The anti/deicing systems on the Caravan I airplanes use: A) Electric power. B) Bleed air. C) Hydraulic power. D) Both A and B. .
Each segment of the wing surface deice boot inflation cycle lasts for approximately: A) 3 seconds. B) 6 seconds. C) 9 seconds D) 12 seconds. .
The windshield, propeller, and pilot-static anti-ice systems are intended to be used: A) After entering icing conditions. B) To prevent ice accumulation. C) To remove ice from their respective surfaces. D) Only in freezing rain conditions. .
The wing, wing strut, and stabilizer deice boots are intended to be used: A) To prevent ice accumulation. B) Continuously. C) During flight in instrument conditions. D) After ¼ to 3/8 inch of clear ice or ½ to ¾ inch of rime has accumulated. .
When the BOOST PRESS switch is moved to the AUTO position: A) One three-segment deice cycle is initiated. B) All deice boots inflate simultaneously.
C) The deice boots inflate automatically every 30 seconds. D) The deice boots inflate automatically every 18 seconds. .
When the BOOTS PRESS switch is moved to the MANUAL position: A) One three-segment deice cycle is initiated. B) Only the wing leading edge boots inflate. C) All deice boots inflate simultaneously. D) None of the above. .
The windshield anti-ice panel can be used: A) To remove ice from the windshield prior to starting. B) Instead of using the deicing boots. C) To prevent ice from forming on the windshield. D) Both A and B.
The standby electrical system: Is powered by a belt-driven alternator. Has the same capacity as the main electrical system. Can be used only for starting the engine. Is used to power the deice/anti-ice system only.
The ice detector light is used: A) At all times during flight in icing conditions. B) Only when visible moisture is present. C) Also as a courtesy light on the ground. D) Momentarily to detect ice accumulations at night.
Maximum weight for flight into known icing conditions for a 208B aircraft with a PT6A114
powerplant is:
A) 6.000 lbs. B) 7.000 lbs. C) 8.000 lbs. D) 8.750 lbs. .
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