A-320 Chapter № 11. Ice and Rain

17問 • 1ヶ月前

Popovich

通報

問題一覧

11.1. An A320\A321 has the following anti-icing systems:

A. Hot air & electrical heating

11.2. The following critical areas of the aircraft are heated by hot air:

A. Three outboard leading-edge slats of each wing and engine air intakes

11.3. When the engine anti-ice is on:

B. Idle N1 is automatically increased, if necessary

11.4. Probe heat comes on automatically when:

C. When at least one engine is running

11.5. Can the probes be heated manually?

C. Yes, the flight crew can push the PROBE/WINDOW HEAT p/b

11.6. Pitot heating logic on the ground:

C. Starts at a low level. The changeover to normal power occurs automatically in flight

11.7. On the ground with WING A.ICE p/b switch ON:

A. WAI control valves open for 30 seconds (test sequence)

11.8. Are there any WING ANTI ICE indications displayed on ECAM?

B. WING A. ICE appears on the ECAM MEMO page in green. In addition for NEO aircraft WAI green memo comes on top of EWD when the thrust levers are in TOGA or FLX/MCT detent

11.9. ICE NOT DET memo appears on the ECAM MEMO page in green if:

B. Ice is no longer detected after period of 190s

11.10. If one engine anti-ice system fails, the second one takes over and provides anti- icing for both engines.

False

11.11. Window heating comes on automatically when:

C. When at least one engine is running

11.12. On the ground, the windshield heating operates as follows:

C. Starts at a low level. The changeover to normal power occurs automatically in flight

11.13. The drain masts are heated by:

B. Electrical heating

11.14. What is the maximum speed for windscreen wipers operation?

C. 230 kts

11.15. The Engine Nacelle is anti-iced by:

A. Air bleed from the high-pressure compressor

11.16. A BOOST ICE PROT indication is displayed on the ENG SD page (Leap-1A). It indicates:

B. That Hot Air is provided to the booster to prevent ice crystal formation

11.17. With the loss of electrical power the wing anti ice valves:

C. Fail to close position

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問題一覧

11.1. An A320\A321 has the following anti-icing systems:

A. Hot air & electrical heating

11.2. The following critical areas of the aircraft are heated by hot air:

A. Three outboard leading-edge slats of each wing and engine air intakes

11.3. When the engine anti-ice is on:

B. Idle N1 is automatically increased, if necessary

11.4. Probe heat comes on automatically when:

C. When at least one engine is running

11.5. Can the probes be heated manually?

C. Yes, the flight crew can push the PROBE/WINDOW HEAT p/b

11.6. Pitot heating logic on the ground:

C. Starts at a low level. The changeover to normal power occurs automatically in flight

11.7. On the ground with WING A.ICE p/b switch ON:

A. WAI control valves open for 30 seconds (test sequence)

11.8. Are there any WING ANTI ICE indications displayed on ECAM?

B. WING A. ICE appears on the ECAM MEMO page in green. In addition for NEO aircraft WAI green memo comes on top of EWD when the thrust levers are in TOGA or FLX/MCT detent

11.9. ICE NOT DET memo appears on the ECAM MEMO page in green if:

B. Ice is no longer detected after period of 190s

11.10. If one engine anti-ice system fails, the second one takes over and provides anti- icing for both engines.

False

11.11. Window heating comes on automatically when:

C. When at least one engine is running

11.12. On the ground, the windshield heating operates as follows:

C. Starts at a low level. The changeover to normal power occurs automatically in flight

11.13. The drain masts are heated by:

B. Electrical heating

11.14. What is the maximum speed for windscreen wipers operation?

C. 230 kts

11.15. The Engine Nacelle is anti-iced by:

A. Air bleed from the high-pressure compressor

11.16. A BOOST ICE PROT indication is displayed on the ENG SD page (Leap-1A). It indicates:

B. That Hot Air is provided to the booster to prevent ice crystal formation

11.17. With the loss of electrical power the wing anti ice valves:

C. Fail to close position