A.320.REC.HELP

Related to the Radome on the A 320 family, now it is known as: 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 posición?. No, dispatch with both PRSOVs lock in open position is not allowed. Yes, if they 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 illuminated 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 (dolor frame). The slide lever must be in disarmed position.

What is the meaning of IR FAULT light illuminated 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 traffic. 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 INDIC/ADR CHECK 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 rank. 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 doors. 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 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 INDIC/ADR CHECK PROC the altitude indications on PFD...: Is replaced by altitude calculated by FMC and Radio Altimeter. Is replaced by GPS altitude. Is replaced by Backup Radio Altitude.

Where are located the main components of the IGGS (Inert Gas Generation System)?. On the 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.

CIDS - Each DEU has to be adressed for proper operation. How is this achieved?. Only on the last DEU is adressed. The DEUs are adressed by the software in the Directors. The DEUs are adressed by "CODING SWITCH".

CIDS - The CIDS system is made of two computers, they are...: Two DEUs. Two Directors. Two CFDCs.

CIDS - What are the units directly related with the pax services?. The Auxiliary Attendant Panels. The Decoder Encoder Unit's A. The Decoder Encoder Unit's B.

The position of the inlet and Extraction valves (equipment ventilation) is shown: It is not shown. In the Bleed page. In the Cab Press page.

The error used to apply the performance criteria (removal, check, etc...) in an ADIRU is: Attitude error. Residual ground speed. Radial position error.

How is the operator warned that there is differential press before to open any door?. By means of a white flashing light. A red flashing light is seen on the door. The door control handle is locked due to the cabin press.