REC A320 TEST

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

In the Avionic Equipment Ventilation System, the Temperature parameter is taken: From TAT sensor. From P2/T2 sensor. From its own skin temperature sensor.

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 by Backup Radio Altitude. is replaced by GPS Altitude.

What is the purpose of the Backup Speed Scale (BUSS). Help the flight crew to fly at a safe speed and altitude in the case of an unreliable speed/altitude indication. Provides a safe speed and altitude to flight at altitudes greater than 25.000 ft. Provides a safe speed and altitude for AP,FD, A/THR and Cabin Pressure.

The position feedback of the Thrust reverser for the EEC comes from: Four (4) proximity sensors and targets. Two (2) LVDTs located in the Upper locking actuators. Four (4) deploy and four (4) stow position switches.

What will be the altitude in the AP/FD TCAS mode after the clear of conflict?. Current altitude. Altitude hold. Previous FCU selected altitude.

On the Thrust Reverser system, the Locking devices known as the "third line of defense" are the: Tertiary Locks. Manual inhibition lever and cable. Locking Actuators.

When the nacelle anti-ice system is operating, a hot air leak detection is done by mean of: Two pressure transducers. One pressure transducer and one temperature sensor. A dual temperature sensor.

Avionic equipment ventilation, when low flow is detected: The Fault light of the Blower or Extractor fan push button will illuminate. The blower fan will stop. The system will go to closed circuit configuration.

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

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

Which parameter are taken in account to calculate Backup speed scale (BUSS)?. Flaps/Slats position. Angle of attack. Both are correct.

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

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

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

In the PW 1100 Engine, where does the nacelle anti-ice system take air from?. Bypass. HP3. HP6.

What type of valve does it have the engine Anti-ice valve (NAI) system: It´s a two pressure regulating & shut off valves system. A shut off type valve, just can be open or close. A modulated electrical type valve.

Usually, the most common configuration on ground for the Equipment Ventilation System is: Partially Open. Open. Closed.

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.

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

In the PW 1100 Engine, the Track Lock Valve (TLV) in the thrust reverse actuation system controls: Alternate deploy of thrust reverse system. Locking and unlocking of the tertiary locks. Locking and unlocking of manual drive units.

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

In the PW 1100 Engine, where are the translating sleeve lockout pins for deactivation of the Thrust Reverser System located?. Next to Hydraulic control Unit (HCU) inhibition lever. In the flight deck, next to landing gear lock pins. On top of the closure assist system.

Related to the Radome on the A320 family, now it is known as: Evolution 2. Evolution 3 (Isovolta). Evolution 1.

Which are the main functions of the AIDS?. Recording of the mandatory flight data requested by the airworthiness authority. Trouble shooting of avionics computers only. Trouble shooting of avionics computers only.