InfoDotInc / archive systemEstablished online record · rebuilding deliberately
InfoDotInc

Technical documents, historic paths, and source-backed reference material.

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

Glossary, Part 3

Glossary — Part 3

FAA-H-8083-25C (2023)

G-16

Indirect indication. A reflection of aircraft pitch-and-bank

attitude by instruments other than the attitude indicator.

Induced drag. Drag caused by the same factors that produce

lift; its amount varies inversely with airspeed. As airspeed

decreases, the angle of attack must increase, in turn increasing

induced drag.

Induction icing. A type of ice in the induction system that

reduces the amount of air available for combustion. The most

commonly found induction icing is carburetor icing.

Inertial navigation system (INS). A computer-based

navigation system that tracks the movement of an aircraft

via signals produced by onboard accelerometers. The initial

location of the aircraft is entered into the computer, and all

subsequent movement of the aircraft is sensed and used to

keep the position updated. An INS does not require any inputs

from outside signals.

Initial approach fix (IAF). The fix depicted on IAP charts

where the instrument approach procedure (IAP) begins unless

otherwise authorized by ATC.

Inoperative components. Higher minimums are prescribed

when the specified visual aids are not functioning; this

information is listed in the Inoperative Components Table

found in the United States Terminal Procedures Publications.

INS. See inertial navigation system.

Instantaneous vertical speed indicator (IVSI). Assists in

interpretation by instantaneously indicating the rate of climb

or descent at a given moment with little or no lag as displayed

in a vertical speed indicator (VSI).

Instrument approach procedures (IAP). A series of

predetermined maneuvers for the orderly transfer of an

aircraft under IFR from the beginning of the initial approach

to a landing or to a point from which a landing may be

made visually.

Instrument flight rules (IFR). Rules and regulations

established by the Federal Aviation Administration to govern

flight under conditions in which flight by outside visual

reference is not safe. IFR flight depends upon flying by

reference to instruments in the flight deck, and navigation is

accomplished by reference to electronic signals.

Instrument landing system (ILS). An electronic system

that provides both horizontal and vertical guidance to a

specific runway, used to execute a precision instrument

approach procedure.

Instrument meteorological conditions (IMC).

Meteorological conditions expressed in terms of visibility,

distance from clouds, and ceiling less than the minimums

specified for visual meteorological conditions, requiring

operations to be conducted under IFR.

Instrument takeoff. Using the instruments rather than

outside visual cues to maintain runway heading and execute

a safe takeoff.

Intercooler. A device used to reduce the temperatures of the

compressed air before it enters the fuel metering device. The

resulting cooler air has a higher density, which permits the

engine to be operated with a higher power setting.

Interference drag. Drag generated by the collision of

airstreams creating eddy currents, turbulence, or restrictions

to smooth flow.

International Civil Aviation Organization (ICAO). The

United Nations agency for developing the principles and

techniques of international air navigation, and fostering

planning and development of international civil air transport.

International standard atmosphere (IAS). A model of

standard variation of pressure and temperature.

Interpolation. The estimation of an intermediate value

of a quantity that falls between marked values in a series.

Example: In a measurement of length, with a rule that is

marked in eighths of an inch, the value falls between 3/8

inch and 1/2 inch. The estimated (interpolated) value might

then be said to be 7/16 inch.

Inversion. An increase in temperature with altitude.

Inversion illusion. The feeling that the aircraft is tumbling

backwards, caused by an abrupt change from climb to straight-

and-level flight while in situations lacking visual reference.

Inverter. A solid-state electronic device that converts D.C.

into A.C. current of the proper voltage and frequency to

operate A.C. gyro instruments.

Isobars. Lines which connect points of equal barometric

pressure.

Isogonic lines. Lines drawn across aeronautical charts to

connect points having the same magnetic variation.

IVSI. See instantaneous vertical speed indicator.

G-17

J

Jet route. A route designated to serve flight operations from

18,000 feet MSL up to and including FL 450.

Jet stream. A high-velocity narrow stream of winds, usually

found near the upper limit of the troposphere, which flows

generally from west to east.

Judgment. The mental process of recognizing and analyzing

all pertinent information in a particular situation, a rational

evaluation of alternative actions in response to it, and a timely

decision on which action to take.

K

KIAS. Knots indicated airspeed.

Knot. The knot is a unit of speed equal to one nautical mile

(1.852 km) per hour, approximately 1.151 mph.

Kollsman window. A barometric scale window of a

sensitive altimeter used to adjust the altitude for the

altimeter setting.

L

LAAS. See local area augmentation system.

Lag. The delay that occurs before an instrument needle attains

a stable indication.

Land breeze. A coastal breeze flowing from land to sea

caused by temperature differences when the sea surface is

warmer than the adjacent land. The land breeze usually occurs

at night and alternates with the sea breeze that blows in the

opposite direction by day.

Land as soon as possible. Land without delay at the nearest

suitable area, such as an open field, at which a safe approach

and landing is assured.

Land as soon as practical. The landing site and duration of

flight are at the discretion of the pilot. Extended flight beyond

the nearest approved landing area is not recommended.

Land immediately. The urgency of the landing is paramount.

The primary consideration is to ensure the survival of the

occupants. Landing in trees, water, or other unsafe areas

should be considered only as a last resort.

Lateral axis. An imaginary line passing through the center

of gravity of an airplane and extending across the airplane

from wingtip to wingtip.

Lateral stability (rolling). The stability about the

longitudinal axis of an aircraft. Rolling stability or the ability

of an airplane to return to level flight due to a disturbance

that causes one of the wings to drop.

Latitude. Measurement north or south of the equator in

degrees, minutes, and seconds. Lines of latitude are also

referred to as parallels.

LDA. See localizer-type directional aid.

Lead radial. The radial at which the turn from the DME arc

to the inbound course is started.

Leading edge. The part of an airfoil that meets the airflow first.

Leading edge devices. High lift devices which are found

on the leading edge of the airfoil. The most common types

are fixed slots, movable slats, and leading edge flaps.

Leading-edge flap. A portion of the leading edge of an

airplane wing that folds downward to increase the camber,

lift, and drag of the wing. The leading-edge flaps are

extended for takeoffs and landings to increase the amount

of aerodynamic lift that is produced at any given airspeed.

Leans, the. A physical sensation caused by an abrupt correction

of a banked attitude entered too slowly to stimulate the motion

sensing system in the inner ear. The abrupt correction can

create the illusion of banking in the opposite direction.

Licensed empty weight. The empty weight that consists

of the airframe, engine(s), unusable fuel, and undrainable

oil plus standard and optional equipment as specified in the

equipment list. Some manufacturers used this term prior to

GAMA standardization.

Lift. A component of the total aerodynamic force on an airfoil

and acts perpendicular to the relative wind.

Limit load factor. Amount of stress, or load factor, that an

aircraft can withstand before structural damage or failure

occurs.

Lines of flux. Invisible lines of magnetic force passing

between the poles of a magnet.

L/MF. See low or medium frequency.

LMM. See locator middle marker.

G-18

Load factor. The ratio of a specified load to the total weight

of the aircraft. The specified load is expressed in terms of

any of the following: aerodynamic forces, inertial forces, or

ground or water reactions.

Loadmeter. A type of ammeter installed between the generator

output and the main bus in an aircraft electrical system.

LOC. See localizer.

Local area augmentation system (LAAS). 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.

Localizer (LOC). The portion of an ILS that gives left/right

guidance information down the centerline of the instrument

runway for final approach.

Localizer-type directional aid (LDA). A NAVAID used

for nonprecision instrument approaches with utility and

accuracy comparable to a localizer but which is not a part

of a complete ILS and is not aligned with the runway. Some

LDAs are equipped with a glideslope.

Locator middle marker (LMM). Nondirectional radio

beacon (NDB) compass locator, collocated with a middle

marker (MM).

Locator outer marker (LOM). NDB compass locator,

collocated with an outer marker (OM).

LOM. See locator outer marker.

Longitude. Measurement east or west of the Prime Meridian

in degrees, minutes, and seconds. The Prime Meridian is 0°

longitude and runs through Greenwich, England. Lines of

longitude are also referred to as meridians.

Longitudinal axis. An imaginary line through an aircraft

from nose to tail, passing through its center of gravity. The

longitudinal axis is also called the roll axis of the aircraft.

Movement of the ailerons rotates an airplane about its

longitudinal axis.

Longitudinal stability (pitching). Stability about the lateral

axis. A desirable characteristic of an airplane whereby it tends

to return to its trimmed angle of attack after displacement.

Low or medium frequency. A frequency range between

190 and 535 kHz with the medium frequency above 300

kHz. Generally associated with nondirectional beacons

transmitting a continuous carrier with either a 400 or 1,020

Hz modulation.

Lubber line. The reference line used in a magnetic compass

or heading indicator.

M

MAA. See maximum authorized altitude.

MAC. See mean aerodynamic chord.

Mach number. The ratio of the true airspeed of the aircraft

to the speed of sound in the same atmospheric conditions,

named in honor of Ernst Mach, late 19th century physicist.

Mach meter. The instrument that displays the ratio of the

speed of sound to the true airspeed an aircraft is flying.

Magnetic bearing (MB). The direction to or from a radio

transmitting station measured relative to magnetic north.

Magnetic compass. A device for determining direction

measured from magnetic north.

Magnetic dip. A vertical attraction between a compass

needle and the magnetic poles. The closer the aircraft is to a

pole, the more severe the effect.

Magnetic heading (MH). The direction an aircraft is pointed

with respect to magnetic north.

Magneto. A self-contained, engine-driven unit that supplies

electrical current to the spark plugs; completely independent

of the airplane’s electrical system. Normally there are two

magnetos per engine.

Magnus effect. Lifting force produced when a rotating

cylinder produces a pressure differential. This is the same

effect that makes a baseball curve or a golf ball slice.

Mandatory altitude. An altitude depicted on an instrument

approach chart with the altitude value both underscored and

overscored. Aircraft are required to maintain altitude at the

depicted value.

Mandatory block altitude. An altitude depicted on an

instrument approach chart with two underscored and

overscored altitude values between which aircraft are

required to maintain altitude.

G-19

Maneuverability. Ability of an aircraft to change directions

along a flight path and withstand the stresses imposed upon it.

Maneuvering speed (VA). The design maneuvering speed.

Operating at or below design maneuvering speed does not

provide structural protection against multiple full control

inputs in one axis or full control inputs in more than one

axis at the same time.

Manifold absolute pressure. The absolute pressure of the

fuel/air mixture within the intake manifold, usually indicated

in inches of mercury.

MAP. See missed approach point.

Margin identification. The top and bottom areas on an

instrument approach chart that depict information about

the procedure, including airport location and procedure

identification.

Marker beacon. A low-powered transmitter that directs its

signal upward in a small, fan-shaped pattern. Used along the

flight path when approaching an airport for landing, marker

beacons indicate both aurally and visually when the aircraft

is directly over the facility.

Mass. The amount of matter in a body.

Maximum altitude. An altitude depicted on an instrument

approach chart with overscored altitude value at which or

below aircraft are required to maintain altitude.

Maximum authorized altitude (MAA). A published altitude

representing the maximum usable altitude or flight level for

an airspace structure or route segment.

Maximum landing weight. The greatest weight that an

airplane normally is allowed to have at landing.

Maximum ramp weight. The total weight of a loaded aircraft,

including all fuel. It is greater than the takeoff weight due to the

fuel that will be burned during the taxi and runup operations.

Ramp weight may also be referred to as taxi weight.

Maximum takeoff weight. The maximum allowable weight

for takeoff.

Maximum weight. The maximum authorized weight of

the aircraft and all of its equipment as specified in the Type

Certificate Data Sheets (TCDS) for the aircraft.

Maximum zero fuel weight (GAMA). The maximum

weight, exclusive of usable fuel.

MB. See magnetic bearing.

MCA. See minimum crossing altitude.

MDA. See minimum descent altitude.

MEA. See minimum en route altitude.

Mean aerodynamic chord (MAC). The average distance

from the leading edge to the trailing edge of the wing.

Mean sea level. The average height of the surface of the

sea at a particular location for all stages of the tide over a

19-year period.

MEL. See minimum equipment list.

Meridians. Lines of longitude.

Mesophere. A layer of the atmosphere directly above the

stratosphere.

METAR. See Aviation Routine Weather Report.

MFD. See multi-function display.

MH. See magnetic heading.

MHz. Megahertz.

Microburts. A strong downdraft which normally occurs

over horizontal distances of 1 NM or less and vertical

distances of less than 1,000 feet. In spite of its small

horizontal scale, an intense microburst could induce

windspeeds greater than 100 knots and downdrafts as strong

as 6,000 feet per minute.

Microwave landing system (MLS). A precision instrument

approach system operating in the microwave spectrum which

normally consists of an azimuth station, elevation station,

and precision distance measuring equipment.

Mileage breakdown. A fix indicating a course change

that appears on the chart as an “x” at a break between two

segments of a federal airway.

Military operations area (MOA). Airspace established for

the purpose of separating certain military training activities

from IFR traffic.

G-20

Military training route (MTR). Airspace of defined vertical

and lateral dimensions established for the conduct of military

training at airspeeds in excess of 250 knots indicated airspeed

(KIAS).

Minimum altitude. An altitude depicted on an instrument

approach chart with the altitude value underscored. Aircraft

are required to maintain altitude at or above the depicted value.

Minimum crossing altitude (MCA). The lowest allowed

altitude at certain fixes an aircraft must cross when proceeding

in the direction of a higher minimum en route altitude (MEA).

Minimum descent altitude (MDA). The lowest altitude (in

feet MSL) to which descent is authorized on final approach,

or during circle-to-land maneuvering in execution of a

nonprecision approach.

Minimum drag. The point on the total drag curve where

the lift-to-drag ratio is the greatest. At this speed, total drag

is minimized.

Minimum en route altitude (MEA). The lowest published

altitude between radio fixes that ensures acceptable

navigational signal coverage and meets obstacle clearance

requirements between those fixes.

Minimum equipment list (MEL). A list developed for larger

aircraft that outlines equipment that can be inoperative for

various types of flight including IFR and icing conditions. This

list is based on the master minimum equipment list (MMEL)

developed by the FAA and must be approved by the FAA for

use. It is specific to an individual aircraft make and model.

Minimum obstruction clearance altitude (MOCA). The

lowest published altitude in effect between radio fixes on VOR

airways, off-airway routes, or route segments, which meets

obstacle clearance requirements for the entire route segment

and which ensures acceptable navigational signal coverage

only within 25 statute (22 nautical) miles of a VOR.

Minimum reception altitude (MRA). The lowest altitude

at which an airway intersection can be determined.

Minimum safe altitude (MSA). The minimum altitude

depicted on approach charts which provides at least 1,000 feet

of obstacle clearance for emergency use within a specified

distance from the listed navigation facility.

Minimum vectoring altitude (MVA). An IFR altitude lower

than the minimum en route altitude (MEA) that provides

terrain and obstacle clearance.

Minimums section. The area on an IAP chart that displays the

lowest altitude and visibility requirements for the approach.

Missed approach. A maneuver conducted by a pilot when

an instrument approach cannot be completed to a landing.

Missed approach point (MAP). A point prescribed in each

instrument approach at which a missed approach procedure

shall be executed if the required visual reference has not

been established.

Mixed ice. A mixture of clear ice and rime ice.

MLS. See microwave landing system.

MM. Middle marker.

MOA. See military operations area.

MOCA. See minimum obstruction clearance altitude.

Mode C. Altitude reporting transponder mode.

Moment. The product of the weight of an item multiplied

by its arm. Moments are expressed in pound-inches (lb-in).

Total moment is the weight of the airplane multiplied by the

distance between the datum and the CG.

Moment arm. The distance from a datum to the applied force.

Moment index (or index). A moment divided by a constant

such as 100, 1,000, or 10,000. The purpose of using a moment

index is to simplify weight and balance computations of

airplanes where heavy items and long arms result in large,

unmanageable numbers.

Monocoque. A shell-like fuselage design in which the

stressed outer skin is used to support the majority of imposed

stresses. Monocoque fuselage design may include bulkheads

but not stringers.

Monoplanes. Airplanes with a single set of wings.

Movable slat. A movable auxiliary airfoil on the leading edge

of a wing. It is closed in normal flight but extends at high

angles of attack. This allows air to continue flowing over the

top of the wing and delays airflow separation.

MRA. See minimum reception altitude.

MSA. See minimum safe altitude.

MSL. See mean sea level.

G-21

MTR. See military training route.

Multi-function display (MFD). Small screen (CRT or LCD)

in an aircraft that can be used to display information to the

pilot in numerous configurable ways. Often an MFD will be

used in concert with a primary flight display.

MVA. See minimum vectoring altitude.

N

N1. Rotational speed of the low pressure compressor in a

turbine engine.

N2. Rotational speed of the high pressure compressor in a

turbine engine.

Nacelle. A streamlined enclosure on an aircraft in which

an engine is mounted. On multiengine propeller-driven

airplanes, the nacelle is normally mounted on the leading

edge of the wing.

NACG. See National Aeronautical Charting Group.

NAS. See National Airspace System.

National Airspace System (NAS). The common network of

United States airspace—air navigation facilities, equipment

and services, airports or landing areas; aeronautical charts,

information and services; rules, regulations and procedures,

technical information; and manpower and material.

National Aeronautical Charting Group (NACG). A

Federal agency operating under the FAA, responsible for

publishing charts such as the terminal procedures and en

route charts.

National Route Program (NRP). A set of rules and

procedures designed to increase the flexibility of user flight

planning within published guidelines.

National Security Area (NSA). Areas consisting of airspace of

defined vertical and lateral dimensions established at locations

where there is a requirement for increased security and safety

of ground facilities. Pilots are requested to voluntarily avoid

flying through the depicted NSA. When it is necessary to

provide a greater level of security and safety, flight in NSAs

may be temporarily prohibited. Regulatory prohibitions are

disseminated via NOTAMs.

National Transportation Safety Board (NTSB). A United

States Government independent organization responsible for

investigations of accidents involving aviation, highways,

waterways, pipelines, and railroads in the United States.

NTSB is charged by congress to investigate every civil

aviation accident in the United States.

NAVAID. Navigational aid.

NAV/COM. Navigation and communication radio.

NDB. See nondirectional radio beacon.

Negative static stability. The initial tendency of an aircraft

to continue away from the original state of equilibrium after

being disturbed.

Neutral static stability. The initial tendency of an aircraft

to remain in a new condition after its equilibrium has been

disturbed.

NM. Nautical mile.

NOAA. National Oceanic and Atmospheric Administration.

No-gyro approach. A radar approach that may be used in

case of a malfunctioning gyro-compass or directional gyro.

Instead of providing the pilot with headings to be flown,

the controller observes the radar track and issues control

instructions “turn right/left” or “stop turn,” as appropriate.

Nondirectional radio beacon (NDB). A ground-based radio

transmitter that transmits radio energy in all directions.

Nonprecision approach. A standard instrument approach

procedure in which only horizontal guidance is provided.

No procedure turn (NoPT). Term used with the appropriate

course and altitude to denote that the procedure turn is not

required.

NoPT. See no procedure turn.

NOTAM. See Notice to Airmen.

Notice to Airmen (NOTAM). A notice filed with an aviation

authority to alert aircraft pilots of any hazards en route or at

a specific location. The authority in turn provides means of

disseminating relevant NOTAMs to pilots.

G-22

NRP. See National Route Program.

NSA. See National Security Area.

NTSB. See National Transportation Safety Board.

NWS. National Weather Service.

O

Obstacle departure procedures (ODP). A preplanned

instrument flight rule (IFR) departure procedure printed for

pilot use in textual or graphic form to provide obstruction

clearance via the least onerous route from the terminal area

to the appropriate en route structure. ODPs are recommended

for obstruction clearance and may be flown without ATC

clearance unless an alternate departure procedure (SID or

radar vector) has been specifically assigned by ATC.

Obstruction lights. Lights that can be found both on and off

an airport to identify obstructions.

Occluded front. A frontal occlusion occurs when a fast-

moving cold front catches up with a slow moving warm front.

The difference in temperature within each frontal system is

a major factor in determining whether a cold or warm front

occlusion occurs.

ODP. See obstacle departure procedures.

OM. Outer marker.

Omission error. The failure to anticipate significant

instrument indications following attitude changes; for

example, concentrating on pitch control while forgetting

about heading or roll information, resulting in erratic control

of heading and bank.

Optical illusion. A misleading visual image. For the

purpose of this handbook, the term refers to the brain’s

misinterpretation of features on the ground associated

with landing, which causes a pilot to misread the spatial

relationships between the aircraft and the runway.

Orientation. Awareness of the position of the aircraft and of

oneself in relation to a specific reference point.

Otolith organ. An inner ear organ that detects linear

acceleration and gravity orientation.

Outer marker. A marker beacon at or near the glideslope

intercept altitude of an ILS approach. It is normally located

four to seven miles from the runway threshold on the

extended centerline of the runway.

Outside air temperature (OAT). The measured or indicated

air temperature (IAT) corrected for compression and friction

heating. Also referred to as true air temperature.

Overcontrolling. Using more movement in the control

column than is necessary to achieve the desired pitch-and-

bank condition.

Overboost. A condition in which a reciprocating engine

has exceeded the maximum manifold pressure allowed by

the manufacturer. Can cause damage to engine components.

Overpower. To use more power than required for the purpose

of achieving a faster rate of airspeed change.

P

P-static. See precipitation static.

PAPI. See precision approach path indicator.

PAR. See precision approach radar.

Parallels. Lines of latitude.

Parasite drag. Drag caused by the friction of air moving

over the aircraft structure; its amount varies directly with

the airspeed.

Payload (GAMA). The weight of occupants, cargo, and

baggage.

Personality. The embodiment of personal traits and

characteristics of an individual that are set at a very early

age and extremely resistant to change.

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.

PFD. See primary flight display.

Phugoid oscillations. Long-period oscillations of an

aircraft around its lateral axis. It is a slow change in pitch

accompanied by equally slow changes in airspeed. Angle

of attack remains constant, and the pilot often corrects for

phugoid oscillations without even being aware of them.

PIC. See pilot in command.

Pilotage. Navigation by visual reference to landmarks.

Original source PDFPublished from pages 16–22 of the recorded source chapter.
Open source PDF ↗