Anti_Ice

Is engine anti-ice available if the respective engine bleed valve is closed ?
1. Yes.
2. Yes, but only if the isolation valve is open.
3. No.
Is wing anti-ice available if the respective engine bleed switch is OFF or the respective engine bleed valve is not open ?
1. Yes, but only if the isolation valve is open.
2. No.
3. Yes.
Is wing anti-ice is available on the ground ?
1. Yes, if the thrust setting is below take-off warning horn activation and the temperature in the distribution duct is below thermal overheat switch activation.
2. Yes, if the temperature in the distribution duct is below thermal overheat switch activation.
3. Yes, if the thrust setting is above take-off warning horn activation.
4. No.
If one wing bleed air distribution duct has an overheat condition
1. wing anti-ice is lost in that wing leading edge and asymmetric lift must be considered in icing conditions.
2. wing anti-ice is lost in that wing leading edge and the WING ANTI-ICE switch must be positioned OFF.
3. both wing anti-ice valves will close automatically and the WING ANTI-ICE switch trips OFF.
4. both wing anti-ice valves will close automatically and the WING ANTI-ICE switch remains ON.
Which statement is true with regard to the wing ant-ice switch.
1. The wing anti-ice switch, if ON, trips OFF at lift-off and must be repositioned to ON if wing anti-ice is required.
2. Both wing anti-ice valves close but the wing anti-ice switch remains ON at lift-off and must be repositioned to OFF and then ON if wing anti-ice is required.
3. The wing an-ice switch, if ON, trips OFF when take-off power is applied and must be repositioned to ON once airborne if wing anti-ice is required.
Which statement is true with regard to the wing and engine anti-ice switches.
1. If engine anti-ice is used during flight, stick shaker logic is set for icing conditions for the remainder of the flight if wing anti-ice has been used.
2. If engine anti-ice is used during flight, stick shaker logic is set for icing conditions for the remainder of the flight regardless of wing anti-ice operation.
3. Stick shaker logic returns to normal if both engine anti-ice and wing anti-ice have been used and are subsequently positioned to OFF.
4. Engine anti-ice operation has no effect on stick shaker logic.
Which statement is true with regard to wing-anti-ice operation.
1. Stick shaker logic is set for icing conditions for the remainder of the flight if wing anti-ice is used regardless of subsequent WING ANTI-ICE switch position.
2. Stick shaker logic is set for icing conditions only when wing anti-ice is being used.
3. Stick shaker logic is set for icing conditions for the remainder of the flight only when both wing ant-ice and engine anti-ice are being used.
Which statement is true with regard to wing anti-ice in flight.
1. Duct temperature and thrust setting logic is disabled and has no effect on wing anti-ice control valve operation.
2. Only thrust setting logic is disabled and has no effect on wing anti-ice control valve operation.
3. Only duct temperature logic is disabled and has no effect on wing anti-ice control valve operation.
4. Duct temperature and thrust setting logic is the same whether in-flight or on the ground.
If a wing anti-ice valve closes in flight and the wing anti-ice switch is ON, what indication will be available to the crew ?
1. The respective L or R VALVE OPEN light will illuminate bright blue.
2. The respective L or R VALVE OPEN light will extinguish.
3. The respective L or R VALVE OPEN light will illuminate dim blue.
4. The respective L or R VALVE OPEN light will illuminate bright blue and then extinguish.
If the ENG ANTI-ICE switch is ON and the respective engine anti-ice valve (cowl valve) does not agree with the engine anti-ice switch position, what are the crew's indications ?
1. The COWL VALVE OPEN light will illuminate bright blue and the TAI annunciator above the N1 gauge turns from green to amber.
2. The COWL VALVE OPEN light will illuminate bright blue and the Master Caution and ANTI-ICE annunciator illuminate.
3. The COWL VALVE OPEN light will extinguish and the Master Caution and ANTI-ICE annunciator illuminate.
4. The COWL VALVE OPEN light will illuminate bright blue and the TAI annunciator above the N1 gauge extinguishes.
The amber COWL ANTI-ICE warning light illuminated indicates ?
1. an overtemperature condition.
2. an overpressure condition.
3. an overtemperature condition or an overpressure condition.
4. The cowl anti-ice valve is in disagreement with the ENG ANTI-ICE switch position.
What is adjusted when stall shaker logic is set during anti-ice use ?
1. Stick shaker and minimum maneuver speeds.
2. Stick shaker and Vref.
3. Minimum maneuver speeds and Vref.
4. Stick shaker, minimum maneuver speeds and Vref.
What is the restriction on the use of windshield wipers ?
1. Windshield wipers may not be operated on a dry windshield.
2. Windshield wipers may not be operated above 230 knots.
3. Windshield wipers have no restrictions.
What is indicated by the window heat OVERHEAT warning light ?
1. An overheat condition is detected or electrical power to the respective window(s) is interrupted.
2. An overheat condition is detected.
3. Electrical power to the respective window(s) is lost if the Master Caution and ANTI-ICE annunciator are also illuminated.
What is the restriction with regard to performing a window heat power test ?
1. The power test may only be conducted when the ambient temperature is below 80 degrees Fahrenheit or 27 degrees Celsius.
2. The power test may not be conducted when all window heat ON lights are illuminated.
3. The power test may not be conducted when all window heat ON lights are extinguished.
4. The power test may not be conducted when any of the window heat switches are ON.
Which statement is true with regard to the window heat overheat (OVHT) test.
1. The test simulates an overheat condition and must be reset by positioning the window heat switches to OFF.
2. The test simulates an overheat condition and must be reset by positioning the test switch to PWR TEST.
3. The test checks the light circuitry and must be reset by positioning the window heat switches to OFF.
4. The test simulates an overheat condition and all window heat ON lights immediately extinguish.
Which windows are capable of being de-fogged using the Windshield Air controls ?
1. L1 and R1 only.
2. L1, L2 and R1, R2 only.
3. L1, L2, L3 and R1, R2, R3.
4. All windows including the "eyebrow" windows.
Which windows have an electrically conductive coating on the outer pane ?
1. L1 and R1 only.
2. L1, L2 and R1, R2 only.
3. L1, L2, L3 and R1, R2, R3.
4. The outer pane is heated on all windows.
Window heat is not available when operating on standby electrical power.
1. True.
2. False.
Which static ports are heated ?
1. None.
2. The four main static ports.
3. All six static ports.
4. The two alternate static ports.
Which statement is true when operating on standby electrical power.
1. All probes remain heated.
2. Only he Captain's and First Officer's probe are heated.
3. Only the Captain's probe is heated.
4. Only the AUX pitot tube is heated.
Are the elevator pitot tubes heated ?
1. Yes.
2. No.
Which warning lights are associated with a probe heat failure ?
1. The respective probe light will illuminate.
2. The respective probe light and Master Caution light will illuminate.
3. The respective probe light, Master Caution light and ANTI-ICE annunciator will illuminate.

Anti Ice and Rain Protection