The measureable height of an aircraft above the actual terrain.

Mechanical and electrical units mounted on an engine necessary for its operation, such as starter, magnetos, fuel pumps, etc.

Automatic Direction Finding via automated radio.

Attitude indicator

The rate at which ascending air cools and descending air warms, given no heat is added or taken away. The rate for dry air is based on 5.4° F per 1000' altitude (1° per 100 meters); saturated rates vary with barometric pressures and temperatures, and must be adjusted for accuracy.

Yaw generated when the ailerons are used. The lifting wing generates more drag, causing an airplane to yaw toward it.

Attitude Heading and Reference System

The movable areas of a wingform that control or affect the roll of an aircraft by working opposite one another — up-aileron on the right wing and down-aileron on the left wing. French: aileron small wing, diminutive of aile, from Latin: ala, wing. The word "aisle" also derives from the same root.

The area of airspace over land or water, extending upward from the surface, within which the ready identification, the location, and the control of aircraft are required in the interest of national security. Domestic Air Defense Identification Zone - An ADIZ within the United States along an international boundary of the United States. Coastal Air Defense Identification Zone - An ADIZ over the coastal waters of the United States. Distant Early Warning Identification Zone (DEWIZ) - An ADIZ over the coastal waters of the State of Alaska. ADIZ locations and operating and flight plan requirements for civil aircraft operations are specified in FAR Part 99.

A facility established to provide air traffic control service to aircraft operating on IFR flight plans within controlled airspace and principally during the en route phase of flight. When equipment capabilities and controller workload permit, certain advisory/assistance services may be provided to VFR aircraft.

An instrument or device that measures the air speed of an aircraft through an air mass.

An aircraft operator who conducts operations for hire or compensation in accordance with FAR Part 135 in an aircraft with 30 or fewer passenger seats and a payload capacity of 7,500# or less. An air taxi operates on an on demand basis and does not meet the "flight scheduled" qualifications of a commuter

A service operated by the appropriate authority to promote the safe, orderly, and expeditious flow of air traffic.

A terminal facility that uses air/ground communications, visual signaling, and other devices to provide ATC services to aircraft operating in the vicinity of an airport or on the movement area. Authorizes aircraft to land or takeoff at the airport controlled by the tower or to transit the Class D airspace area regardless of flight plan or weather conditions (IFR or VFR). A tower may also provide approach control services (radar or non-radar).

Trademark name of Alcoa for high-strength sheet aluminum clad with a layer (approximately 5.5% thickness per side) of high-purity aluminum, popularly used in airplane manufacture.

Devised for reasons of clarity in aviation voice radio, this is the current NATO version in global use: ALFA BRAVO CHARLEY DELTA ECHO FOXTROT GOLF HOTEL INDIA JULIET KILO LIMA MIKE NOVEMBER OSCAR PAPA QUEBEC ROMEO SIERRA TANGO UNIFORM VICTOR WHISKY X-RAY YANKEE ZULU The original, from early in World War 2, was: ABLE BAKER CHARLEY DOG EASY FOX GEORGE HOW ITEM JIG KING LOVE MIKE NAN OBOE PETER QUEEN ROGER SUGAR TARE UNCLE VICTOR WILLIAM X-RAY YOKE ZEBRA

An adjustable aneroid-barometic cockpit instrument used to measure an aircraft's altitude.

A SEAPLANE or FLOATPLANE with retractable wheels for use on land, as well. The latter spelling was used in the '20s and '30s but has since fallen out of favor.

The acute angle at which a moving airfoil meets the airstream.

The angle at which an airfoil is normally fixed in relation to the longitudinal axis of an aircraft.

The downward angle of a wing in relation to a horizontal cross-section line; aka CATHEDRAL. SEE DIHEDRAL.

Short for autopilot

The hard-surfaced or paved area around a hangar.

SEE CONTROLLED AIRSPACE

A vacuum-powered panel instrument that displays pitch and roll movements about the lateral and longitudinal axes; aka Attitude Indicator.

The ratio of the span to the chord of an airfoil — a high-aspect ratio wing has wide span and narrow chord, and vice-versa.

SEE CONTROLLED AIRSPACE

SEE AUTOMATIC TERMINAL INFORMATION SERVICE

Automatic rotation of rotary blades from a helicopter in an unpowered glide or the forward movement of an autogyro.

An aircraft, often wingless, with unpowered rotary airfoil blades that auto-rotate and serve as wings as it moves through the air when driven by an engine

Continuous broadcast of recorded noncontrol information in selected terminal areas, to improve controller effectiveness and to relieve frequency congestion by automating repetitive transmissions of essential but routine information.

A movable control surface, as an aileron or rudder, having an added physical extension or weights forward of the hinge-point to reduce forces on a joystick or yoke.

Since the pressure of a fluid is proportional to its velocity, airflow over the upper surface of an airfoil causes suction [lift] because the airstream has been speeded up in relation to positive pressure of the airflow on the lower surface.

Hot air at high pressure, usually from the bypass section of a gas turbine engine, for de-icing, heating, and other uses.

The design or control of slotted or perforated wings with suction methods to reduce undesirable aerodynamic effects caused by the boundary layer, that region adjacent to the boundary where shear stresses dominate in the airflow over a wingform.

An engine fairing, generally circular, with welts or compound shapes in its surface to accommodate cylinder heads.

Wing strut attached to the fuselage.

The indicated airspeed of an aircraft, corrected for position and instrument error. CAS is equal to true airspeed in standard atmosphere at sea level. Compare INDICATED AIRSPEED and TRUE AIRSPEED.

The convex or concave curvature of an airfoil.

An arrangement in which the horizontal stabilizer and elevators of an aircraft are mounted in front of the main wing(s).

Clear-Air Turbulence.

Ceiling and Visibility Unlimited; ideal flying weather.

1) The heights above the earth's surface of the lowest layer of clouds or obscuring phenomena that is reported as "broken," "overcast," or "obscuration," and not classified as "thin" or "partial". (2) The maximum height above sea level in Standard Air attainable by an aircraft under given conditions — SEE ABSOLUTE CEILING, SERVICE CEILING.

An Air Route Traffic Control Center (ARTCC).

The longitudinal and lateral point in an aircraft where it is stable; the static balance point.

An airport operating under FAR Part 139. The FAA issues airport operating certificates to all airports serving scheduled or unscheduled air carrier aircraft designed for more than 30 passenger seats. Certificated airports must meet minimum safety standards in accordance with FAR Part 139.

The measurable distance between the leading and trailing edges of a wingform.

Airspace not designated as Class A, B, C, D or E.

A cockpit control that changes the pitch of a helicopter's rotor blades; used in climbing or descending.

A circular duct on a radial engine into which exhaust gases from its cylinders are discharged.

A frequency designed for the purpose of carrying out airport advisory practices while operating to or from an airport without an operating control tower. The CTAF may be a UNICOM, Multicom, FSS, or tower frequency and is identified in appropriate aeronautical publications.

An air carrier operator operating under 14 CFR 135 that carries passengers on at least five round trips per week on at least one route between two or more points according to its published flight schedules that specify the times, day of the week, and places between which these flights are performed. The aircraft that a commuter operates has 30 or fewer passenger seats and a payload capability of 7,500# or less.

A bearing as indicated by the horizontal angle between the compass needle and the centerline of the aircraft. A Compass Course is equal to a True Course ± variation and deviation; also equal to a Magnetic Course ± deviation.

The North point at which a liquid compass needle points, rather than Geographical, or True, North. Compare MAGNETIC NORTH.

SEE RADIO NAVIGATION

A hydraulically-controlled propeller that governs an engine at its optimum speed by the blade pitch being increased or decreased automatically.

Streaks of condensed water vapor created in the air by aircraft flying at high altitudes; aka Vapor Trails.

An airspace of defined dimensions within which air traffic control service is provided to IFR flights and to VFR flights in accordance with the airspace classification. Controlled airspace is a generic term that covers Class A, B, C, D, and E airspace. Controlled airspace is also that airspace within which all aircraft operators are subject to certain pilot qualifications, operating rules, and equipment requirements in FAR Part 91. For IFR operations in any class of controlled airspace, a pilot must file an IFR flight plan and receive an appropriate ATC clearance. Each B, C, and D airspace area designated for an airport contains at least one primary airport around which the airspace is designated (for specific designations and descriptions of the airspace classes, refer to FAR Part 71. Class A (formerly PCA - Positive Control Area) generally, that airspace from 18,000' mean sea level (MSL) up to and including flight level (FL) 600 (60,000' pressure altitude), including the airspace overlying the waters within 12 nautical miles of the coast of the 48 contiguous States and Alaska. Unless otherwise authorized, all persons must operate their aircraft under IFR. Class B (formerly TCA - Terminal Control Area) Generally, that airspace from the surface to 10,000' MSL surrounding the nation's busiest airports in terms of airport operations or passenger enplanements. The configuration of each Class B airspace area is individually tailored and consists of a surface area and two or more layers (some Class B airspace areas resemble upside-down wedding cakes), and is designed to contain all published instrument procedures once an aircraft enters the airspace. An ATC clearance is required for all aircraft to operate in the area, and all aircraft that are so cleared receive separation services within the airspace. The cloud clearance requirement for VFR operations is "clear of clouds." Class C (formerly ARSA - Airport Radar Service Area) Generally, that airspace from the surface to 4,000' MSL above the airport elevation surrounding those airports that have an operational control tower, are serviced by a radar approach control, and that have a certain number of IFR operations or passenger enplanements. Although the configuration of each Class C area is individually tailored, the airspace usually consists of a surface area with a 5 nautical mile (nm) radius, an outer circle with a 10 nm radius that extends from 1,200' to 4,000' above the airport elevation and an outer area. Each person must establish two-way radio communications with the ATC facility providing air traffic services prior to entering the airspace and thereafter maintain those communications while within the airspace. VFR aircraft are only separated from IFR aircraft within the airspace. Class D (formerly ATA - Airport Traffic Area and CZ - Control Zone) Generally, that airspace from the surface to 2,500' MSL above the airport elevation 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 will normally be designed to contain the procedures. Arrival extensions for instrument approach procedures may be Class D or E airspace. Unless otherwise authorized, each person must establish two-way radio communications with the ATC facility providing air traffic services prior to entering the airspace and thereafter maintain those communications while in the airspace. No separation services are provided to VFR aircraft. Class E (formerly General Controlled Airspace) Generally, if the airspace is not Class A, B, C, or D, and is controlled airspace, it is Class E airspace. Class E airspace extends upward from either the surface or a designated altitude to the overlying or adjacent controlled airspace. When designated as a surface area, the airspace will be configured to contain all instrument procedures. Also in this class are Federal airways, airspace beginning at either 700' or 1,200' AGL used to transition to/from the terminal or enroute environment, enroute domestic, and offshore airspace areas designated below 18,000' MSL. Unless designated at a lower altitude, Class E airspace begins at 14,500' MSL over the USA, including that airspace overlying the waters within 12 nautical miles of the coast of the 48 contiguous States and Alaska, up to, but not including 18,000' MSL, and the airspace above Flight Level 600.

Having two main landing wheels at the front and a tailwheel or tailskid at the rear as opposed to having a tricycle gear with three main wheels. Such an aircraft is popularly called a TAILDRAGGER.

A controllable louvre to regulating airflow through an engine's cowling.

A circular, removable fairing around an aircraft engine (generally radial) for the purposes of streamling or cooling; aka RING COWLING.

A rudder-controlled yawing motion to compensate for a crosswind in maintaining a desired flight path, as in a landing approach.

SEE COMMON TRAFFIC ADVISORY FREQUENCY

Descending flight with engine and propeller stopped.

The difference in angular settings [Angles of Attack] of the wings of a biplane or multiplane.

With respect to the operation of aircraft, the height at which point a decision must be made during an instrument approach to either continue the approach or to execute a missed approach [abort].

A triangularly-shaped aircraft wing having a low aspect ratio, a sharply-tapered leading edge, a straight trailing edge, and a pointed tip.

SEE RADIO NAVIGATION

A stall in the takeoff configuration with power.

The error of a Magnetic Compass due to inherent magnetic influences in the structure and equipment of an aircraft.

SEE AIR DEFENSE IDENTIFICATION ZONE

The acute angle, usually upward, between the wing of an airplane and a horizontal cross-section line. Opposite of ANHEDRAL.

A panel instrument providing a gyroscopic reading of an aircraft's compass heading.

Distance Measuring Equipment, a radio navigation device that determines an aircraft's distance from a given ground station, as well as its groundspeed and time to/from the station.

A lateral fin/rudder extension on the top of a fuselage.

The air deflected perpendicular to the direction of movement of an airfoil.

The resisting force exerted on an aircraft in its line of flight opposite in direction to its motion. Compare THRUST.

A wire designed to resist drag forces, usually running from a forward inboard point to an outboard aft point.

The angle between the heading of an aircraft and its Track, or flight path, over the ground as affected by winds.

The weight of an engine exclusive of any fuel, oil, and coolant.

Originally a tradename for a wrought aluminum-copper alloy created by Bausch Machine Tool Co, now fallen into generic use as any aluminum alloy containing 3.0-4.5% copper, 0.4-1.0% magnesium, and 0.1-0.7% manganese. Alcoa's version is commonly referred to as "Duraluminum," popularly used in aircaft manufacture.

One whose indications depend on the current generated in a coil revolving in the earth's magnetic field.

The movable part of a horizontal airfoil which controls the pitch of an aircraft; the fixed part being the STABILIZER.

A hinged device on the rear portion of an aircraft wing combining the functions of an elevator and an aileron. Usually found on delta-wing aircraft, it can be moved in the same direction on either side of the aircraft to obtain longitudinal control, or differentially to obtain lateral control. Also see FLAPERON.

Emergency Locator Transmitter

An aircraft's tail group, includes rudder and fin, and stabilizer and elevator. Old French: empenner,to feather an arrow, from Latin penna, feather. Other words derived from the same root are panache, pen, pin, pinnacle, and pennant.

Air traffic control services provided aircraft on IFR flight plans, generally by centers, when these aircraft are operating between departure and destination terminal areas. When equipment, capabilities, and controller workload permit, certain advisory/assistance services may be provided to VFR aircraft.

Estimated Time of Arrival.

Estimated Time of Departure.

An added streamlining structure or auxiliary member, most often of light metal, whose only purpose is to reduce drag. Fairings are not load-bearing and, therefore, are not meant to carry any principal air loads placed on the airplane structure.

SEE RADIO NAVIGATION

Fixed-Base Operator, a commercial operator supplying fuel, maintenance, flight training, and other services at an airport.

In the event of engine failure, the process of adjusting a controllable-pitch propeller to a pitch position where the blade angle is about 90° to the plane of rotation in order to stop windmilling.

FAR Part 91 - General Aviation (portions apply to all operators) FAR Part 103 - Ultralight Vehicles FAR Part 105 - Parachute Jumping FAR Part 108 - Airplane Operator Security FAR Part 119 - Certification: Air Carriers and Commercial Operators FAR Part 121 - Domestic, Flag, and Supplemental Air Carriers and Commercial Operators of Large Aircraft FAR Part 123 - Travel Clubs FAR Part 125 - US Civil Airplanes, seating 20 or more passengers or a maximum payload capacity 6,000# or more FAR Part 127 - Air Carriers using helicopters for scheduled interstate flights (within the 48 contiguous states) FAR Part 129 - Foreign Air Carrier and Foreign Operators of US registered aircraft engaged in common carriage FAR Part 133 - Rotorcraft External Load Operations FAR Part 135 - Air Taxi Operators and Commercial Operators FAR Part 137 - Agricultural Aircraft Operations FAR Part 141 - Pilot School

A flight for the purpose of (1) returning an aircraft to base; (2) delivering an aircraft from one location to another; (3) moving an aircraft to and from a maintenance base. Ferry flights, under certain conditions, may be conducted under terms of a special flight permit.

The fixed part of a vertical airfoil that controls the yaw of an aircraft; the movable part being the RUDDER. Sometime referred to as Vertical Stabilizer.

A fire-resistant bulkhead that isolates the engine from other parts of an airplane's structure.

A rudder-controlled side-to-side [yawing] motion to reduce air speed, generally prior to landing.

In radio jargon, affirms that a radioed transmission was received clear and loud. Rated one to five, with the first figure for clearness and the second second for loudness.

A movable, usually hinged airfoil set in the trailing edge of an aircraft wing, designed to increase lift or drag by changing the camber of the wing or used to slow an aircraft during landing by increasing lift. Also see FOWLER FLAP, SLOTTED FLAP, and SPLIT FLAP.

A control surface combining the functions of a flap and an aileron.

A maneuver performed moments before landing in which the nose of an aircraft is pitched up to minimize the touchdown rate of speed.

An aircraft's performance limits, specifically the curves of speed plotted against other variables to indicate the limits of speed, altitude, and acceleration that a particular aircraft can not safely exceed.

A level of constant atmospheric pressure related to a reference datum of 29.92 inches of mercury. Each is stated in three digits that represent hundreds of feet — flight level 250 represents a barometric altimeter indication of 25,000'; flight level 255 an indication of 25,500'.

Specified information relating to the intended flight of an aircraft that is filed orally or in writing with an FSS or an ATC facility.

Air traffic facilities which provide pilot briefing, enroute communications and VFR search and rescue services, assist lost aircraft and aircraft in emergency situations, relay ATC clearances, originate Notices to Airmen, broadcast aviation weather and NAS information, receive and process IFR flight plans, and monitor NAVAIDs. In addition, at selected locations, FSSs provide Enroute Flight Advisory Service (Flight Watch), take weather observations, issue airport advisories, and advise Customs and Immigration of transborder flights.

A water-based aircraft with one or more mounted pontoons, as differentiated from a hulled SEAPLANE or Flying Boat, but sometimes used generically.

Interplane bracing wires that help support wingloads when the plane is in flight. Direction of travel is upward and outward from the fuselage to the interplane struts. Also known as LIFT WIRES, the opposite of LANDING WIRES.

Trademark name of a split-flap attached to a wing through a system of tracks and rollers to roll the flap backward and downward, increasing the wing area.

A type of aileron that has a beveled leading edge projecting beyond its inset hinges. When lowered, it forms an extension of the wing surface; when raised, its nose protrudes below the wing, increasing drag and reducing yaw. Named for its inventor, British engineer Leslie George Frise.

SEE FLIGHT SERVICE STATION

An aircraft's main body structure housing the flight crew, passengers, and cargo and to which the wings, tail and, in most single-engined airplanes, engine are attached. French: fuselé,tapering.

SEE LOAD FACTOR

The distance between two adjacent wings of a biplane or multiplane.

Ground-Controlled Approach; part of ILS.

That portion of civil aviation which encompasses all facets of aviation except air carriers holding a certificate of public convenience and necessity from the Civil Aeronautics Board and large aircraft commercial operators.

The northern axis around which the Earth revolves; aka "Map North." Also see MAGNETIC NORTH, TRUE NORTH.

Said of an aircraft's control cabin which has all-electronic, digital and computer-based, instrumentation.

(1) The angle between horizontal and the glide path of an aircraft. (2) A tightly-focused radio beam transmitted from the approach end of a runway indicating the minimum approach angle that will clear all obstacles; one component of an instrument landing system (ILS).

An unpowered aircraft capable of maintaining altitude only briefly after release from tow, then gliding to earth. Compare SAILPLANE.

Global Positioning System; satellite-based navigation.

Approval for landing. A carryover expression from days when aircraft for the most part had no radios, and communication from a control tower was by means of a light-gun that beamed various green, red, and yellow signals to pilots in the air and on the ground.

The total weight of an aircraft when fully loaded; aka Takeoff Weight.

Tower control, by radioed instructions from air traffic control, of aircraft ground movements at an airport.

Increased lift generated by the interaction between a lift system and the ground when an aircraft is within a wingspan distance above the ground. It affects a low-winged aircraft more than a mid- or high-winged aircraft because its wings are closer to the ground; aka GROUND CUSHION.

The actual speed that an aircraft travels over the ground — its "shadow speed"; it combines the craft's airspeed and the wind speed relative to the aircraft's direction of flight.

Descriptive of wing in frontal view bent as the wing of a seagull; a distinctive shallow, inverted "V" shape — see Stinson SR-7 or inverted gull-wing Vought F4U.

A rotorcraft whose rotors are not engine-driven, except for initial starting, but are made to rotate by action of the air when the rotorcraft is moving and whose means of propulsion, usually a conventional propeller, is independent of the rotor system. Similar to AUTOGYRO.

An enclosed structure for housing aircraft. Originated with the floating homes of the original German Zeppelins in which they were "hung" from cables, which explains the erroneous, oft-seen spelling of "hanger." French: shed, outbuilding, from Latin: angarium,shed.

A wingless aircraft acquiring its lift from revolving blades driven by an engine about a near-vertical axis. A ROTORCRAFT acquiring its primary motion from engine-driven rotors that accelerate the air downward, providing a reactive lift force, or accelerate the air at an angle to the vertical, providing lift and thrust.

A blower-type supercharger set at high rpm

Any stall made to occur at more than 1g, such as pulling out of a dive or while turning.

The motive energy required to raise 550# one foot in one second, friction disregarded.

Speed of flight at or greater than Mach 5.0.

Indicated airspeed

Instrument Flight Rules, governing the conduct of flight under instrument meteorological conditions.

Instrument Landing System. A radar-based system allowing ILS-equipped aircraft to find a runway and land when clouds may be as low as 200 feet (or lower for special circumstances).

A direct instrument reading obtained from an airspeed indicator uncorrected for altitude, temperature, atmospheric density, or instrument error. Compare CALIBRATED AIRSPEED and TRUE AIRSPEED.

Meteorological conditions expressed in terms of visibility, distance from clouds, and ceiling less than minima specified for visual meteorological conditions (VMC).

Railroad tracks, as favored by pilots of yore as a dependable aid to surface navigation.

A single floor- or roof-mounted control stick — sideways movement produces roll, and forward/backward movement produces pitch (rudder pedals produce yaw).

One nautical mile per hour, about 1.15 statute miles (6,080') per hour.

A low-drag airfoil designed to maintain laminar flow over a high percentage of the chord about itself. Often relatively thin, especially along the leading edge, with most of its bulk near the center of the chord.

Interplane bracing wires that help support wingloads when the plane is on the ground. Direction of travel is downward and outward from the fuselage. Opposite of FLYING WIRES.

The force exerted on the top of a moving airfoil as a low-pressure area that causes a wingform to rise.

Interplane bracing wires that help support wingloads when the plane is in flight. Direction of travel is upward from the bottom of the fuselage to the top of the interplane struts. Also known as LIFT WIRES, the opposite of LANDING WIRES.

The lift of a wing divided by the drag, or the lift coefficient divided by the drag coefficient, as the primary measure of the efficiency of an aircraft; aka L/D Ratio.

A non-electronic, calibratable compass floating in a liquid as a panel instrument; aka Wet Compass.

The proportion between lift and weight commonly seen as g (sometimes capitalized) — a unit of force equal to the force of gravity times one.

Design or fabrication of a complex aircraft component, as with sheet metal, using actual-size patterns or plans, generally laid out on a floor. The term is borrowed from boat builders.

A principal longitudinal member of a fuselage's framing, usually continuous across a number of supporting points.

A circular radio antenna, either in the open or in a streamlined, teardrop housing, remotely turned 360° to fine-tune a station in league with other radio-directive devices. See also RADIO COMPASS, RADIO DIRECTION FINDER

Long Range Navigation system, which utilizes timing differences between multiple low-frequency transmissions to provide accurate latitude/longitude position information to within 50'.

Lighter-than-air craft, generally referring to powered blimps and dirigibles, but often also includes free balloons.

A manual fuel drain placed handily along a fuel line for checking avgas, such as for water or sediment.

A number representing the ratio of the speed of an object to the speed of sound in the surrounding air or medium in which it is moving.

The most common liquid-type compass, capable of calibration to compensate for magnetic influences within the aircraft.

COMPASS COURSE ± deviation

The magnetic North pole, located near 71° North latitude and 96° West longitude, that attracts a magnetic compass which is not influenced by local magnetic attraction, as opposed to GEOGRAPHIC NORTH.

An accessory that produces and distributes a high-voltage electric current for ignition of a fuel charge in an internal combustion engine.

The effect on a spinning cylinder or sphere moving through a fluid, in which force acts perpendicular to the direction of motion and to the direction of spin. This is used to advantage in baseball, in which the trajectory of a pitched ball is a distinct curve. Applied to aeronautics in experimental wingforms, the Magnus Theory states that if air is directed against a smooth, revolving cylinder, whose circumferential speed is greater than that of the air current, a force is directed against one side of the cylinder — air compressed on one side and vacuum formed on the other — creating lift. Named after physicist Heinrich Gustav Magnus (1802-70).

SEE RADIO NAVIGATION

SEE MSL

SEE SPECIAL USE AIRSPACE

Type of fuselage design with little or no internal bracing other than bulkheads, where the outer skin bears the main stresses; usually round or oval in cross-section. Additional classifications are (1) Semi-Monocoque, where the skin is reinforced by longerons or bulkheads, but with no diagonal web members, and (2) Reinforced Shell, in which the skin is supported by a complete framework or structural members. French: monocoque,single shell.

Mean Sea Level. The average height of the surface of the sea for all stages of tide; used as a reference for elevations, and differentiated from AGL.

A streamlined enclosure or housing to protect something such as the crew, engine, or landing gear. French: nacelle,from Latin, navicella,little ship.

The common network of US airspace; air navigation facilities, equipment and services, airports or landing areas; aeronautical charts, information and services; rules, regulations and procedures, technical information, and human resources and material. Included are system components shared jointly with the military.

An L/MF or UHF radio beacon transmitting nondirectional signals whereby the pilot of an aircraft equipped with direction finding equipment can determine his bearing to or from the radio beacon and "home" on or track to or from the station. When the radio beacon is installed in conjuncion with the Instrument Landing System (ILS) marker, it is normally called a Compass Locator.

A popular word for streamlined, non-load bearing fairings to cover landing wheels. Also sometimes called Spats or, when fully enclosing the wheel struts, Skirts.

A popular word for streamlined, non-load bearing fairings to cover landing wheels. Also sometimes called Spats or, when fully enclosing the wheel struts, Skirts.

Precision Approach Radar, a ground-radar-based instrument approach providing both horizontal and vertical guidance

The path of aircraft traffic around an airfield, at an established height and direction. At tower-controlled fields the pattern is supervised by radio (or, in non-radio or emergency conditions by red and green light beams) by air traffic controllers.

Anything that an aircraft carries beyond what is required for its operation during flight, theoretically that from which revenue is derived, such as cargo and passengers.

SEE ALPHABET

The pilot responsible for the operation and safety of an aircraft during flight time.

(1) Of the three axes in flight, this specifies the vertical action, the up-and-down movement. Compare ROLL and YAW. (2) The angle of a propeller or rotor blade in relation to its arc; also the distance advanced by a blade in one full rotation.

More accurately but less popularly used, Pitot-Static Tube, a small tube most often mounted on the outward leading edge of an airplane wing (out of the propeller stream) that measures the impact pressure of the air it meets in flight, working in conjuction with a closed, perforated, coaxial tube that measures the static pressure. The difference in pressures is calibrated as airspeed by a panel instrument. Named after French scientist Henri Pitot (1695-1771).

The separation of all air traffic within designated airspace by air traffic control.

The Gross Weight of an airplane divided by the rated horsepower, computed for Standard Air density.

A propeller mounted in back of its engine, pushing an aircraft through the air, as opposed to a TRACTOR configuration.

A terminal ATC facility that uses radar and non-radar capabilities to provide approach control services to aircraft arriving, departing, or transiting airspace controlled by the facility. This facility provides radar ATC services to aircraft operating in the vicinity of one or more civil/military airports in a terminal area. The facility may provide services of a ground-controlled approach (GCA). A radar approach control facility may be operated by FAA or a military service, or jointly. Specific facility nomenclatures are used for administrative purposes only and are related to the physical location of the facility and the operating service generally: Army Radar Approach Control (ARAC) (Army) Radar Air Traffic Control Facility (RATCF) (Navy/FAA) Radar Approach Control (RAPCON) (Air Force/FAA) Terminal Radar Approach Control (TRACON) (FAA) Tower/Airport Traffic Control Tower (ATCT) (FAA ‚ only towers delegated approach control authority)

SEE RADIO NAVIGATION

An aerodynamic duct in which fuel is burned to produce a high-velocity propulsive jet. It needs to be accelerated to high speed before it can become operative.

A circular engine fairing.

A flexible, delta-wing plan in which three rigid members are shaped in the form of an arrowhead and joined by a flexible fabric, which inflates upward under flight loads. Originally specific to paragliders, but now found on some powered aircraft.

Of the three axes in flight, this specifies the action around a central point. Compare PITCH and YAW.

A powerplant that rotates on a stationary propeller shaft. An American invention by Adams-Farwell Co (1896), it was first used for buses and trucks in the US (1903), then copied by French engineers for early aircraft engines (1914).

A heavier-than-air aircraft that depends principally for its support in flight on the lift generated by one or more rotors. Includes helicopters and gyroplanes.

The movable part of a vertical airfoil which controls the yaw of an aircraft; the fixed part being the FIN.

An unpowered, soaring aircraft capable of maintaining level flight for long periods of time after release from tow and of gaining altitude using wind currents, as opposed to a GLIDER.

An unpowered, soaring aircraft capable of maintaining level flight for long periods of time after release from tow and of gaining altitude using wind currents, as opposed to a GLIDER.

A low, foglike cloud layer.

A water-based aircraft with a boat-hull fuselage, often amphibious.The term is also used generically to define a similar Flying Boat and a pontoon FLOATPLANE.

Any stall resulting from pulling back too soon and too hard while recovering from any other stall. Usually a HIGH-SPEED or ACCELERATED STALL.

The height above sea level at which an aircraft with normal rated load is unable to climb faster than 100' per minute under Standard Air conditions.

A mid-wing monoplane with its wing mounted directly to the top of the fuselage without use of cabane struts.

A mid-wing monoplane with its wing mounted directly to the top of the fuselage without use of cabane struts.

A movement of an aircraft in which a relative flow of air moves along the lateral axis, resulting in a sideways movement from a projected flight path, especially a downward slip toward the inside of a banked turn.

Too shallow a bank in a turn, causing an aircraft to slide outward from its ideal turing path.

Movable vanes or auxiliary airfoils, usually set along the leading edge of a wing but able to be lifted away at certain angles of attack.

Too steep a bank in a turn, causing an aircraft to slide inward from its ideal turing path.

The flow of air driven backward by a propeller or downward by a rotor.

A long, narrow, spanwise gap in a wing, usually near the leading edge, to improve airflow at high angles of attack for slower landing speeds.

A flap that, when depressed, exposes a slot and increases airflow between itself and the rear edge of the wing.

"Since Major Overhaul," an acronym seen in reference to the operating hours, or time remaining, on an engine.

Airspace of defined dimensions identified by an area on the surface of the earth wherein activities must be confined because of their nature and/or wherein limitations may be imposed upon aircraft operations that are not a part of those activities: Alert Area - Airspace which may contain a high volume of pilot training activities or an unusual type of aerial activity, neither of which is hazardous to aircraft. Alert Areas are depicted on aeronautical charts for the information of non-participating pilots. All activities within an Alert Area are conducted in accordance with Federal Aviation Regulations, and pilots of participating aircraft as well as pilots transiting the area are equally responsible for collision avoidance. Military Operations Area (MOA) - Airspace established outside of Class A airspace area to separate or segregate certain non-hazardous military activities from IFR traffic and to identify for VFR traffic where these activities are conducted. Prohibited Area - Airspace designated under part 73 within which no person may operate an aircraft without the permission of the using agency. Restricted Area - Airspace designated under FAR Part 73, within which the flight of aircraft, while not wholly prohibited, is subject to restriction. Most restricted areas are designated joint use and IFR/VFR operations in the area may be authorized by the controlling ATC facility when it is not being utilized by the using agency. Restricted areas are depicted on enroute charts. Where joint use is authorized, the name of the ATC controlling facility is also shown. Warning Area - A warning area is airspace of defined dimensions extending from 3 nautical miles outward from the coast of the USA, that contains activity that may be hazardous to non-participating aircraft. The purpose of such warning area is to warn non-participating pilots of the potential danger. A warning area may be located over domestic or international waters or both.

A flap built into the underside of a wing, as opposed to a Full Flap wherein a whole portion of the trailing edge is used.

A long, movable, narrow plate along the upper surface of an airplane wing used to reduce lift and increase drag by breaking or spoiling the smoothness of the airflow.

A short, winglike protuberance on each side of a seaplane to increase lateral stability.

A four-digit number which is dialed into his transponder by a pilot to identify his aircraft to air traffic controllers

A movable horizontal tail that combines the actions of a stabilizer and elevator, increasing longitudinal stability while creating a pitching moment.

The fixed part of a horizontal airfoil that controls the pitch of an aircraft; the movable part being the ELEVATOR.

The relative longitudinal position of the wings on a biplane. Positive Stagger is when the upper wing's leading edge is in advance of that of the lower wing [eg: Waco YKS], and vice versa for Negative Stagger [eg: Beechcraft D17].

(1) Sudden loss of lift when the angle of attack increases to a point where the flow of air breaks away from a wing or airfoil, causing it to drop. (2) A maneuver initiated by the steep raising of an aircraft's nose, resulting in a loss of velocity and an abrupt drop.

An arbitrary atmosphere established for calibration of aircraft instruments. Standard Air Density is 29.92 inches of mercury and temperature of 59° F, equivalent to an atmospheric air pressure of 14.7# per square inch.

A turn in which the heading of an aircraft changes 3° per second, or 360° in two minutes.

A clip-on wire used to ground an aircraft by drawing off static electricity, a potential fire hazard, during refueling.

SEE SPECIAL USE AIRSPACE

Speed of flight at or greater than Mach 1.0; literally, faster than the speed of sound.

A backward inclination of an airfoil from root to tip in a way that causes the leading edge and often the trailing edge to meet relative wind obliquely, as wingforms that are swept back.

A wing whose horizontal angle to the fuselage centerline can be adjusted in flight to vary aircraft motion at differing speeds.

SEE CONVENTIONAL GEAR

(1) A bituminous material used in paving; a trade name for Tar MacAdam. (2) An airport surface paved with this substance, especially a runway or an APRON at a hangar.

True airspeed

True Airspeed. Because an airspeed indicator indicates true airspeed only under standard sea-level conditions, true airspeed is usually calculated by adjusting an Indicated Airspeed according to temperature, density, and pressure. Compare CALIBRATED AIR SPEED and INDICATED AIR SPEED.

SEE CONTROLLED AIRSPACE

Airspace surrounding designated airports wherein ATC provides radar vectoring, sequencing, and separation on a full-time basis for all IFR and participating VFR aircraft. Service provided at a TRSA is called Stage III Service. TRSAs are depicted on VFR aeronautical charts. Pilot participation is urged but is not mandatory.

Ground-based, free-rotating, triangular-shaped wind direction indicator, genrally placed near a runway.

The driving force of a propeller in the line of its shaft or the forward force produced in reaction to the gases expelled rearward from a jet or rocket engine. Opposite of DRAG.

A twisting, gyroscopic force acting in opposition to an axis of rotation, such as with a turning propeller; aka Torsion.

Landing practice wherein an aircraft does not make a full stop after a landing, but proceeds immediately to another take-off.

A propeller mounted in front of its engine, pulling an aircraft through the air, as opposed to a PUSHER configuration.

An airborne transmitter that responds to ground-based interrogation signals to provide air traffic controllers with more accurate and reliable position information than would be possible with "passive" radar; may also provide air traffic control with an aircraft's altitude.

A small, auxiliary control surface in the trailing edge of a wingform, adjustable mechanically or by hand, to counteract ("trim") aerodynamic forces on the main control surfaces.

The speed of an aircraft along its flight path, in respect to the body of air (air mass) through which the aircraft is moving. Also see CALIBRATED AIRSPEED, GROUND SPEED, INDICATED AIRSPEED.

The northern direction of the axis of the Earth; aka "Map North." GEOGRAPHICAL NORTH, as opposed to MAGNETIC NORTH.

An aircraft having a jet engine in which the energy of the jet operates a turbine that in turn operates the air compressor.

An aircraft having a jet engine in which the energy of the jet operates a turbine that drives the propeller.

An aeronautical vehicle operated for sport or recreational purposes which does not require FAA registration, an airworthiness certificate, nor pilot certification. Primarily single-occupant vehicles, although some two-place vehicles are authorized for training purposes. Operation of an ultralight vehicle in certain airspaces requires authorization from ATC.

Class G Airspace; airspace not designated as Class A, B, C, D or E.

The landing gear of a land-based aircraft, including struts, frames, and wheels.

To land short of a runwway or planned landing spot. Opposite is OVERSHOOT.

A common radio frequency (usually 121.0 mHz) used at uncontrolled (non-tower) airports for local pilot communication.

The slight, upward flow of air just prior to its reaching the leading edge of a rapidly moving airfoil.

Long a point of contest among pilots, there is in reality no such thing as far as the airplane is concerned. Proponents claim that airplanes lose airspeed when turning upwind, while opponents (and the laws of physics) argue that an airplane, like a boat in a river whose speed is only relative to the shore, is unaffected within the movement of an air mass and that it loses only groundspeed.

The weight of crew, passengers, fuel, baggage, and ballast, generally excluding emergency or portable equipment and ordnance.

Velocity, now used in defining airspeeds: VA = Maneuvering Speed (max structural speed for full control deflection) VD = Max Dive Speed (for certification only) VFE = Max Flaps Extended Speed VLE = Max Landing Gear Extended Speed VLO = Max Landing Gear Operation Speed VNE = Never Exceed Speed VNO = Max Structural Cruising Speed VS0 = Stalling Speed Landing Configuration VS1 = Stalling Speed in a specified Configuration VX = Best Angle of Climb Speed VXSE = Best Angle of Climb Speed, one engine out VY = Best Rate of Climb Speed VYSE = Best Rate of Climb Speed, one engine out

A panel instrument, often as simple as a tiny ball in a vertical tube, indicating subtle pitch movements of an aircraft.

A fin/rudder extension on the bottom of a fuselage. Opposite of DORSAL FIN.

A small, hourglass-shaped metal tube, usually set laterally on a fuselage in the slipstream to create suction for gyroscopic panel instruments. Now outdated by more sophisticated means.

Visual Flight Rules that govern the procedures for conducting flight under visual conditions. The term is also used in the US to indicate weather conditions that are equal to or greater than minimum VFR requirements. Also used by pilots and controllers to indicate a type of flight plan.

Flight in which a cloud ceiling exists but modified VISUAL FLIGHT RULES are in effect if the aircraft travels above the cloud layer.

Meteorological conditions expressed in terms of visibility, distance from clouds, and ceiling equal to or better than specified minima.

VHF Omnirange. A ground-based navigation aid transmitting very high frequency (VHF) navigation signals 360° in azimuth, on radials oriented from magnetic north. The VOR periodically identifies itself by Morse Code and may have an additional voice identification feature. Voice features can be used by ATC or FSS for transmitting information to pilots.

VOR + TACAN (Tactical Air Navigation); combined radio navigation aids.

Vertical Speed Indicator. A panel instrument that gauges rate of climb or descent in feet-per-minute (fpm). Also Rate Of Climb Indicator.

A method of increasing lift by increasing (Wash-In) or decreasing (Wash-Out) the angle of incidence on the outer part of an airplane wing to counteract the effects of engine torque.

SEE COMPASS

The maximum take-off (Gross) weight of an aircraft divided by its wing area.

A small, stabilizing, rudderlike addition to the tips of a wing to control or employ air movement.

Of the three axes in flight, this specifies the side-to-side movement of an aircraft on its vertical axis, as in skewing. Compare PITCH and ROLL.

The control wheel of an aircraft, akin to a automobile steering wheel.