Lernkarten

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

1/144

Fenster schliessen

Aircraft systems and structures are identified by means of a specific classification system. Name it.

ATA chapters (Air Transport Assocciation System)

Fenster schliessen

For maintenance purposes, mainly related to the landing gear, four jacking points are provided. Where have they located?

  • one below each wing
  • one in front of the nose landing gear bay
  • one safety point under the rear fuselage point
Fenster schliessen

The air conditioning system basically ensures

  • temperatur regulation
  • ventilation and pressurisation
Fenster schliessen

Which are the controllers related to the pressurization system?

CPC 1 & CPC 2

Fenster schliessen

Correct cabin pressurization is obtained by controlling the conditioned air discharge through

two outflow valves

Fenster schliessen

Which and how many valves do prevent excessive positive or negative differential pressure?

  • Two Safety Valves (installed on aft pressure dome)
  • One Negative Pressure Relieve Valve (installed on FWD Fuselage)
Fenster schliessen

Mention 5 communication systems installed on A330 Aircraft.

  • 2 HF / 3VHF Systems
  • SELCAL (selective calling)
  • ACARS (Aicraft Communication Addressing and Reporting System)
  • SATCOM System
  • Passenger Address System
  • CIDS (Cabin Intercommunication Data System)
  • IFE
  • Interphone communication System
  • Cockpit Voice Recorder
  • CPDLC
Fenster schliessen

For what reason interphones are used – mention 3

  1. Cabin interphone (Cabin - Cockpit)
  2. Flight interphone (Ground engineer)
  3. Service interphone (com. between verious interphones)
Fenster schliessen
Lizenzierung: Keine Angabe

Mention the possible supply sources for the aircraft’s electrical systems

Lizenzierung: Keine Angabe
Fenster schliessen

AC electrical power supplied to the aircraft systems has following voltage/frequency characteristics:

115V / 400Hz

Fenster schliessen

How many Batteries are installed (name it)?

3 Batteries (2 Main Batteries BAT 1+2; 1 APU Battery)

Fenster schliessen

How are the main electrical systems feeded if during flight both IDG and the APU Generator fails?

With the Emergency Generator (Constant Speed Motor / Generator) driven by the green hydraulic system & RAT activation

Fenster schliessen

What are the aircraft equipment and furnishings?

- the cockpit
- the passenger compartment
- the cargo compartments
- the avionics compartment
- the emergency equipment

Fenster schliessen

What is the Nacelle and what is the purpose of it?

- Nacelle is the aerodynamic structure around the basic engine (Nose Cowl or Intake Cowl, Fan Cowls, Thrus Reverser, Exhaust Nozzle and Exhaust Plug)
- The purpose is to prevent damage to the basic engine, to smoothout the Fan Air Flow, give additional strenght to the engine structure.

Fenster schliessen

Write in full text the following acronyms:

  • DFDR:
  • THS:
  • RAT:
  • CVR:
  • FCPC:
  • SFCC:
  • ACARS:

DFDR: Digital Flight Data Recorder
THS: Trimmable Horizont Stabilizer
RAT: Ram Air Turbine
CVR: Cockpit Voice Recorder
FCPC: Flight Control Primary Computer
SFCC: Slat/Flap Control Computer
ACARS: Aicraft Communication Addressing and Reporting System

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

3 FCPC, 2 FCSC, 2 SFCC, 2 FCDC

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?

Yes

No

Fenster schliessen

The purpose of the Trim Transfer System is to

control the center of gravity position