R. A320FAM... part2

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

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

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 for AP, FD, A/THR and Cabin Pressure. Provides a safe speed and altitude to flight at altitudes greater than 25.000 ft.

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

In the UNRELIABLE SPEED INDIC/ADR CHECK PROC the altitude indications on PFD: is replaced by GPS Altitude. is replaced by Altitude calculated by FMC and Radio Altimeter. is replaced by by Backup Radio Altitude.

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

Which are the main functions of the AIDS?. Engine condition, APU condition and aircraft performance monitoring. Trouble shooting of avionics computers only. Recording of the mandatory flight data requested by the airworthiness authority.

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

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

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.

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

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

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

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

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

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

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

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.

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

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

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

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 DEUs. Two Directors.

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