Indicating and Recording Flashcards
Electronic Instrument System EIS comprised by:
6 Display Units DUs. DUs full cathode raytubes and identical
Electronic Instrument System EIS:
Electronic Flight Instrument System EFIS; Electronic Centralized Aircraft Monitor ECAM
ECAM comprised by:
Engine / Warning Display E/WD; System Display SD
Display Management Computers – 3. Sensors:
NAV Data/ ADIRS data – DMC 1,2,3
Each DMC has
2 independent channels
2 identical FWCs :
Red warnings, amber cautions, alert messages, memos, aural alerts, synthetic voice messages
ECAM/ND XFR: allows ECAM system display to be shown on
Either the Captain’s or FO’s ND
DMC sw in AUTO:
DMC3 supplies data for both ECAM DUs
Pulling barometric knob will set
QNH pressure
Flight data recording system:
Flight data interface and management unit, digital flight data recorder DFDR, linear accelerometer LA
Digital Flight Data Recorder DFDR -
25h, underwater locator beacom
If PFD – if bank angle exceeds 45º, all PFD symbols disappear, except for
Attitude, speed, heading, altitude, and vertical speed
Between 30º up and 10º down, markers set every
2,5º
Pitch attitude and roll angle protection symbols represent max bank
67º and max pitch 30ºup and 15ºdown
Side slip blue if EO, config 1, 1+F, 2,3, or full (beta target) >1.3 EPR or difference ENG EPR
> .25
Airspeed scale- speed trend arrow – predicted speed in
10 sec (at constant rate); pointer appears if rate of change >2kt; pointer disappears if rate of change < 1kt or FMGC fail
Blue triangle = selected speed from FCU
Magenta triangle -
Managed speed
Green Mach number when current speed > M 0.5