737 AQP Anti-ice /Rain

ICE6.30.1 Engine ignition must be selected to _____ prior to and during engine anti-ice operation. GRD. CONT. OFF.

ICE6.30.2 Window heat must be ON _______ before takeoff. 10 minutes. 15 minutes. 5 minutes.

ICE6.30.3 Probe heat must be ____________. ON before engine start. ON before takeoff. ON before taxi.

ICE6.30.4 Which flight deck windows are not electrically heated?. L2 and R2. L3 and R3. L2, L3, R2 and R3.

ICE6.30.5 Temperature controllers maintain window heat on windows ________ at the correct temperature to ensure maximum strength of the windows in the event of bird impact. L1, R1, L2, and R2. L1, L3, R1, and R3. L3, L2, L1, R1, R2, and R3.

ICE6.30.6 On the Window Heat Panel, when an overheat condition is detected, power is removed from the window, __________, and the green ON light extinguishes. an amber OVERHEAT Light is illuminated. a green OVERHEAT Light is illuminated. a red fire warning light is illuminated.

ICE6.30.8 Placing the WINDOW HEAT Test Switch to OVHT_______________. bypasses all overheat circuitry. simulates an overheat condition. simulates an overheat condition and all window ON lights illuminate.

What happens when placing the WINDOW HEAT Test Switch to PWR TEST_______________. the controller is forced to remove all power, bypassing normal temperature control. bypasses all overheat protection. provides a confidence test.

Engine bleed air thermal anti-icing prevents the formation of ice on the _____. spinner. engine fan blades. engine cowl lip.

Each cowl anti-ice valve is _______ controlled and ______ actuated. pressure; electrically. electrically; pressure. electrically; hydraulically.

What occurs when the ENG ANTI-ICE switches are positioned to ON?. The stick shaker and minimum speed bars on airspeed indications are adjusted. The airspeed indications return to normal when engine anti-ice is positioned OFF if wing anti-ice has not been used in flight. Engine bleed air is allowed to flow through the cowl anti-ice valve for cowl lip anti-icing, and the stick shaker logic is set for icing conditions. All answers are correct.

If the cowl anti-ice valve fails to move to the position indicated by the ENG ANTI-ICE switch, an amber TAI indication illuminates on the CDS after a short delay, and the COWL VALVE OPEN light. remains illuminated bright blue. remains illuminated dim blue. illuminates amber.

On the Engine Anti-Ice Panel, an amber illuminated COWL ANTI-ICE Light indicates __________. cowl anti-ice needs to be turned on. an over-temperature condition in duct downstream of engine cowl anti-ice valve. excessive pressure in the duct leading from the cowl anti-ice valve to the cowl lip.

What does an amber TAI on the upper display unit above the N1 gauge indicates?. cowl anti-ice valve is not in the position indicated by the related engine anti-ice switch. cowl anti-ice valve is in the requested position indicated by related engine anti-ice switch. cowl anti-ice needs to be turned on.

The wing anti-ice system does not include the _______ or the_________. leading edge flaps; inboard leading edge slats. leading edge flaps; outboard leading edge slats. any of leading edge devices; trailing edge flaps.

On the ground, both of the wing anti-ice valves close if either engine thrust is above the takeoff warning setting or ____________. a duct leak condition is sensed. either temperature sensor senses a duct over temperature. there is a split in temperature of greater than 20C.

On the Wing Anti-Ice Panel, what does a bright blue Wing Anti-Ice VALVE OPEN Light indicate?. The related wing anti-ice control valve is open (switch ON). The related wing anti-ice control valve is closed (switch OFF). The related wing anti-ice control valve is in transit, or, related wing anti-ice control valve position disagrees with WING ANTI–ICE switch position.

On the Probe Heat Panel, an amber CAPT PITOT light indicates ________. the probe is operating normally. the probe is not heated. all answers are correct.