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.