Instruments Flashcards
ADIRU
Air Data Inertial Reference Unit
ADIRU power
#1 Emergency AC Bus - A/C battery for backup (60mins) #2 Right AC Bus - internal battery backup (30mins)
ADIRU modes
1) Align mode (“No Taxi”)
2) Taxi mode (“Taxi”)
ADIRU Data Acronym for info provided
HAAAVPP
Heading (true and mag) Acceleration Attitude Angular Rate Velocity Present Position
What info provided on ISIS
Integrated Standby Instrument System
Attitude - Altitude - Airspeed
Primary Functions of VIAs
Versatile Integrated Avionics
1) Electronic Instrument System (data display)
2) Flight Management
3) Master Warning and Caution Lights
4) Central Audio
5) Digital Flight Data Acquisition
How are VIAs powered
VIA1 Emergency DC bus
VIA2 Right DC bus
Aural Warnings (sound types)
Sirens, Horns, Chimes, Bells, Voice Messages
Alert Levels
LEVEL 3 - red and within red box
Level 2 - boxed amber
Level 1 - amber
Level 0 - cyan
ECP
EIS Control Panel - select what to be displayed on ND
MAP, PLAN, TCAS, VOR, APPR
EIS
Electronic Instrument System - consists of:
6 Display Units (DUs or LCDUs)
1 System Display Control Panel (SDCP)
2 Versatile Integrated Avionics (VIA) units
MCDU
SDCP
FCC
Multi-Function Control Display Unit
System Display Control Panel
Flight Control Computer