A320 2023

Related to the Radome on the A 320 family, now it is known. Evolution 2. Evolution 3 (isovolta). Evolution 1.

What happens to AP/FD when the TCAS Resolution Advisory is triggered. Engages APs if they are disengaged. Lateral AP/FD mode does change. Engages FDs if they are disengaged.

In the PW 1100 Engine, could you dispatch the aircraft with both engine anti-ice PRSOV locked in open position?. No, dispatch with both PRSOVs lock in open position is not allowed. Yes, if the aircraft is operated in known or forecast icing conditions. Yes, increasing fuel planning in 5%.

The main AIDS MCDU functions for line maintenance purposes are: Alpha and Label call-up. List of Previous Reports. Special reprogramming functions.

What is the meaning of IR FAULT light iluminated intermittently?. Inertial part is lost. Attitude and heading information may be recovered in ATT mode. No present position inserted.

For Maintenance purpose. On A321 airplane, to avoid inadvertent deployment of the slides of the aditional emergency exit doors: The slide lever must be in disarmed position, and pins installed in the slide cylinder and the release lever on door frame. The slide lever must be in armed position and a pin installed on the Slide Release Lever (door frame). The slide lever must be in disarmed position.

What is the meaning of IR FAULT light ulluminated steady on CDU MODE SELECTOR UNIT (MSU) or CONTROL DISPLAY UNIT?. No present position inserted. Attitude and heading information may be recovered in ATT mode. Inertial part of the ADIRU is not working.

The AIDS reports, are generated...: manually only. manually or automatically. automatically only.

Which is the purpose of the TCAS system: Is to avoid collisions air trafic. Is to show areas of severe weather. Is to guide the airplane during flight.

In the PW1100 engine, in the thrust reverser system the manual drive unit allows: Deactivate the thrust reverser to flight. Manual translation of the thrust reverser during maintenance. Hydraulic operation during maintenance.

In the PW1100 engine, the fail position of the engine anti-ice valves is: Both full open. Upper valve full open and lower valve partially open. Both full close.

In the UNRELIABLE SPEED INDICATOR CHECK PROC the speed indications on PFD...: Is replaced by Backup Groundspeed (GS). Is replaced by Backup Speed Scale. Is replaced by Backup True Airspeed (TAS).

In the PW1100 engine, where is the inhibit hydraulic control unit (HCU) lever located?. Next to engine oil tank. On the same HCU located at pylon zone. On the locking feedback actuator.

The A-321 is provided with: Two type 1 emergency exit doors. Four type 1 emergency exit door. Four overwing emergency exit hatches.

In the A321, where are the inflation reservoirs of the emergency exit slides installed?. In the slide compartment. Above the respective emergency exit. In the aft cargo compartment.

CIDS- What happens if CIDS-Director 1 fails?. Director 2 automatically takes over the entire CIDS functions. The Top Line Cut Off Relay deactivates the DEU´s A. The EMER-Pushbutton has to be pushed to activate the second CIDS-Director.

In the PW1100 engine, during an autostart on ground, when is the ignition system alternated?. In each start. Every two start attempts. If the ignition system 1 fails.

In the UNRELIABLE SPEED INDICATOR CHECK PROC the alttitude indications on PFD...: Is replaced by Altitude calculated by FMC and Radio Altimeter. Is replaced by GPS Altitude. Is replaced by by Backup Radio Altitude.

Where are located the main components of the IGGS (Inert Gas Generation System). On a pallet located very close to the mixing unit (fwd cargo compartment, rear area). Most of the components are located just above the center fuel tank. On a pallet located in the left air conditioned pack compartment.