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DA42 Anti-ice system
anti-ice system operation and limitations
6
Aviation
Professional
05/19/2014

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Cards

Term
Describe the components of the anti-ice system.
Definition
TKS weeping wing system certificated for known icing, except greater than moderate or freezing rain.

7.9 gallon (72 lbs) reservoir (located in nose baggage compartment.

2 main pumps that feed fluid to the wings, horizontal stabilizer, and vertical stabilizer.

Deice lights for each wing.

Control panel in cockpit.

Spreads a thin film of fluid over the wings, windshield, horizontal and vertical stabilizer and propellers.
Term
Describe the normal mode.
Definition
Switch placed in normal position
Both pumps run for 30 second on, 90 seconds off.
Maximum duration - 2.5 hours
Term
Describe the high mode.
Definition
One pump runs continuously.
Used when ice has accumulated.
Maximum duration - 1 hour
Term
Describe max mode.
Definition
Both pumps run continuously for 2 minutes each time the MAX button is pushed.

Maximum duration - 30 minutes
Term
Describe canopy anti-icing.
Definition
Pushing the windshield button will spray the canopy for 5 seconds.
Term
Describe Alternate mode.
Definition
The LH bus normally powers the anti-ice system. In the event the LH bus fails, activating the ALTERNATE switch connects the system to the RH bus, however only #2 pump will function and only in HIGH mode.
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