Galling
Fretting or pulling out chunks of a surface by sliding contact with another surface or body.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
Taught in PP-L Procedures.
The curriculum
2,678 terms. Where the regulation defines a term (14 CFR 1.1 and 1.2, 280 of them), its definition is quoted word for word, and it governs. The FAA handbooks' definitions follow as guidance, each with the page of the handbook that prints it.
Fretting or pulling out chunks of a surface by sliding contact with another surface or body.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
Taught in PP-L Procedures.
General Aviation Manufacturers Association.
The basic gas turbine engine. It consists of the compressor, diffuser, combustor, and turbine. The gas generator is also called the core engine.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
An internal combustion engine that burns its fuel in a constant-pressure cycle and uses the expansion of the air to drive a turbine which, in turn, rotates a compressor. Energy beyond that needed to rotate the compressor is used to produce torque or thrust.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
Taught in PP-B Quick reference, PP-H Quick reference.
A seal between two parts where there is no relative motion.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
Taught in PP-H Hands-on, AF-J Procedures, PP-C Concepts, PP-G Procedures, PP-I Procedures.
The distance between rows of rivets in a multirow seam. Gauge is also called transverse pitch.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
Pressure referenced from the existing atmospheric pressure.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
Pressure referenced from existing atmospheric pressure.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
A constant-displacement fluid pump that contains two meshing large-tooth spur gears. Fluid is drawn into the pump as the teeth separate and is carried around the inside of the housing with teeth and is forced from the pump when the teeth come together.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
A term used to describe the total field of aviation operation except the military and airlines.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
While these documents are no longer published, they are still available at www.faa.gov. These are used to alert technicians of problems that have been found in specific models of aircraft, and reported on Malfunction and Defect Reports. Airworthiness Alerts suggest corrective action, but compliance with the suggestion is not mandatory.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
A mechanical device that transforms mechanical energy into electrical energy by rotating a coil inside a magnetic field. As the conductors in the coil cut across the lines of magnetic flux, a voltage is generated that causes current to flow.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
Taught in AF-K Quick reference, PP-F Quick reference, PP-F Concepts, PP-F Procedures, AF-G Concepts, AF-K Procedures and 4 more.
A set of heavy field windings in a generator connected in a series with the armature. The magnetic field produced by the series windings is used to change the characteristics of the generator.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
A set of field windings in a generator connected in parallel with the armature. Varying the amount of current flowing in the shunt field windings controls the voltage output of the generator.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
The distance a propeller would advance in one revolution if it were rotating in a solid.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
The point in the standard atmosphere where the temperature stops dropping and becomes constant. This is the tropopause, or the dividing line between the troposphere and the stratosphere.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
A form of constant-displacement gear pump. A gerotor pump uses an external-tooth spur gear that rides inside of and drives an internal-tooth rotor gear. There is one more tooth space inside the rotor than there are teeth on the drive gear. As the gears rotate, the volume of the space between two of the teeth on the inlet side of the pump increases, while the volume of the space between the two teeth on the opposite side of the pump decreases.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
A form of constant-displacement pump that uses an external-tooth drive gear that meshes with and drives an internal-tooth gear that has one more space for a tooth than there are teeth on the drive gear. Both gears turn inside a close-tolerance housing. As the gears rotate, fluid flows between the teeth that are beginning to un-mesh, and is carried around the pump as the space continues to open up. On the discharge side of the pump, the teeth becomes smaller, fluid is forced out of the pump.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
1,000,000,000 cycles per second.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
A support that allows a gyroscope to remain in an upright condition when its base is tilted.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
A type of support that allows an object, such as a gyroscope, to remain in an upright condition when its base is tilted.
An aircraft instrument system that uses a few cathode-ray-tube displays to replace a large number of mechanically actuated instruments.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
An aircraft instrument system that uses a few color cathode-ray-tube displays to replace a large number of mechanically actuated instruments.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
Ice that forms when large drops of water strike a surface whose temperature is below freezing. Glaze ice is clear and heavy.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
The portion of an ILS (Instrument Landing System) that provides the vertical path along which an aircraft descends on an instrument landing.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
Glider means a heavier-than-air aircraft, that is supported in flight by the dynamic reaction of the air against its lifting surfaces and whose free flight does not depend principally on an engine.
Part of the ILS that projects a radio beam upward at an angle of approximately 3° from the approach end of an instrument runway. The glideslope provides vertical guidance to aircraft on the final approach course for the aircraft to follow when making an ILS approach along the localizer path.
The minimum altitude of an intermediate approach segment prescribed for a precision approach that ensures obstacle clearance.
An instrument approach with lateral and vertical guidance with integrity limits (similar to barometric vertical navigation (BARO VNAV).
Satellite navigation system that provides autonomous geospatial positioning with global coverage. It allows small electronic receivers to determine their location (longitude, latitude, and altitude) to within a few meters using time signals transmitted along a line of sight by radio from satellites.
Navigation system that uses satellite rather than ground-based transmitters for location information.
Taught in AF-I Quick reference.
See global landing system.
See global navigation satellite system.
Go-around power or thrust setting means the maximum allowable in-flight power or thrust setting identified in the performance data.
Electronic circuitry in an ADF system that uses the output of a fixed loop antenna to sense the angle between a fixed reference, usually the nose of the aircraft, and the direction from which the radio signal is being received.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
As used in radio frequency (RF) antenna systems, a direction-sensing device consisting of two fixed loops of wire oriented 90° from each other, which separately sense received signal strength and send those signals to two rotors (also oriented 90°) in the sealed direction-indicating instrument. The rotors are attached to the direction-indicating needle of the instrument and rotated by a small motor until minimum magnetic field is sensed near the rotors.
A control used to automatically change the pitch of a constant speed propeller to maintain a constant engine rpm as air loads vary in flight.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
Taught in PP-M Quick reference, PP-M Concepts, PP-M Procedures.
See global positioning system.
Taught in AF-I Quick reference.
An authorization for pilots to use GPS avionics under IFR for flying designated existing nonprecision instrument approach procedures, with the exception of LOC, LDA, and SDF procedures.
Ground power unit. A service component used to supply electrical power and compressed air to an aircraft when it is operating on the ground.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
See ground proximity warning system.
Taught in AF-I Quick reference.
The basic unit of weight or mass in the metric system. One gram equals approximately 0.035 ounce.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
A form of carbon. Structural graphite is used in composite structure because of its strength and stiffness.
Aviation Maintenance Technician Handbook — Airframe, p. G-17
The illusion of the cessation of a turn while still in a prolonged, coordinated, constant rate turn, which can lead a disoriented pilot to a loss of control of the aircraft.
See weight.
Taught in GEN-H Concepts, GEN-C Quick reference, AF-O Concepts, AF-C Concepts, GEN-A Procedures, GEN-C Concepts and 1 more.
The shortest distance across the surface of a sphere (the Earth) between two points on the surface.
The unshrunk condition of a polyester fabric as it is removed from the loom.
Aviation Maintenance Technician Handbook — Airframe, p. G-18
The thrust produced by a turbojet or turbofan engine when the engine is static or not moving. The air is considered to have no inlet velocity, and the velocity of the gas leaving the engine is considered to be the acceleration factor.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
The sum of the basic empty weight and useful load.
The voltage reference point in an aircraft electrical system. Ground has zero electrical potential. Voltage values, both positive and negative, are measured from ground. In the United Kingdom, ground is spoken of as “earth.”
Aviation Maintenance Technician Handbook — Airframe, p. G-18
Used throughout the curriculum.
Non-movable metal trim tab on a control surface. Bent in one direction or another while on the ground to apply trim forces to the control surface.
An aircraft reciprocating engine with a built-in supercharger that boosts the sea-level rated horsepower of the engine.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
The increased aerodynamic lift produced when an airplane or helicopter is flown nearer than half wing span or rotor span to the ground. This additional lift is caused by an effective increase in angle of attack without the accompanying increase in induced drag, which is caused by the deflection of the downwashed air.
Aviation Maintenance Technician Handbook — Airframe, p. G-18
A usually beneficial influence on helicopter performance that occurs while flying close to the ground. It results from a reduction in upwash, downwash, and bladetip vortices, which provide a corresponding decrease in induced drag.
The condition of slightly increased air pressure below an airplane wing or helicopter rotor system that increases the amount of lift produced. It exists within approximately one wing span or one rotor diameter from the ground. It results from a reduction in upwash, downwash, and wingtip vortices, and provides a corresponding decrease in induced drag.
A service component used to supply electrical power to an aircraft when it is being operated on the ground.
Aviation Maintenance Technician Handbook — Airframe, p. G-18
A system designed to determine an aircraft’s clearance above the Earth and provides limited predictability about aircraft position relative to rising terrain.
Taught in AF-I Quick reference.
Selfexcited vibration occurring whenever the frequency of oscillation of the blades about the lead-lag axis of an articulated rotor becomes the same as the natural frequency of the fuselage.
Ground visibility means prevailing horizontal visibility near the earth's surface as reported by the United States National Weather Service or an accredited observer.
Speed over the ground, either closing speed to the station or waypoint, or speed over the ground in whatever direction the aircraft is going at the moment, depending upon the navigation system used.
GS means glide slope.
See glideslope.
Guidance: Pilot's Handbook of Aeronautical Knowledge, p. G-14
The British name for a wrist pin, or piston pin. See wrist pin.
Aviation Maintenance Technician Handbook — Powerplant, p. G-13
A highly explosive material made by treating cotton fibers with nitric and sulfuric acids. Guncotton is used in making the film base of nitrate dope.
Aviation Maintenance Technician Handbook — Airframe, p. G-18
A small plate attached to two or more members of a truss structure. A gusset strengthens the truss.
Aviation Maintenance Technician Handbook — Airframe, p. G-18
See ground proximity warning system.
The sensing device in an autopilot system. A gyroscope is a rapidly spinning wheel with its weight concentrated around its rim. Gyroscopes have two basic characteristics that make them useful in aircraft instruments: rigidity in space and precession. See rigidity in space and precession.
Aviation Maintenance Technician Handbook — Airframe, p. G-18
Gyrodyne means a rotorcraft whose rotors are normally engine-driven for takeoff, hovering, and landing, and for forward flight through part of its speed range, and whose means of propulsion, consisting usually of conventional propellers, is independent of the rotor system.
Gyroplane means 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, consisting usually of conventional propellers, is independent of the rotor system.
Taught in AF-N Quick reference.
The characteristic of a gyroscope that causes it to react to an applied force as though the force were applied at a point 90° in the direction of rotation from the actual point of application. The rotor of a helicopter acts in much the same way as a gyroscope and is affected by gyroscopic precession.
Aviation Maintenance Technician Handbook — Airframe, p. G-18
An inherent quality of rotating bodies, which causes an applied force to be manifested 90° in the direction of rotation from the point where the force is applied.
An inherent quality of rotating bodies, which causes an applied force to be manifested 90° in the direction of rotation from the point where the force is applied.
The glossary is CC BY-SA 4.0 as an arrangement; the quoted regulation text is a work of the US Government. Handbook definitions are quoted from the FAA's handbooks, each linked to the FAA's own copy.