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

Glossary, Part 5

Glossary — Part 5

FAA-H-8083-25C (2023)

G-30

TEC. See Tower En Route Control.

Technique. The manner in which procedures are executed.

Telephone information briefing service (TIBS). An FSS

service providing continuously updated automated telephone

recordings of area and/or route weather, airspace procedures,

and special aviation-oriented announcements.

Temporary flight restriction (TFR). Restriction to flight

imposed in order to:

1. Protect persons and property in the air or on the surface

from an existing or imminent flight associated hazard;

2. Provide a safe environment for the operation of

disaster relief aircraft;

3. Prevent an unsafe congestion of sightseeing aircraft

above an incident;

4. Protect the President, Vice President, or other public

figures; and,

5. Provide a safe environment for space agency

operations.

Pilots are expected to check appropriate NOTAMs during

flight planning when conducting flight in an area where a

temporary flight restriction is in effect.

Tension. Maintaining an excessively strong grip on the control

column, usually resulting in an overcontrolled situation.

Terminal aerodrome forecast (TAF). A report established

for the 5 statute mile radius around an airport. Utilizes the

same descriptors and abbreviations as the METAR report.

Terminal arrival area (TAA). A procedure to provide a

new transition method for arriving aircraft equipped with

FMS and/or GPS navigational equipment. The TAA contains

a “T” structure that normally provides a NoPT for aircraft

using the approach.

Terminal instrument approach procedure (TERP).

Prescribes standardized methods for use in designing

instrument flight procedures.

TERP. See terminal instrument approach procedure.

Terminal radar service areas (TRSA). Areas where

participating pilots can receive additional radar services. The

purpose of the service is to provide separation between all

IFR operations and participating VFR aircraft.

Terrain awareness and warning system (TAWS). A

timed-based system that provides information concerning

potential hazards with fixed objects by using GPS positioning

and a database of terrain and obstructions to provide true

predictability of the upcoming terrain and obstacles.

TFR. See temporary flight restriction.

Thermosphere. The last layer of the atmosphere that begins

above the mesosphere and gradually fades away into space.

Threshold crossing height (TCH). The theoretical height

above the runway threshold at which the aircraft’s glideslope

antenna would be if the aircraft maintained the trajectory

established by the mean ILS glideslope or MLS glidepath.

Thrust. The force which imparts a change in the velocity of a

mass. This force is measured in pounds but has no element of

time or rate. The term “thrust required” is generally associated

with jet engines. A forward force which propels the airplane

through the air.

Thrust (aerodynamic force). The forward aerodynamic

force produced by a propeller, fan, or turbojet engine as it

forces a mass of air to the rear, behind the aircraft.

Thrust line. An imaginary line passing through the center of

the propeller hub, perpendicular to the plane of the propeller

rotation.

Time and speed table. A table depicted on an instrument

approach procedure chart that identifies the distance from the

FAF to the MAP, and provides the time required to transit

that distance based on various groundspeeds.

Timed turn. A turn in which the clock and the turn

coordinator are used to change heading a definite number

of degrees in a given time.

TIS. See traffic information service.

Title 14 of the Code of Federal Regulations (14 CFR).

Includes the federal aviation regulations governing the

operation of aircraft, airways, and airmen.

Torque. (1) A resistance to turning or twisting. (2) Forces that

produce a twisting or rotating motion. (3) In an airplane, the

tendency of the aircraft to turn (roll) in the opposite direction

of rotation of the engine and propeller. (4) In helicopters with

a single, main rotor system, the tendency of the helicopter

to turn in the opposite direction of the main rotor rotation.

G-31

Torquemeter. An instrument used with some of the larger

reciprocating engines and turboprop or turboshaft engines to

measure the reaction between the propeller reduction gears

and the engine case.

Total drag. The sum of the parasite drag and induced drag.

Touchdown zone elevation (TDZE). The highest elevation

in the first 3,000 feet of the landing surface, TDZE is

indicated on the instrument approach procedure chart when

straight-in landing minimums are authorized.

Touchdown zone lights. Two rows of transverse light bars

disposed symmetrically about the runway centerline in the

runway touchdown zone.

Tower En Route Control (TEC). The control of IFR

en route traffic within delegated airspace between two

or more adjacent approach control facilities, designed to

expedite traffic and reduce control and pilot communication

requirements.

TPP. See United States Terminal Procedures Publication.

Track. The actual path made over the ground in flight.

Tracking. Flying a heading that will maintain the desired

track to or from the station regardless of crosswind conditions.

Traffic Alert Collision Avoidance System (TCAS).

An airborne system developed by the FAA that operates

independently from the ground-based Air Traffic Control

system. Designed to increase flight deck awareness of

proximate aircraft and to serve as a “last line of defense” for

the prevention of midair collisions.

Traffic information service (TIS). A ground-based service

providing information to the flight deck via data link using

the S-mode transponder and altitude encoder to improve the

safety and efficiency of “see and avoid” flight through an

automatic display that informs the pilot of nearby traffic.

Trailing edge. The portion of the airfoil where the airflow

over the upper surface rejoins the lower surface airflow.

Transcribed Weather Broadcast (TWEB). An FSS service,

available in Alaska only, providing continuously updated

automated broadcast of meteorological and aeronautical data

over selected L/MF and VOR NAVAIDs.

Transponder. The airborne portion of the ATC radar

beacon system.

Transponder code. One of 4,096 four-digit discrete codes

ATC assigns to distinguish between aircraft.

Trend. Immediate indication of the direction of aircraft

movement, as shown on instruments.

Tricycle gear. Landing gear employing a third wheel located

on the nose of the aircraft.

Trim. To adjust the aerodynamic forces on the control

surfaces so that the aircraft maintains the set attitude without

any control input.

Trim tab. A small auxiliary hinged portion of a movable

control surface that can be adjusted during flight to a position

resulting in a balance of control forces.

Tropopause. The boundary layer between the troposphere

and the stratosphere which acts as a lid to confine most of the

water vapor, and the associated weather, to the troposphere.

Troposphere. The layer of the atmosphere extending from

the surface to a height of 20,000 to 60,000 feet, depending

on latitude.

True airspeed. Actual airspeed, determined by applying a

correction for pressure altitude and temperature to the CAS.

True altitude. The vertical distance of the airplane above

sea level—the actual altitude. It is often expressed as feet

above mean sea level (MSL). Airport, terrain, and obstacle

elevations on aeronautical charts are true altitudes.

Truss. A fuselage design made up of supporting structural

members that resist deformation by applied loads. The truss-

type fuselage is constructed of steel or aluminum tubing.

Strength and rigidity is achieved by welding the tubing

together into a series of triangular shapes, called trusses.

T-tail. An aircraft with the horizontal stabilizer mounted on

the top of the vertical stabilizer, forming a T.

Turbine discharge pressure. The total pressure at the

discharge of the low-pressure turbine in a dual-turbine axial-

flow engine.

Turbine engine. An aircraft engine which consists of an

air compressor, a combustion section, and a turbine. Thrust

is produced by increasing the velocity of the air flowing

through the engine.

G-32

Turbocharger. An air compressor driven by exhaust gases,

which increases the pressure of the air going into the engine

through the carburetor or fuel injection system.

Turbofan engine. A fanlike turbojet engine designed to

create additional thrust by diverting a secondary airflow

around the combustion chamber.

Turbojet engine. A turbine engine which produces its thrust

entirely by accelerating the air through the engine.

Turboprop engine. A turbine engine which drives a

propeller through a reduction gearing arrangement. Most of

the energy in the exhaust gases is converted into torque, rather

than using its acceleration to drive the aircraft.

Turboshaft engine. A gas turbine engine that delivers power

through a shaft to operate something other than a propeller.

Turn-and-slip indicator. A flight instrument consisting

of a rate gyro to indicate the rate of yaw and a curved glass

inclinometer to indicate the relationship between gravity and

centrifugal force. The turn-and-slip indicator indicates the

relationship between angle of bank and rate of yaw. Also

called a turn-and-bank indicator.

Turn coordinator. A rate gyro that senses both roll and

yaw due to the gimbal being canted. Has largely replaced

the turn-and-slip indicator in modern aircraft.

TWEB. See Transcribed Weather Broadcast.

U

UHF. See ultra-high frequency.

Ultra-high frequency (UHF). The range of electromagnetic

frequencies between 300 MHz and 3,000 MHz.

Ulitimate load factor. In stress analysis, the load that

causes physical breakdown in an aircraft or aircraft

component during a strength test, or the load that according

to computations, should cause such a breakdown.

Uncaging. Unlocking the gimbals of a gyroscopic instrument,

making it susceptible to damage by abrupt flight maneuvers

or rough handling.

Uncontrolled airspace. Class G airspace that has not been

designated as Class A, B, C, D, or E. It is airspace in which

air traffic control has no authority or responsibility to control

air traffic; however, pilots should remember there are VFR

minimums which apply to this airspace.

Underpower. Using less power than required for the purpose

of achieving a faster rate of airspeed change.

United States Terminal Procedures Publication (TPP).

Booklets published in regional format by FAA Aeronautical

Navigation Products (AeroNav Products) that include DPs,

STARs, IAPs, and other information pertinent to IFR flight.

Unusual attitude. An unintentional, unanticipated, or

extreme aircraft attitude.

Useful load. The weight of the pilot, copilot, passengers,

baggage, usable fuel, and drainable oil. It is the basic empty

weight subtracted from the maximum allowable gross weight.

This term applies to general aviation aircraft only.

User-defined waypoints. Waypoint location and other data

which may be input by the user, this is the only GPS database

information that may be altered (edited) by the user.

V

V1. See takeoff decision speed.

V2. See takeoff safety speed.

VA. See maneuvering speed.

Vapor lock. A problem that mostly affects gasoline-fuelled

internal combustion engines. It occurs when the liquid fuel

changes state from liquid to gas while still in the fuel delivery

system. This disrupts the operation of the fuel pump, causing

loss of feed pressure to the carburetor or fuel injection system,

resulting in transient loss of power or complete stalling.

Restarting the engine from this state may be difficult. The

fuel can vaporize due to being heated by the engine, by the

local climate or due to a lower boiling point at high altitude.

Variation. Compass error caused by the difference in

the physical locations of the magnetic north pole and the

geographic north pole.

VASI. See visual approach slope indicator.

VDP. See visual descent point.

Vector. A force vector is a graphic representation of a force

and shows both the magnitude and direction of the force.

Vectoring. Navigational guidance by assigning headings.

VEF. Calibrated airspeed at which the critical engine of a

multi-engine aircraft is assumed to fail.

G-33

Velocity. The speed or rate of movement in a certain

direction.

Venturi tube. A specially shaped tube attached to the outside

of an aircraft to produce suction to allow proper operation

of gyro instruments.

Vertical axis. An imaginary line passing vertically through

the center of gravity of an aircraft. The vertical axis is called

the z-axis or the yaw axis.

Vertical card compass. A magnetic compass that consists of

an azimuth on a vertical card, resembling a heading indicator

with a fixed miniature airplane to accurately present the

heading of the aircraft. The design uses eddy current damping

to minimize lead and lag during turns.

Vertical speed indicator (VSI). A rate-of-pressure change

instrument that gives an indication of any deviation from a

constant pressure level.

Vertical stability. Stability about an aircraft’s vertical axis.

Also called yawing or directional stability.

Very-high frequency (VHF). A band of radio frequencies

falling between 30 and 300 MHz.

Very-high frequency omnidirectional range (VOR).

Electronic navigation equipment in which the flight deck

instrument identifies the radial or line from the VOR station,

measured in degrees clockwise from magnetic north, along

which the aircraft is located.

Vestibule. The central cavity of the bony labyrinth of the

ear, or the parts of the membranous labyrinth that it contains.

VFE. The maximum speed with the flaps extended. The upper

limit of the white arc.

VFR. See visual flight rules.

VFR on top. ATC authorization for an IFR aircraft to operate

in VFR conditions at any appropriate VFR altitude.

VFR over the top. A VFR operation in which an aircraft

operates in VFR conditions on top of an undercast.

VFR terminal area chart. At a scale of 1:250,000, a chart

that depicts Class B airspace, which provides for the control

or segregation of all the aircraft within the Class B airspace.

The chart depicts topographic information and aeronautical

information including visual and radio aids to navigation,

airports, controlled airspace, restricted areas, obstructions,

and related data.

V-G diagram. A chart that relates velocity to load factor. It

is valid only for a specific weight, configuration and altitude

and shows the maximum amount of positive or negative lift

the airplane is capable of generating at a given speed. Also

shows the safe load factor limits and the load factor that the

aircraft can sustain at various speeds.

Victor airways. Airways based on a centerline that extends

from one VOR or VORTAC 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.

Visual approach slope indicator (VASI). A visual aid of

lights arranged to provide descent guidance information

during the approach to the runway. A pilot on the correct

glideslope will see red lights over white lights.

Visual descent point (VDP). A defined point on the final

approach course of a nonprecision straight-in approach

procedure from which normal descent from the MDA to the

runway touchdown point may be commenced, provided the

runway environment is clearly visible to the pilot.

Visual flight rules (VFR). Flight rules adopted by the

FAA governing aircraft flight using visual references. VFR

operations specify the amount of ceiling and the visibility the

pilot must have in order to operate according to these rules.

When the weather conditions are such that the pilot cannot

operate according to VFR, he or she must use instrument

flight rules (IFR).

Visual meteorological conditions (VMC). Meteorological

conditions expressed in terms of visibility, distance from

cloud, and ceiling meeting or exceeding the minimums

specified for VFR.

VLE. Landing gear extended speed. The maximum speed at

which an airplane can be safely flown with the landing gear

extended.

VLO. Landing gear operating speed. The maximum speed for

extending or retracting the landing gear if using an airplane

equipped with retractable landing gear.

VMC. Minimum control airspeed. This is the minimum

flight speed at which a light, twin-engine airplane can be

satisfactorily controlled when an engine suddenly becomes

inoperative and the remaining engine is at takeoff power.

VMC. See visual meteorological conditions.

G-34

VNE. The never-exceed speed. Operating above this speed is

prohibited since it may result in damage or structural failure.

The red line on the airspeed indicator.

VNO. The maximum structural cruising speed. Do not

exceed this speed except in smooth air. The upper limit of

the green arc.

VOR. See very-high frequency omnidirectional range.

VORTAC. A facility consisting of two components, VOR

and TACAN, which provides three individual services: VOR

azimuth, TACAN azimuth, and TACAN distance (DME)

at one site.

VOR test facility (VOT). A ground facility which emits a

test signal to check VOR receiver accuracy. Some VOTs are

available to the user while airborne, while others are limited

to ground use only.

VOT. See VOR test facility.

VSI. See vertical speed indicator.

VS0. The stalling speed or the minimum steady flight speed

in the landing configuration. In small airplanes, this is the

power-off stall speed at the maximum landing weight in the

landing configuration (gear and flaps down). The lower limit

of the white arc.

VS1. The stalling speed or the minimum steady flight speed

obtained in a specified configuration. For most airplanes, this

is the power-off stall speed at the maximum takeoff weight

in the clean configuration (gear up, if retractable, and flaps

up). The lower limit of the green arc.

V-tail. A design which utilizes two slanted tail surfaces to

perform the same functions as the surfaces of a conventional

elevator and rudder configuration. The fixed surfaces act as

both horizontal and vertical stabilizers.

VX. Best angle-of-climb speed. The airspeed at which an

airplane gains the greatest amount of altitude in a given

distance. It is used during a short-field takeoff to clear an

obstacle.

VY. Best rate-of-climb speed. This airspeed provides the

most altitude gain in a given period of time.

VYSE. Best rate-of-climb speed with one engine inoperative.

This airspeed provides the most altitude gain in a given

period of time in a light, twin-engine airplane following an

engine failure.

W

WAAS. See wide area augmentation system.

Wake turbulence. Wingtip vortices that are created when

an airplane generates lift. When an airplane generates lift,

air spills over the wingtips from the high pressure areas

below the wings to the low pressure areas above them. This

flow causes rapidly rotating whirlpools of air called wingtip

vortices or wake turbulence.

Warm front. The boundary area formed when a warm air

mass contacts and flows over a colder air mass. Warm fronts

cause low ceilings and rain.

Warning area. An area containing hazards to any aircraft

not participating in the activities being conducted in the

area. Warning areas may contain intensive military training,

gunnery exercises, or special weapons testing.

WARP. See weather and radar processing.

Waste gate. A controllable valve in the tailpipe of an aircraft

reciprocating engine equipped with a turbocharger. The valve

is controlled to vary the amount of exhaust gases forced

through the turbocharger turbine.

Waypoint. A designated geographical location used for route

definition or progress-reporting purposes and is defined in

terms of latitude/longitude coordinates.

WCA. See wind correction angle.

Weather and radar processor (WARP). A device that

provides real-time, accurate, predictive, and strategic weather

information presented in an integrated manner in the National

Airspace System (NAS).

Weather depiction chart. Details surface conditions as

derived from METAR and other surface observations.

Weight. The force exerted by an aircraft from the pull of

gravity.

Wide area augmentation system (WAAS). A differential

global positioning system (DGPS) that improves the accuracy

of the system by determining position error from the GPS

satellites, then transmitting the error, or corrective factors,

to the airborne GPS receiver.

Wind correction angle (WCA). The angle between the

desired track and the heading of the aircraft necessary to

keep the aircraft tracking over the desired track.

G-35

Wind direction indicators. Indicators that include a

wind sock, wind tee, or tetrahedron. Visual reference will

determine wind direction and runway in use.

Wind shear. A sudden, drastic shift in windspeed, direction,

or both that may occur in the horizontal or vertical plane.

Winds and temperature aloft forecast (FB). A twice daily

forecast that provides wind and temperature forecasts for

specific locations in the contiguous United States.

Wing area. The total surface of the wing (in square feet),

which includes control surfaces and may include wing area

covered by the fuselage (main body of the airplane), and

engine nacelles.

Wings. Airfoils attached to each side of the fuselage and are

the main lifting surfaces that support the airplane in flight.

Wing root. The wing root is the part of the wing on a fixed-

wing aircraft that is closest to the fuselage. Wing roots

usually bear the highest bending forces in flight and during

landing, and they often have fairings to reduce interference

drag between the wing and the fuselage. The opposite end

of a wing from the wing root is the wing tip.

Wing span. The maximum distance from wingtip to wingtip.

Wingtip vortices. The rapidly rotating air that spills over an

airplane’s wings during flight. The intensity of the turbulence

depends on the airplane’s weight, speed, and configuration.

Also referred to as wake turbulence. Vortices from heavy

aircraft may be extremely hazardous to small aircraft.

Wing twist. A design feature incorporated into some wings

to improve aileron control effectiveness at high angles of

attack during an approach to a stall.

Work. A measurement of force used to produce movement.

World Aeronautical Charts (WAC). A standard series

of aeronautical charts covering land areas of the world at a

size and scale convenient for navigation (1:1,000,000) by

moderate speed aircraft. Topographic information includes

cities and towns, principal roads, railroads, distinctive

landmarks, drainage, and relief. Aeronautical information

includes visual and radio aids to navigation, airports, airways,

restricted areas, obstructions and other pertinent data.

Z

Zone of confusion. Volume of space above the station where

a lack of adequate navigation signal directly above the VOR

station causes the needle to deviate.

Zulu time. A term used in aviation for coordinated universal

time (UTC) which places the entire world on one time standard.

G-36

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