NAVIGATION & DISPLAY PANEL Flashcards
1
Q
VHF NAV Transfer Switch
- 3 positions -
BOTH ON 1
NORMAL
BOTH ON 2
A
- this switch changes the source of the data that the DEUs use for the Nav Displays (ND).
- transfers: DME, ILS, VOR and MCP Course information
- enables selection of the opposite vhf nav receiver/MMR if it fails
BOTH ON 1:
- DEUs use MMR 1 as the source for CAPT & FO displays
- if neither AP’s are in CMD and both FD switches are ON - in this position FD B will bias out of view
- FO instruments are referenced to CAPT selected course and Nav receiver
NORMAL:
- MMR 1 drives Capts display and MMR 2 drives FO display
BOTH ON 2:
- DEUs use MMR 2 as the source for CAPT & FO displays
- if neither AP’s are in CMD and both FD switches are ON - in this position FD A will bias out of view
- CAPT instruments are referenced to FO selected course and Nav receiver
Notes:
- if in either BOTH ON 1 (or 2) - the RMI needles will not transfer (ie if both on 2, the narrow VOR needles on both RMIs are inop. - has nothing to do with ADFs
CAUTION:
- the DFCS (digital flt control sys) can’t use VOR/ILS data that is not shown on the displays.
- so, when the AP is engaged - the VHF Nav control MUST MATCH the primary AP that is ENGAGED for proper ILS/VOR ops
- CMD A uses VHF Nav 1 - CMD B uses VHF Nav 2
2
Q
IRS Transfer Switch
- 3 position -
BOTH ON L
NORMAL
BOTH ON R
A
- enables selection of the opposite IRS (ADIRU) in the event of attitude or compass failures
- moving this switch will kick off the AP
- when selected to either BOTH ON L (or R) - either AP can be engaged (but should use the unfaulted one)
- when AP is ENGAGED - the YD will DISENGAGE and CANNOT BE RECONNECTED until AP is disengaged
BOTH ON L:
- switches the gyro source (ATT and HDG) to the left IRS
NORMAL:
- Default setting. Left flight instrument source - LEFT ADIRU and Right inst source - RIGHT ADIRU
BOTH ON R:
- switches the gyro source (ATT and HDG) to the right IRS
Note:
- when this switch is NOT in the NORMAL position - you will get a ‘INSTR SWITCH’ message which tells you that CAPT and FO are using same ADIRU source
- this light is on the LOWER RIGHT of BOTH PFD’s
3
Q
FMC Source Select Switch
- 3 position -
BOTH ON L
NORMAL
BOTH ON R
A
- Dual FMCs
- when either BOTH ON L (or R) selected the second FMC will become a navigation monitor - info will still be sent to the FMC
- Moving this switch - causes LNAV to DISENGAGE (revert to CWS ROLL) and VNAV disengages (revert to ALT HOLD)
BOTH ON L:
- Selects Left FMC for all FMC operations
- Right Map will show ‘FMC L’ light
NORMAL:
- LEFT FMC -
- controls CDUs
- provides inputs to Auto Throttle
- RIGHT FMC -
- dual operation enabled (ie Right is synced to the Left)
- Maps display composite info from BOTH FMCs
- each FMC provides it own inputs to its own:
- FCC
- MAP
- Auto Pilot
- Nav / Radio tuning
BOTH ON R:
- Selects RIGHT FMC for all FMC operations
- LEFT Map will show ‘FMC R’ light
4
Q
DISPLAYS ‘SOURCE’ Switch
- 3 position -
ALL ON 1
AUTO
ALL ON 2
A
- controls the 2 DEUs (all DUs can be driven by either one or both DEUs)
- controls which DEU sends info to which DU
- normally this is used on the ground for maint purposes
- under airspeed tape a [CDS FAULT] light might illuminate (non-dispatchable)
ALL ON 1:
- selects CAPTs DEU (#1 deu) to drive all 6 displays
- ‘DSPLY SOURCE’ light on BOTH PFDs below the speed tape
AUTO:
- DEU 1 drives Capt side DUs and Upper DU
- DEU 2 drives FO side DUs and Lower DU
- provides automatic switching from both to one if there is a single DEU failure
ALL ON 2:
- selects FOs DEU (#2 deu) to drive all 6 displays
- ‘DSPLY SOURCE’ light on BOTH PFDs below the speed tape
5
Q
DISPLAYS - CONTROL PANEL Switch
- 3 position -
BOTH ON 1
NORMAL
BOTH ON 2
A
- normally these switches are used on the ground for maint purposes
- might get [DISPLAYS CONTROL PANEL] light - due to invalid EFIS panel data
BOTH ON 1:
- both CAPT & FO displays are controlled by the CAPTs EFIS panel
NORMAL:
- left EFIS panel controls CAPT displays and right EFIS panel controls FOs displays
BOTH ON 2:
- both CAPT & FO displays are controlled by the FOs EFIS panel