Ice & Rain Protection Flashcards
What is the correct position of the cabin window heat switch prior to takeoff?
Selected IN (legend indicating OFF)
If the wing and/or cowl anti-ice system is automatically activated during descent, at what point will it turn off automatically?
When the WoW system shifts to ground mode
How are the total air temperature (TAT) probes properly checked prior to flight?
Check for proper aspirated airflow at the aft end of the probe after APU air is selected ON
When should the cowl anti-ice system be manually turned on?
Temp < +10C and visible moisture present
If engine vibration increases while flying in icing conditions, what is the corrective action?
Decrease engine power to idle for 5 sec, then accelerate the engine to 85% LP RPM for 2 sec
When is automatic activation of the cowl and wing anti-ice systems inhibited?
Below 1500’ AGL on takeoff, and above FL350
When should continuous airstart ignition be selected ON?
Contaminated runway, heavy rain
When does the anti-ice system automatically turn OFF?
L-R ice detect message after 60 sec
Cowl anti-ice after 3 minutes
Wing anti-ice after 5 minutes
What is the power source of the windshield heat?
LF/RS - L MAIN AC BUS
RF/LS - R MAIN AC BUS
At what temperature does the windshield heat cycle?
Automatically ON at 104F
Automatically OFF at 114F
What does it mean if the WINDSHIELD HEAT annunciator lights begin blinking at 1 cycle per second for 90 sec followed by an amber WSHLD FAIL CAS?
- Over-temp conditions exist
- Both heat sensors have failed
- Over-current or no current detected with switch selected ON
- Current detected with switch selected OFF
What does it mean if the WINDSHIELD HEAT annunciation lights begin blinking at 3 cycles per second for 90 sec followed by a blue “L/R (F) or (S) WSHLD FAULT” CAS?
- Single windshield sensor failure
- Windshield heating film exceeds acceptable range of operation
Which anti-ice probes use bleed air on the ground?
TAT Probes
Which probes are powered during HMG operations?
AOA1 - L ESS DC
AOA2 - R ESS DC
L upper / R lower pitot - L/R STBY AC
R upper / L lower pitot - ESS AC BUS Phase A
TAT1 - L STBY AC
TAT2 - R STBY AC
Since the COWL and WING ANTI-ICE systems operates in the AUTO mode between 1500’ AGL and FL350, what must be done in icing conditions below 1500’ AGL on an approach?
Nothing, it will remain ON in the AUTO mode until WoW