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De/Anti-Icing Terminology

Horizontales
A procedure by which fluid is applied to provide protection against the formation of frost or ice or the accumulation of snow or slush on treated surfaces of an aircraft for a limited period of time. (Hyphenated)
Airfoils that are set in the wing trailing edge.
Small probes attached to the trailing edge of the wings, vertical stabilizers and horizontal stabilizers that are designed to dissipate static electrical charge from the aircraft. (2 Words)
A control surface that is attached to the trailing edge of the vertical stabilizer and controls the yaw of the aircraft.
__________ Time is the estimated time for which an anti-icing fluid will prevent the formation of frost or ice and the accumulation of snow on the treated surfaces of an aircraft.
_______ Tubes are pressure measurement instruments used to determine aircraft airspeed during flight.
The _______ Edge is the part which first meets the oncoming air.
The body of the aircraft, designed to accommodate the crew, passengers and cargo.
When conditions exist during ground operations that are conducive to aircraft icing, no person shall conduct or attempt to conduct a take-off in an aircraft that has frost, ice or snow adhering to any of its critical surfaces. (3 words)
Pilot responsible for the operation and safety of an aircraft. (Abbreviation)
Provides electrical and pneumatic power to the aircraft and assists in starting engines. (Abbreviation)
Wingtip _________ increase the efficiency of the wing by increasing lift and reducing drag.
Landing ______ is the structure that absorbs the shock of landing, supports the aircraft on the ground and allows the aircraft to maneuver.
_________ Surfaces can be readily and clearly observed by flight crew during day and night operations, and which are suitable for judging whether critical surfaces are contaminated.
Examination of an aircraft surface against a relevant standard by a trained and qualified person.
The window system in the front of the flight deck.
Verticales
Airfoils that are set in the wing leading edge.
This "effect" is when the wings contain very cold fuel as a result of the aircraft having just landed after a flight at high altitude or from having been refueled with very cold fuel. (2 Words)
The lowest temperature at which a de/anti-icing fluid can be applied to an aircraft. (Abbreviation)
All forms of frozen or semi-frozen deposits on an aircraft, such as frost, snow, slush or ice. Failed aircraft ground de/anti-icing fluid is also considered contamination.
The procedure by which frost, ice, slush or snow is removed from an aircraft in order to provide clean surfaces and components.
Movable control surfaces on the trailing edge of the horizontal stabilizer that control the pitch of the aircraft.
Total Air ________ Probes are mounted on the side of the aircraft near the flight deck that read temperature.
Any surface that affects an aircraft’s ability to fly. (2 Words)
__________ Stabilizers are airfoils located near the rear of the aircraft that provides longitudinal stability.
The _________ Stabilizer is located on the top of the rear portion of the fuselage and provides aircraft lateral stability.
Plates on the top surface of the wing that can be extended upward into the airflow.
A structural enclosure located on the nose of the aircraft that protects the aircraft’s radar system.
The _________ Edge is the rear edge of the surface where the airflow separated by the leading edge rejoins.
A __________ Check is a touch or hands-on inspection to determine the presence of clear ice and other contaminants that are hard to detect.
Ground Icing _________ exist when frost, ice, or snow is adhering or may adhere to the critical surfaces of an aircraft.
The propulsion system for aircraft. (Plural)
Movable surfaces on the trailing edge of the wing near the wing tip that control the roll of the aircraft.
Deicing ________ are ice protection systems installed on leading edge surfaces of certain aircraft that inflate to deice the covered surface.
Angle of _________ Sensors measure the angle between the chord line of the wing and the relative wind.
Primary lifting surface of the aircraft.