AVIÔNICOS (Especial - English)
Fonte: Avionics and maintenance of aircraft
ELECTRICAL SYSTEM:
Attitude representation by the attitude indicator corresponds to the relation of the aircraft to the real horizon:
Pitot-Static system and instruments:
Avionics System - ATR 60:
Hydraulic System of Rudder:
Structure of EIS (Electronic Instruments System) (ECAM & EFIS):
DMC - Displays Management Computer
It is responsible for processing the data; parameters to be displayed on screen, there are 3 DMC, one DMC, can manage three screens, PFD, ND and one of ECAM.
FWC - Flight Warning Computer
Monitoring systems, and generates all the messages; both on screen and the audible messages.
SDAC - System Data Acquisition Computer
Responsible for receiving data from the systems and send them to the FWC and DMC.
It is responsible for processing the data; parameters to be displayed on screen, there are 3 DMC, one DMC, can manage three screens, PFD, ND and one of ECAM.
FWC - Flight Warning Computer
Monitoring systems, and generates all the messages; both on screen and the audible messages.
SDAC - System Data Acquisition Computer
Responsible for receiving data from the systems and send them to the FWC and DMC.
Main controls of cockpit:
Conventional Wingtip VS Blended Winglet:
A distribuição na cabine, é formado por 5 partes principais:
1 - parte superior (painel de sobrecarga)
2 - painel anti-brilho (Glareshield)
3 - painel principal (painel de instrumentos principal)
4 - painel de controle do suporte (controle Pedestal)
5 - consoles de lado (lado Consoles):
AIRBUS BOEING ou AIRBUS: fuselagem é em linha reta no topo. (A fuselagem é uma linha reta na parte superior)
BOEING: fuselagem se inclina para baixo na cauda. (A fuselagem se inclina para baixo na fila)
