22-11. FLIGHT MANAGAMENT SYSTEMS (FMS)
All questions: 76
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1. Which FMC/CDU page normally appears on initial power application to the B737-400 Electronic Flight Instrument System?
2. The most common sensors interfacing a FMS to compute the aircraft position along the flight plan are:
1) DME
2) GPS
3) LOCALIZER
4) NDB
The combination which regroups all of the correct statements is:
3. The FMS provides the following functions: 1) aircraft position computation 2) traffic alerts 3) lateral flight plan management 4) fuel management The combination which regroups all of the correct statements is:
4. When initial position is put into an FMS, the system:
5. The FMC position is:
