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Archive / FAA Pilot’s Handbook of Aeronautical Knowledge / Pilot’s Handbook — Glossary

Glossary, Part 1

Glossary — Part 1

FAA-H-8083-25C (2023)

G-1

A

14 CFR. See Title 14 of the Code of Federal Regulations.

100-hour inspection. An inspection identical in scope to

an annual inspection. Conducted every 100 hours of flight

on aircraft of under 12,500 pounds that are used to carry

passengers for hire.

Absolute accuracy. The ability to determine present position

in space independently, and is most often used by pilots.

Absolute altitude. The actual distance between an aircraft

and the terrain over which it is flying.

Absolute pressure. Pressure measured from the reference

of zero pressure, or a vacuum.

A.C. Alternating current.

Acceleration. Force involved in overcoming inertia, and

which may be defined as a change in velocity per unit of time.

Acceleration error. A magnetic compass error apparent when

the aircraft accelerates while flying on an easterly or westerly

heading, causing the compass card to rotate toward North.

Accelerate-go distance. The distance required to accelerate

to V1 with all engines at takeoff power, experience an engine

failure at V 1, and continue the takeoff on the remaining

engine(s). The runway required includes the distance required

to climb to 35 feet by which time V2 speed must be attained.

Accelerate-stop distance. The distance required to accelerate

to V1 with all engines at takeoff power, experience an engine

failure at V1, and abort the takeoff and bring the airplane to

a stop using braking action only (use of thrust reversing is

not considered).

Accelerometer. A part of an inertial navigation system

(INS) that accurately measures the force of acceleration in

one direction.

Glossary

ADC. See air data computer.

ADF. See automatic direction finder.

ADI. See attitude director indicator.

Adiabatic cooling. A process of cooling the air through

expansion. For example, as air moves up slope it expands with

the reduction of atmospheric pressure and cools as it expands.

Adiabatic heating. A process of heating dry air through

compression. For example, as air moves down a slope it is

compressed, which results in an increase in temperature.

Adjustable-pitch propeller. A propeller with blades whose

pitch can be adjusted on the ground with the engine not

running, but which cannot be adjusted in flight. Also referred

to as a ground adjustable propeller. Sometimes also used to

refer to constant-speed propellers that are adjustable in flight.

Adjustable stabilizer. A stabilizer that can be adjusted in

flight to trim the airplane, thereby allowing the airplane to

fly hands-off at any given airspeed.

ADM. See aeronautical decision-making.

ADS-B. See automatic dependent surveillance-broadcast.

Advection fog. Fog resulting from the movement of warm,

humid air over a cold surface.

Adverse yaw. A condition of flight in which the nose of an

airplane tends to yaw toward the outside of the turn. This is

caused by the higher induced drag on the outside wing, which

is also producing more lift. Induced drag is a by-product of

the lift associated with the outside wing.

Aerodynamics. The science of the action of air on an object,

and with the motion of air on other gases. Aerodynamics

deals with the production of lift by the aircraft, the relative

wind, and the atmosphere.

G-2

Aeronautical chart. A map used in air navigation containing

all or part of the following: topographic features, hazards and

obstructions, navigation aids, navigation routes, designated

airspace, and airports.

Aeronautical decision-making (ADM). A systematic

approach to the mental process used by pilots to consistently

determine the best course of action in response to a given

set of circumstances.

Agonic line. An irregular imaginary line across the surface of

the Earth along which the magnetic and geographic poles are

in alignment, and along which there is no magnetic variation.

Ailerons. Primary flight control surfaces mounted on the

trailing edge of an airplane wing, near the tip. Ailerons control

roll about the longitudinal axis.

Aircraft. A device that is used, or intended to be used, for

flight.

Aircraft altitude. The actual height above sea level at which

the aircraft is flying.

Aircraft approach category. A performance grouping of

aircraft based on a speed of 1.3 times the stall speed in the

landing configuration at maximum gross landing weight.

Air data computer (ADC). An aircraft computer that

receives and processes pitot pressure, static pressure, and

temperature to calculate very precise altitude, indicated

airspeed, true airspeed, and air temperature.

Airfoil. Any surface, such as a wing, propeller, rudder, or

even a trim tab, which provides aerodynamic force when it

interacts with a moving stream of air.

Air mass. An extensive body of air having fairly uniform

properties of temperature and moisture.

AIRMET. Inflight weather advisory issued as an amendment

to the area forecast, concerning weather phenomena of

operational interest to all aircraft and that is potentially

hazardous to aircraft with limited capability due to lack of

equipment, instrumentation, or pilot qualifications.

Airplane. An engine-driven, fixed-wing aircraft heavier than

air that is supported in flight by the dynamic reaction of air

against its wings.

Airplane Flight Manual (AFM). A document developed

by the airplane manufacturer and approved by the Federal

Aviation Administration (FAA). It is specific to a particular

make and model airplane by serial number and it contains

operating procedures and limitations.

Airplane Owner/Information Manual. A document

developed by the airplane manufacturer containing general

information about the make and model of an airplane. The

airplane owner’s manual is not FAA approved and is not

specific to a particular serial numbered airplane. This manual

is not kept current, and therefore cannot be substituted for

the AFM/POH.

Airport diagram. The section of an instrument approach

procedure chart that shows a detailed diagram of the

airport. This diagram includes surface features and airport

configuration information.

Airport/Facility Directory (A/FD). See Chart Supplement

U.S.

Airport surface detection equipment (ASDE). Radar

equipment specifically designed to detect all principal

features and traffic on the surface of an airport, presenting the

entire image on the control tower console; used to augment

visual observation by tower personnel of aircraft and/or

vehicular movements on runways and taxiways.

Airport surveillance radar (ASR). Approach control

radar used to detect and display an aircraft’s position in the

terminal area.

Airport surveillance radar approach. An instrument

approach in which ATC issues instructions for pilot

compliance based on aircraft position in relation to the final

approach course and the distance from the end of the runway

as displayed on the controller’s radar scope.

Air route surveillance radar (ARSR). Air route traffic

control center (ARTCC) radar used primarily to detect

and display an aircraft’s position while en route between

terminal areas.

Air route traffic control center (ARTCC). Provides ATC

service to aircraft operating on IFR flight plans within

controlled airspace and principally during the en route phase

of flight.

Airspeed. Rate of the aircraft’s progress through the air.

G-3

Airspeed indicator. A differential pressure gauge that

measures the dynamic pressure of the air through which the

aircraft is flying. Displays the craft’s airspeed, typically in

knots, to the pilot.

Air traffic control radar beacon system (ATCRBS).

Sometimes called secondary surveillance radar (SSR), which

utilizes a transponder in the aircraft. The ground equipment is

an interrogating unit, in which the beacon antenna is mounted

so it rotates with the surveillance antenna. The interrogating

unit transmits a coded pulse sequence that actuates the aircraft

transponder. The transponder answers the coded sequence

by transmitting a preselected coded sequence back to the

ground equipment, providing a strong return signal and

positive aircraft identification, as well as other special data.

Airway. An airway is based on a centerline that extends from

one navigation aid or intersection to another navigation aid

(or through several navigation aids or intersections); used

to establish a known route for en route procedures between

terminal areas.

Airworthiness Certificate. A certificate issued by the FAA

to all aircraft that have been proven to meet the minimum

standards set down by the Code of Federal Regulations.

Airworthiness Directive. A regulatory notice sent out by

the FAA to the registered owner of an aircraft informing

the owner of a condition that prevents the aircraft from

continuing to meet its conditions for airworthiness.

Airworthiness Directives (AD notes) are to be complied with

within the required time limit, and the fact of compliance,

the date of compliance, and the method of compliance are

recorded in the aircraft’s maintenance records.

Alert area. An area in which there is a high volume of pilot

training or an unusual type of aeronautical activity.

Almanac data. Information the global positioning system

(GPS) receiver can obtain from one satellite which describes

the approximate orbital positioning of all satellites in the

constellation. This information is necessary for the GPS

receiver to know what satellites to look for in the sky at a

given time.

ALS. See approach lighting system.

Alternate airport. An airport designated in an IFR flight

plan, providing a suitable destination if a landing at the

intended airport becomes inadvisable.

Alternate static source valve. A valve in the instrument static

air system that supplies reference air pressure to the altimeter,

airspeed indicator, and vertical speed indicator if the normal

static pickup should become clogged or iced over.

Altimeter. A flight instrument that indicates altitude by

sensing pressure changes.

Altimeter setting. Station pressure (the barometric pressure

at the location the reading is taken) which has been corrected

for the height of the station above sea level.

Altitude engine. A reciprocating aircraft engine having a

rated takeoff power that is producible from sea level to an

established higher altitude.

Ambient pressure. The pressure in the area immediately

surrounding the aircraft.

Ambient temperature. The temperature in the area

immediately surrounding the aircraft.

AME. See aviation medical examiner.

Amendment status. The circulation date and revision

number of an instrument approach procedure, printed above

the procedure identification.

Ammeter. An instrument installed in series with an electrical

load used to measure the amount of current flowing through

the load.

Aneroid. The sensitive component in an altimeter or

barometer that measures the absolute pressure of the air.

It is a sealed, flat capsule made of thin disks of corrugated

metal soldered together and evacuated by pumping all of

the air out of it.

Aneroid barometer. An instrument that measures the

absolute pressure of the atmosphere by balancing the weight

of the air above it against the spring action of the aneroid.

Angle of attack. The angle of attack is the angle at which

relative wind meets an airfoil. It is the angle that is formed

by the chord of the airfoil and the direction of the relative

wind or between the chord line and the flight path. The

angle of attack changes during a flight as the pilot changes

the direction of the aircraft and is related to the amount of

lift being produced.

G-4

Angle of incidence. The acute angle formed between the

chord line of an airfoil and the longitudinal axis of the aircraft

on which it is mounted.

Anhedral. A downward slant from root to tip of an aircraft’s

wing or horizontal tail surface.

Annual inspection. A complete inspection of an aircraft and

engine, required by the Code of Federal Regulations, to be

accomplished every 12 calendar months on all certificated

aircraft. Only an A&P technician holding an Inspection

Authorization can conduct an annual inspection.

Anti-ice. Preventing the accumulation of ice on an aircraft

structure via a system designed for that purpose.

Antiservo tab. An adjustable tab attached to the trailing edge

of a stabilator that moves in the same direction as the primary

control. It is used to make the stabilator less sensitive.

Approach lighting system (ALS). Provides lights that will

penetrate the atmosphere far enough from touchdown to

give directional, distance, and glidepath information for safe

transition from instrument to visual flight.

Area chart. Part of the low-altitude en route chart series,

this chart furnishes terminal data at a larger scale for

congested areas.

Area forecast (FA). A report that gives a picture of clouds,

general weather conditions, and visual meteorological

conditions (VMC) expected over a large area encompassing

several states.

Area navigation (RNAV). Allows a pilot to fly a selected

course to a predetermined point without the need to overfly

ground-based navigation facilities, by using waypoints.

Arm. See moment arm.

ARSR. See air route surveillance radar.

ARTCC. See air route traffic control center.

ASDE. See airport surface detection equipment.

ASOS. See Automated Surface Observing System.

Aspect ratio. Span of a wing divided by its average chord.

ASR. See airport surveillance radar.

Asymmetric thrust. Also known as P-factor. A tendency for

an aircraft to yaw to the left due to the descending propeller

blade on the right producing more thrust than the ascending

blade on the left. This occurs when the aircraft’s longitudinal

axis is in a climbing attitude in relation to the relative wind.

The P-factor would be to the right if the aircraft had a

counterclockwise rotating propeller.

ATC. Air Traffic Control.

ATCRBS. See air traffic control radar beacon system.

ATIS. See automatic terminal information service.

Atmospheric propagation delay. A bending of the

electromagnetic (EM) wave from the satellite that creates

an error in the GPS system.

Attitude. A personal motivational predisposition to respond

to persons, situations, or events in a given manner that can,

nevertheless, be changed or modified through training as sort

of a mental shortcut to decision-making.

Attitude and heading reference system (AHRS). A system

composed of three-axis sensors that provide heading, attitude,

and yaw information for aircraft. AHRS are designed to

replace traditional mechanical gyroscopic flight instruments

and provide superior reliability and accuracy.

Attitude director indicator (ADI). An aircraft attitude

indicator that incorporates flight command bars to provide

pitch and roll commands.

Attitude indicator. The foundation for all instrument flight,

this instrument reflects the airplane’s attitude in relation to

the horizon.

Attitude instrument flying. Controlling the aircraft by

reference to the instruments rather than by outside visual cues.

Attitude management. The ability to recognize hazardous

attitudes in oneself and the willingness to modify them as

necessary through the application of an appropriate antidote

thought.

Autokinesis. Nighttime visual illusion that a stationary light

is moving, which becomes apparent after several seconds of

staring at the light.

G-5

Automated Surface Observing System (ASOS). Weather

reporting system which provides surface observations every

minute via digitized voice broadcasts and printed reports.

Automated Weather Observing System (AWOS).

Automated weather reporting system consisting of various

sensors, a processor, a computer-generated voice subsystem,

and a transmitter to broadcast weather data.

Automatic dependent surveillance—broadcast (ADS–B).

A function on an aircraft or vehicle that periodically

broadcasts its state vector (i.e., horizontal and vertical

position, horizontal and vertical velocity) and other

information.

Automatic direction finder (ADF). Electronic navigation

equipment that operates in the low- and medium-frequency

bands. Used in conjunction with the ground-based

nondirectional beacon (NDB), the instrument displays the

number of degrees clockwise from the nose of the aircraft

to the station being received.

Automatic terminal information service (ATIS). The

continuous broadcast of recorded non-control information in

selected terminal areas. Its purpose is to improve controller

effectiveness and relieve frequency congestion by automating

repetitive transmission of essential but routine information.

Autopilot. An automatic flight control system which keeps

an aircraft in level flight or on a set course. Automatic pilots

can be directed by the pilot, or they may be coupled to a radio

navigation signal.

Aviation medical examiner (AME). A physician with

training in aviation medicine designated by the Civil

Aerospace Medical Institute (CAMI).

Aviation Routine Weather Report (METAR). Observation

of current surface weather reported in a standard international

format.

AWOS. See Automated Weather Observing System.

Axes of an aircraft. Three imaginary lines that pass through

an aircraft’s center of gravity. The axes can be considered

as imaginary axles around which the aircraft rotates. The

three axes pass through the center of gravity at 90° angles to

each other. The axis from nose to tail is the longitudinal axis

(pitch), the axis that passes from wingtip to wingtip is the

lateral axis (roll), and the axis that passes vertically through

the center of gravity is the vertical axis (yaw).

Axial flow compressor. A type of compressor used in a

turbine engine in which the airflow through the compressor

is essentially linear. An axial-flow compressor is made up of

several stages of alternate rotors and stators. The compressor

ratio is determined by the decrease in area of the succeeding

stages.

Azimuth card. A card that may be set, gyroscopically

controlled, or driven by a remote compass.

B

Back course (BC). The reciprocal of the localizer course

for an ILS. When flying a back-course approach, an aircraft

approaches the instrument runway from the end at which the

localizer antennas are installed.

Balance tab. An auxiliary control mounted on a primary

control surface, which automatically moves in the direction

opposite the primary control to provide an aerodynamic

assist in the movement of the control.

Baro-aiding. A method of augmenting the GPS integrity

solution by using a nonsatellite input source. To ensure that

baro-aiding is available, the current altimeter setting must

be entered as described in the operating manual.

Barometric scale. A scale on the dial of an altimeter to which

the pilot sets the barometric pressure level from which the

altitude shown by the pointers is measured.

Basic empty weight (GAMA). Basic empty weight

includes the standard empty weight plus optional and special

equipment that has been installed.

BC. See back course.

Bernoulli’s Principle. A principle that explains how the

pressure of a moving fluid varies with its speed of motion.

An increase in the speed of movement causes a decrease in

the fluid’s pressure.

Biplanes. Airplanes with two sets of wings.

Block altitude. A block of altitudes assigned by ATC to

allow altitude deviations; for example, “Maintain block

altitude 9 to 11 thousand.”

Bypass ratio. The ratio of the mass airflow in pounds per

second through the fan section of a turbofan engine to the

mass airflow that passes through the gas generator portion

of the engine.

G-6

C

Cabin altitude. Cabin pressure in terms of equivalent altitude

above sea level.

Cage. The black markings on the ball instrument indicating

its neutral position.

Calibrated. The instrument indication compared with a

standard value to determine the accuracy of the instrument.

Calibrated orifice. A hole of specific diameter used to delay

the pressure change in the case of a vertical speed indicator.

Calibrated airspeed. The speed at which the aircraft

is moving through the air, found by correcting IAS for

instrument and position errors.

Camber. The camber of an airfoil is the characteristic curve

of its upper and lower surfaces. The upper camber is more

pronounced, while the lower camber is comparatively flat.

This causes the velocity of the airflow immediately above the

wing to be much higher than that below the wing.

Canard. A horizontal surface mounted ahead of the main

wing to provide longitudinal stability and control. It may

be a fixed, movable, or variable geometry surface, with or

without control surfaces.

Canard configuration. A configuration in which the span

of the forward wings is substantially less than that of the

main wing.

Cantilever. A wing designed to carry loads without external

struts.

CAS. Calibrated airspeed.

CDI. Course deviation indicator.

Ceiling. The height above the earth’s surface of the lowest

layer of clouds, which is reported as broken or overcast, or

the vertical visibility into an obscuration.

Center of gravity (CG). The point at which an airplane

would balance if it were possible to suspend it at that point.

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.

Center of gravity limits. The specified forward and aft

points within which the CG must be located during flight.

These limits are indicated on pertinent airplane specifications.

Center of gravity range. The distance between the forward

and aft CG limits indicated on pertinent airplane specifications.

Center of pressure. A point along the wing chord line where

lift is considered to be concentrated. For this reason, the center

of pressure is commonly referred to as the center of lift.

Centrifugal flow compressor. An impeller-shaped device

that receives air at its center and slings the air outward at high

velocity into a diffuser for increased pressure. Also referred

to as a radial outflow compressor.

Centrifugal force. An outward force that opposes centripetal

force, resulting from the effect of inertia during a turn.

Centripetal force. A center-seeking force directed inward

toward the center of rotation created by the horizontal

component of lift in turning flight.

CG. See center of gravity.

Changeover point (COP). A point along the route or

airway segment between two adjacent navigation facilities

or waypoints where changeover in navigation guidance

should occur.

Chart Supplement U.S. (formerly Airport/Facility

Directory). An FAA publication containing information on

all airports, communications, and NAVAIDs.

Checklist. A tool that is used as a human factors aid in

aviation safety. It is a systematic and sequential list of all

operations that must be performed to properly accomplish

a task.

Chord line. An imaginary straight line drawn through an

airfoil from the leading edge to the trailing edge.

Circling approach. A maneuver initiated by the pilot to

align the aircraft with a runway for landing when a straight-

in landing from an instrument approach is not possible or is

not desirable.

G-7

Class A airspace. Airspace from 18,000 feet MSL up to and

including FL 600, including the airspace overlying the waters

within 12 NM of the coast of the 48 contiguous states and

Alaska; and designated international airspace beyond 12 NM

of the coast of the 48 contiguous states and Alaska within areas

of domestic radio navigational signal or ATC radar coverage,

and within which domestic procedures are applied.

Class B airspace. Airspace from the surface to 10,000 feet

MSL surrounding the nation’s busiest airports in terms of

IFR operations or passenger numbers. The configuration of

each Class B airspace is individually tailored and consists

of a surface area and two or more layers, and is designed to

contain all published instrument procedures once an aircraft

enters the airspace. For all aircraft, an ATC clearance is

required to operate in the area, and aircraft so cleared receive

separation services within the airspace.

Class C airspace. Airspace from the surface to 4,000 feet

above the airport elevation (charted in MSL) surrounding

those airports having an operational control tower, serviced

by radar approach control, and having a certain number of IFR

operations or passenger numbers. Although the configuration

of each Class C airspace area is individually tailored, the

airspace usually consists of a 5 NM radius core surface area

that extends from the surface up to 4,000 feet above the airport

elevation, and a 10 NM radius shelf area that extends from

1,200 feet to 4,000 feet above the airport elevation.

Class D airspace. Airspace from the surface to 2,500 feet

above the airport elevation (charted in MSL) surrounding

those airports that have an operational control tower. The

configuration of each Class D airspace area is individually

tailored, and when instrument procedures are published, the

airspace is normally designed to contain the procedures.

Class E airspace. Airspace that is not Class A, Class B, Class

C, or Class D, and is controlled airspace.

Class G airspace. Airspace that is uncontrolled, except

when associated with a temporary control tower, and has

not been designated as Class A, Class B, Class C, Class D,

or Class E airspace.

Clean configuration. A configuration in which all flight

control surfaces have been placed to create minimum drag.

In most aircraft this means flaps and gear retracted.

Clearance. ATC permission for an aircraft to proceed under

specified traffic conditions within controlled airspace, for

the purpose of providing separation between known aircraft.

Clearance delivery. Control tower position responsible for

transmitting departure clearances to IFR flights.

Clearance limit. The fix, point, or location to which an

aircraft is cleared when issued an air traffic clearance.

Clearance on request. An IFR clearance not yet received

after filing a flight plan.

Clearance void time. Used by ATC, the time at which the

departure clearance is automatically canceled if takeoff has

not been made. The pilot must obtain a new clearance or

cancel the IFR flight plan if not off by the specified time.

Clear ice. Glossy, clear, or translucent ice formed by the

relatively slow freezing of large, supercooled water droplets.

Coefficient of lift (CL). The ratio between lift pressure and

dynamic pressure.

Cold front. The boundary between two air masses where

cold air is replacing warm air.

Compass course. A true course corrected for variation and

deviation errors.

Compass locator. A low-power, low- or medium-frequency

(L/MF) radio beacon installed at the site of the outer or middle

marker of an ILS.

Compass rose. A small circle graduated in 360° increments,

to show direction expressed in degrees.

Complex aircraft. An aircraft with retractable landing gear,

flaps, and a controllable-pitch propeller.

Compressor pressure ratio. The ratio of compressor

discharge pressure to compressor inlet pressure.

Compressor stall. In gas turbine engines, a condition in

an axial-flow compressor in which one or more stages of

rotor blades fail to pass air smoothly to the succeeding

stages. A stall condition is caused by a pressure ratio that is

incompatible with the engine rpm. Compressor stall will be

indicated by a rise in exhaust temperature or rpm fluctuation,

and if allowed to continue, may result in flameout and

physical damage to the engine.

Computer navigation fix. A point used to define a

navigation track for an airborne computer system such as

GPS or FMS.

G-8

Concentric rings. Dashed-line circles depicted in the plan

view of IAP charts, outside of the reference circle, that show

en route and feeder facilities.

Condensation. A change of state of water from a gas (water

vapor) to a liquid.

Condensation nuclei. Small particles of solid matter in the

air on which water vapor condenses.

Cone of confusion. A cone-shaped volume of airspace

directly above a VOR station where no signal is received,

causing the CDI to fluctuate.

Configuration. This is a general term, which normally refers

to the position of the landing gear and flaps.

Constant-speed propeller. A controllable-pitch propeller

whose pitch is automatically varied in flight by a governor

to maintain a constant rpm in spite of varying air loads.

Continuous flow oxygen system. System that supplies

a constant supply of pure oxygen to a rebreather bag that

dilutes the pure oxygen with exhaled gases and thus supplies a

healthy mix of oxygen and ambient air to the mask. Primarily

used in passenger cabins of commercial airliners.

Control and performance. A method of attitude instrument

flying in which one instrument is used for making attitude

changes, and the other instruments are used to monitor the

progress of the change.

Control display unit. A display interfaced with the master

computer, providing the pilot with a single control point

for all navigations systems, thereby reducing the number of

required flight deck panels.

Controllability. A measure of the response of an aircraft

relative to the pilot’s flight control inputs.

Controllable-pitch propeller (CPP). A type of propeller

with blades that can be rotated around their long axis to

change their pitch. If the pitch can be set to negative values,

the reversible propeller can also create reverse thrust for

braking or reversing without the need of changing the

direction of shaft revolutions.

Controlled airspace. An airspace of defined dimensions

within which ATC service is provided to IFR and VFR flights

in accordance with the airspace classification. It includes

Class A, Class B, Class C, Class D, and Class E airspace.

Control pressures. The amount of physical exertion on the

control column necessary to achieve the desired attitude.

Convective weather. Unstable, rising air found in

cumiliform clouds.

Convective SIGMET. Weather advisory concerning

convective weather significant to the safety of all aircraft,

including thunderstorms, hail, and tornadoes.

Conventional landing gear. Landing gear employing a third

rear-mounted wheel. These airplanes are also sometimes

referred to as tailwheel airplanes.

Coordinated flight. Flight with a minimum disturbance of

the forces maintaining equilibrium, established via effective

control use.

COP. See changeover point.

Coriolis illusion. The illusion of rotation or movement in an

entirely different axis, caused by an abrupt head movement,

while in a prolonged constant-rate turn that has ceased to

stimulate the brain’s motion sensing system.

Coupled ailerons and rudder. Rudder and ailerons are

connected with interconnected springs in order to counteract

adverse yaw. Can be overridden if it becomes necessary to

slip the aircraft.

Course. The intended direction of flight in the horizontal

plane measured in degrees from north.

Cowl flaps. Shutter-like devices arranged around certain

air-cooled engine cowlings, which may be opened or closed

to regulate the flow of air around the engine.

Crew resource management (CRM). The application of

team management concepts in the flight deck environment.

It was initially known as cockpit resource management,

but as CRM programs evolved to include cabin crews,

maintenance personnel, and others, the phrase “crew

resource management” was adopted. This includes single

pilots, as in most general aviation aircraft. Pilots of small

aircraft, as well as crews of larger aircraft, must make

effective use of all available resources; human resources,

hardware, and information. A current definition includes

all groups routinely working with the flight crew who

are involved in decisions required to operate a flight

safely. These groups include, but are not limited to pilots,

dispatchers, cabin crewmembers, maintenance personnel,

and air traffic controllers. CRM is one way of addressing

the challenge of optimizing the human/machine interface

and accompanying interpersonal activities.

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