gravity (CG). The point at which an airplane
in landing from an instrument approach is not possible or is
would balance if it were possible to suspend it at that point.
not desirable.
It is the mass center of the airplane, or the theoretical point
at which the entire weight of the airplane is assumed to
be concentrated. It may be expressed in inches from the
reference datum, or in percentage of mean aerodynamic
chord (MAC). The location depends on the distribution of
weight in the airplane.
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