Anti-Ice/Rain Flashcards
What are the components of the anti-ice and rain removal system?
Anti-Ice
–EAI
–WAI
–Window heat L1/R1 L2/R2
–Probe and sensor heat
Rain Removal
–Windshield wiper
–Hydrophobic coating on L1/R1
What external probes, vanes, ports, antennas are electrically heated?
CAPT, FO, STANDBY PITOT
L/R ELEVATOR FEEL PITOT
L/R ALPHA VANES
TAT PROBE
Heated in AUTO if either engine operating, or manually selected ON
Which flight deck windows are heated? When do ON/OVERHEAT illuminate/extinguish?
L1/R1 and L2/R2 are electrically heated
ON
-Power is supplied to window
-Extinguishes for
–Switch off
–System failure
–Window OVERHEAT (~62C)
–Window temp warm (~43C) (could be normal)
OVERHEAT
–Overheat for window (~62C), or
–Power interruption to window
–To reset, window must cool and re-cycle switch
What does the Engine Anti-Ice system protect? How does it operate?
Engine cowl lip heated with bleed air
–From respective engine bleed upstream of bleed air valve
Electrically controlled, pressure actuated
Operate in icing conditions
Adjusts stall warning logic (SMYD)
EECs set approach idle
What is the logic associated with the EAI switch ON?
Opens EAI valve allowing bleed air to heat cowl lip (irrespective of engine bleed air sw)
COWL VALVE OPEN (bright blue, then dim blue)
TAI (amber then green)
Adjusts stall warning logic (SMYD) while EAI switch on
EECs set approach idle
What does an amber COWL ANTI-ICE light indicate?
Excessive pressure in duct leading to cowl lip
(Normally 50 PSI max, caution >65 PSI)
What does a COWL VALVE OPEN light indicate? Dim/bright/extinguished?
EAI cowl valve position
Dim blue – valve open w/ switch ON
Bright blue – valve disagreement/in-transit
Extinguished – valve closed w/ switch OFF
What does an amber/green TAI above the N1 gauge indicate?
Amber TAI – cowl valve fails to move to commanded position
Green TAI – cowl valve open with switch ON
What does the Wing Anti-Ice system protect? How does it operate?
3 inboard leading edge slats heated by bleed air from respective duct downstream of bleed air valve, then exhausted overboard
WAI valve controlled by switch/AC motor
Adjusts stall warning logic for remainder of flight (SMYD)
Automatically close
–TLA advanced for takeoff, or
–Overheat on the ground
What is the logic associated with the WAI switch position to ON? OFF?
ON
-Valves open (except autoclose on ground due overheat/takeoff)
-Stall warning adjusted for remainder of flight
OFF
-Valves close
-Stall warning remains adjusted for rest of flight
How is WAI logic different on the ground vs in-flight?
In-Flight
-Stall warning adjusted for remainder of flight
-Overheat and TLA logic disabled
Ground
-Valves automatically close for overheat or TLA advanced for takeoff
What does L/R VALVE OPEN for WAI indicate? Bright/dim/extinguished?
Dim blue - valves open with switch on
Bright blue - valve disagreement or in-transit
Extinguished - valves closed with switch off
When is probe heat applied with switch in AUTO?
Either engine running
What do CAPT PITOT, L/R ELEV PITOT, L/R ALPHA VANE, TEMP PROBE, and AUX PITOT caution lights indicate?
Electrical power not provided to respective sensor
Illuminate with fault/failure or switch AUTO and engines OFF
Lights inhibited if operating on STANDBY POWER