Deice Flashcards
De-ice Master
When ON, with ENG ANTI-ICE , WINDSHIELD ANTI-ICE and BLADE DEICE POWER switches OFF, automatically turns these systems on when ice accumulation detected by sensor (if any individual systems already on, disables auto function and runs continuously)
OFF disables automatic function
Rotor Blade De-ice
Provides controlled electrical power to integral heating elements in the main and tail rotor blades allowing symmetrical ice shedding
Ice Detector
Senses ice accumulation on a vibrating probe by measuring change in probe frequency–triggers ICE DETECTED
Simultaneously, aspirator heater on the probe is turned on to heat the probe, shed the ice and reset it for another cycle
Severity of icing is proportional to rate at which the probe heater is cycled
MODE Selector AUTO Operation
OAT sensor provides signal to controller to govern heating EOT; the lower the OAT, the longer EOT will be
Ice-rate signal produces heating element off-time
Deice Cycles
Used to reduce power requirements (not on tail rotor, all at same time)
Droop Stop Heaters
Continuously heated as long as the BLADE DEICE control panel power switch is in the POWER ON or TEST position
MANUAL L, T, M Operation
Results in fixed off-time based on setting
Should be selected when an icing rate system malfunction is indicated by ICE DETECT FAIL or when there is no indication of failure, but any of these has occurred:
1. Pilot has determined by judgement of icing intensity that ice rate system is inaccurate
- Torque has increased to an unacceptable level
- Helo vibes increased to unacceptable level
Windshield Anti-ice
Each windshield has own system operated by switch on upper console
WARNING
A faulty windshield anti-ice system could result in arcing and delamination of the windshield. If not secured in a timely manner, an electrical fire could result
Pitot Heat
Shall be turned on when OAT <5*C or when visible moisture is present. Failure to turn on pitot heat in icing conditions may cause erroneous airspeed indications which can lead to erratic and/or downward programming of the stabilator and loss of control of the aircraft