Karten 144 Karten
Lernende 59 Lernende
Sprache Deutsch
Stufe Universität
Erstellt / Aktualisiert 22.12.2016 / 26.01.2021
Lizenzierung Keine Angabe
0 Exakte Antworten 122 Text Antworten 22 Multiple Choice Antworten
Fenster schliessen

Which compartments are given to load freight?

FWD, AFT and BULK Cargo compartments

Fenster schliessen

The fire protection system consists of

Fire detection system

Fire detection system and fire extinguishing system

Fire extinguishing system

Fenster schliessen

The flight controls are driven by which hydraulic system?

Green, Blue and Yellow Hydraulic Systems

Fenster schliessen

The roll movement is achieved by which surfaces?

2 Ailerons and 5 spoilers on each wing

Fenster schliessen

A computer arrangement permanently controls and monitors the flight control surfaces. Name the involved computers


Fenster schliessen

All the flight controll surfaces are electrically controlled and hydraulically operated. Which flight Controlls (actuators) are backed-up with mechanical cables?

- THS (Pitch axis) -> Trimmable horizontal stabilizer

- Rudder (Yaw Axis)

Fenster schliessen

The 3 principal flight control modes are

Ground mode, Flight mode, Flare mode

Ground mode, Flight mode, Landing mode

Take-off mode, Flight mode, Landing mode

Fenster schliessen

The purpose of the Manoeuvre Load Alleviation (MLA) function is to reduce the loads applied to the outer wing structure during high g manoeuvre. Explain the function's principle.

The function is achieved by 2 ailerons & 3 external spoilers on each wing. These surfaces are deflected upwards on both wings.

Fenster schliessen

Fill in the missing word within the below shown "fly by wire" philosophy.

Auto Pilot or Pilot command/order - Computed order - ...

Feedback / Aircraft response

Fenster schliessen

What are the main advantages of the "fly by wire" philosophy?

Improvement in redundancy, in handling qualities and thus in performances.

Fenster schliessen

Name the three Flight Laws.

- Normal Law

- Alternate Law

- Direct Law

Fenster schliessen

Name all available Fuel Tanks.

  • Center Tank
  • LH & RH Inner Wing Tanks
  • LH & RH Outer Wing Tanks
  • LH & RH Wing surge vent Tanks
  • Trim Tank
  • Ventilisation Tank / Vent Box
Fenster schliessen

From which Fuel Tank the engine are feeded?

LH & RH Inner Wing Tanks (Collector Cell)

Fenster schliessen

Are the Fuel Tank Pumps interchangeable?



Fenster schliessen

The purpose of the Trim Transfer System is to

control the center of gravity position

Fenster schliessen

There are a number of Magnetic Lever Indicators installed. For what reason?

To determine the physical Aircraft fuel volume in the tanks, if the indication system is inoperative or showing a wrong value.

Fenster schliessen

The aircraft is equipped with three hydraulic systems which are connected to each other. True or False?

False! Green, Blue and Yellow System are fully independent

Fenster schliessen

In normal operation the Hydraulic Systems are powered by Engine Driven Pumps (EDPs). What is the nominal pressure?

3000 psi

Fenster schliessen

Engines are not running and the yellow electrical pump for cargo door opening is not functioning. What can be done?

Cargo door opening with the mechanical hand pump (located at the yellow ground service panel)

Fenster schliessen

Which is the main Hydraulic System?

Green Hydraulic System

Fenster schliessen

The leak measurement valve operation is inhibited during flight



Fenster schliessen

What is a RAT and what is its purpose?

It pressurizes the green hydraulic system in emergency conditions.

Fenster schliessen

The Ice and Rain Protection system permits aircraft operation without restriction in icing conditions or heavy rain. Critical areas of the aircraft are protected by hot air or electrical heating. List 5 systems where hot air or electrical heating is applied.

Slats, Engines, Windows, Windshield Wipers & Rain Repellent System, Static Probes, Pitot Probes, Drain lines, Escape Slide locking mech

Fenster schliessen

The ice detection system sends warning mesages to the flight crew when icing conditions and heavy icing are detected. The ice detectors work according

a vibration frequency shift principle

Fenster schliessen

The slats on the wing's leading edge are protected against ice through the wing anit-ice system. Ice formaiton is prevented by

active heating through telespopic pneumatic tubes with hot air comig from the pneumatic system

Fenster schliessen

The cockpit comprises various panels. List 2 control panels.

OHP (Overhead Panel), Pedestal, Glareshield, Main Instrumental Panel

Fenster schliessen

The Electronic Instrumental System (EIS) comprises

an Electornic Flight Instrument System (EFIS) and an Electronic Centralized Aircraft Monitoring System (ECAM)

Fenster schliessen

The EFIS comprises

  • two Primary Flight Displays (PFD)
  • two Navigation Displays (ND)
Fenster schliessen

The ECAM comprises

  • an Engine and Warning Display (E/WD)
  • a System Display (SD)
Fenster schliessen

What is the purpose of the landing gear shortening mechanism?

It decreases the main landing gear leg length, so that it can go into the main gear bay