FMS Flashcards
FMS
3d flight management system that calculates a 4d flight trajectory
CDU
control display unit
1 for captain 1 for FO, sometimes a third
FMC
flight management computer
2, one for each CDU, connected as a backup up to other CDU
X-talk bus- connects both FMC so they can communicate
Duel mode
normal operation
each CDU connected to its own FMC
FMCs communicate via x-talk bus
info entered on either side will update eon both
single mode
one FMC failed
both CDUs on one FMC
info can still be entered on either side
may be limitations on AP usage and EFIS
NAV displays may need the same mode and range set
independent mode
X-talk bus failed
FMCs cant communicate
entering on CDU1 only FMC1 would receive it
need to enter information on both sides separately
FMS inputs
pilot clock database GPS IRS ADC configuration fuel air ground logic switch FWS CDU NAV radios
FMS outputs
autopilot
auto thrust
HUD
EFIS
navigation database
SID's- standard instrument approaches STAR's- standard arrivals airways way points airports approaches runways company routes
valid over 28 day period
ways to enter way points
lat and long
Wpt name
nav aid ident
ICAO airport code
performance data base
fuel parameters drag parameters engine parameters speeds one engine inoperative data
it can account for engine failure
can not account for non-standard configuration
FMS position calculation
mixes various sources of position to find most likely position sources: -VOR,DME , localiser on some - GPS -IRS
priority of sources
GPS>DME>VOR>IRS
initialising the fms
1) who am I? IDENT- aircraft type/ engine type
2) where am I? pos init- position info
3) where am I going? route- route info
4) how do I get there? performance
FMS functions: LEGS page
waypoints tracks distances predicted speed predicted altitude speed constraints altitude constraints
FMS functions:LNAV
lateral navigation
connects auto pilot and FMS
FMS tells AP to fly: headings & bank angles to achieve flight planned route