10. Ice And Rain Protection Flashcards
What is the minimum OAT to operate deice boots?
-40 deg C
What is the time cycle for SINGLE deice boot inflation?
6 seconds wings, then 4 seconds tail
What does the MANUAL position for deice boot inflation do?
Inflates all boots simultaneously for as long as the switch is held
Does loss of an engine affect deice boot operation?
No. The loss of one engine’s pneumatic pressure will not affect boot operation.
There is a check valve in the bleed line from each engine to prevent pressure loss
Is electrical power required for operation of boot system?
Yes, but with electrical power loss, the vacuum will hold them tightly against leading edge
How can it be confirmed that brake deice valves are opening or closing correctly?
By observing a slight increase or decrease in ITT (about 20deg C) when BRAKE DEICE is cycled.
During ground operation, simultaneous use of brake deice and wing boots can cause red BLEED AIR FAIL. Why is this?
The substantial drop is pneumatic pressure can cause it to flash momentarily, though light should
What is the minimum power on each engine to maintain proper boot inflation if brake heating is on?
85%
Which system is the single biggest use of engine bleed air, and can cause rudder boost to be inoperative in an engine failure?
Brake deice
What heat is the windshield normally heated to?
95-105deg F
What is the difference between normal and high windshield heating?
Normal supplies heat to the broadest area. High supplies a higher intensity of heat to a smaller but more essential viewing area
Can windshield heat be used anytime?
Yes. It is protected from overheating by thermal sensors.
It also causes erratic compass indications and possibly distorted visual cues
What is the AUTO prop heat sequence on later models approx BB-900 onwards?
90 seconds entire right prop, 90 seconds entire left prop, cycling continuously
What does MANUAL prop heat do?
Spring loaded switch supplies current to both props at once. PROP AMPS ammeter does not register flow on manual, however it can be observed on loadmeters
How is stall warning heat affected by left landing gear squat switch?
Current flow to heater is minimal while on the ground and full in flight