Ice & Rain Flashcards
What are the ATA Code’s
30 Ice & Rain
— 00 General
— 10 Airfoils
— 20 Air Intakes
— 30 Pitot & Static
— 38 Water and Waste
— 40 Windows & Windshields
— 50 Antenna & Radomes
— 60 Propellers/Rotors
— 70 Water Lines
— 80 Detections
What must all aircraft that operate in weather conditions where ice is likely to form have?
They MUST have ice protection
Ice increases ______ and reduces ______.
Drag & Lift
Ice hampers instrument readings and causes ________
Vibrations
Anti-Icing Systems prevents the ________ of ice
Formation
Anti-Ice systems are operated in flight when icing conditions are present or _________
When expected.
Deicing Systems ______ ice on the aircraft
Removes
How does the De-icing system work?
It allows the ice to accumulate and then break off
Visual inspection is done by flight _____ monitoring
Crew
(Visually seeing ice on surface)
Deicer Boots are coated with _______ to dissipate static.
Neoprene
Air ________ are on the back side
Connections
De-Ice boots are driven by a ______________
Vacuum Pump
________________ controls the inflation sequence by directing the vacuum
Distributor Valve.
Boots are inflated alternately to minimize _________________
Airflow Disruption
A __________________ holds the boots deflated when the system is off, by regulating the vacuum.
Suction relief valve.
With wet type vacuum pumps, an _____________ is used to protect the boots from oil deterioration by removing the oil from the air.
Oil Separator
(Inspecting & Maintaining Deicer Boots)
What does Deicer boots installation require?
Removing all paint from the area to be covered by the Deicer boot. Check for cuts, abrasion, or other damage.
Remove any _______ or _____ with soap and water
Grease or Oil
Check _________ __________ for removal procedures
Maintenance manual
(Wing Anti-Ice WAI system Thermal Anti-Icing)
Uses heated air flowing _____ ______ ______ passages in the wing, or electric resistance heat elements in a “blanket”.
And what kind of system is it?
Through
Anti-ice system
Heat sources for pneumatic systems are combustion heaters, ____ _____ or _______ tubes.
Bleed air or augmenter
Wing leading edges, or leading-edge slats, and horizontal and vertical stabilizer leading edges, and some _______ and _____ ______ _____ are heated with a Thermal electric boot system.
Turbine and turbo prop inlets
(Electro thermal Propeller)
Many propellers are Deiced by an _________ heated boot on each side.
Electrically
The boot, firmly cemented in place, receives current from a ________ and _______ assembly on the spinner bulkhead
Slip ring and Brush
(Propellers Fluid Anti-Icing)
10 PSI variable output controlled by a _______
Rheostat
Flow rate ranges from less than ______ to more that _______per hour
1 quart
1 Gallon