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Boeing 717 > Instrument and Navigation > Flashcards

Instrument and Navigation Flashcards

1
Q

What are the EIS displays / six DU’s (1 thru 6)

A

DU1 and DU6 primary displaysPFD
DU2 and DU5 Nav displays ND
DU3 engine and alert display upper2/3 engine display lower 1/3 Alerts
DU4 is the System Display (SD) engine data , systems synoptic, status page, miscellaneous pages or consequence pages

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2
Q

Versatile Integrated Avionics unit (VIA) provide data to what DU’s

A

2 VIA’s provide data display, flight management, central aural warning,master warning, caution light activation, flight data acquisition, converts data received from airplane systems to graphic display on the DU’s
VIA-1 provides data for 1-3 , (PFD,ND and EAD)
VIA-2 provides data for the DU’s 4-6(SD,NDand pfd)
If failure either VA provides data for all DU’s

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3
Q

colors associated with DU’s

A 
Red Warning
Amber caution
Brown earth
white scales
green engaged mode
Blue sky
cyan advisory or status
magenta ILS déviation pointer and flight bars
Color for systems synoptic symbols
Red warnign
Amber abnormal state
White inactive
Green active
Cyan general
Synoptic lines
Red manifold failure
Amber high temperature
White primary flow lines no flow
Green primary flow lines with proper flow
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4
Q

Primary flight Display indications

A

The PFD displays the following:

  1. Conventional attitude indication.
  2. Flight director bars (pitch and roll).
  3. Lateral (localizer) deviation.
  4. Vertical (glideslope) deviation.
  5. Marker beacon.
  6. Radio altitude.
  7. Airspeed/Mach/taxi speed.
  8. Limit speed.
  9. Pitch limit/ bank angle limit indication.
  10. Vertical speed/ TCAS.
  11. Slip (lateral acceleration).
  12. Flight mode annunciation (FMA).
  13. Windshear and predictive windshear.
  14. Airplane configuration.
  15. Heading/track.
  16. STALL annunciation.
  17. Altitude/ baroset/ selected altitude.
  18. Marker beacon.
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5
Q

ND displays

A

The ND displays the following:

  1. Heading/ track.
  2. Selected heading, course.
  3. Drift angle.
  4. Vertical deviation.
  5. Wind - speed / direction.
  6. DME distance.
  7. Distance to waypoint (DTW)/ estimate time of arrival (ETA).
  8. Active waypoint.
  9. MAP and Plan modes.
  10. GMT.
  11. VOR/ADF bearing and distance.
  12. VOR/LOC deviations.
  13. ADF bearing.
  14. To/From information.
  15. Ground speed.
  16. True airspeed.
  17. TCAS information.
  18. Weather radar.
  19. Course deviation or navigation map.
  20. Windshear/ predictive windshear.
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6
Q

pitot/static system

A

3 pitot tubes on nose CA,FO and AUX
rudder pitot tube
2 static plates on each side and 2 alternate
CA pitot static goes to ADIRU-1 FO goes to ADIRU-2 alternative goes to ISIS(integrated standby Instrument System)

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7
Q

IRS functions and controls

A

ADIRU air data and inertial info to the PFD and ND
single IRS control panel located on the overhead panel controls ADIRUs
backup batter for ADIRU-2 30 min
airplane battery powers ADIRU-1

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8
Q

NAV OFF light

A

1) ADIRU is off
2) in align mode
3) primary ADIRU failure

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9
Q

NAV OFF flashes amber

A

does not receive PP within 5 to 10 min,

PP entry fails the comparison test with either stored or calculated position

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10
Q

Mode Selector

A

OFF- turns ADIRU off
NAV- normal position after power up normal starts automatically Align mode takes 10min if PP initialization has been done
3 min fast realignment is done by cycling NAV to OFF to NAV within 5 seconds initialized with existing attitude and heading

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11
Q

VOR’s tuned

A

automatically by the VIA versatile integrated avionics unit
ID’s of VOR’s currently providing data are displayed on the FMS POS REF 2/3
ND automatically displays the ID/freq of the tuned VOR’s

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12
Q

Manual tuning on the FMS NAV RADIO

A

Manual tuning on FMS NAV RADIO page

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13
Q

Radio Altimeter system operation

A

provide terrain clearance data 2500 feet 2 radio altimeter receiver/transmitter and antennas

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14
Q

ISIS

A

provides altitude ,airspeed,attitude and baro settings on LCD

 Pushing the ANNUN LT TEST button on the overhead panel displays
ALIGN, ATT FAIL messages, and all red diagonal crosses overlay the
displays.
 The airplane battery will power the system if the electrical power is lost.
1. ALIGN Button
Push - Resets attitude display. Airplane should be in level flight.
2. BARO Set Knob
Sets barometric pressure display in inches of mercury and
hectopascals
3. ISIS Knob
Rotate - Adjusts ISIS LCD brightness. The LCD will illuminate
full bright automatically during electrical failure.

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15
Q

where is standby Mag compass and light switch

A

Standy mag compass above behind FO
Viewing mirrors on the glare shield
light switch lower right hand corner of overhead panel

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16
Q

Understand function of the FMS

A

FMS consists of FMF1 and 2 provided by VIA’s and 2 MCDU’s
pilot uses FCP to select flight modes and the multifunction control display unit to enter flight plans and other flight data flight progress monitored through MCDU
After data entry the FMF’s generate a flight profile from origin to destination airport

17
Q

know mcdi functions and basic ops

A

Light Sensor
 Senses ambient light and automatically adjust reference brightness
level.
1. Line Select Key
 Push - Provides for the entry, selection, or deletion of information on an
adjacent line.
 Entry - Moves information to a selected line from scratchpad.
 Selection - Selects a page, procedure, or performance mode as
required. Moves information to scratchpad from selected line when the
scratchpad is blank.
 Deletes information from the selected line when DELETE is displayed
in the scratchpad.
2. BRT Knob
 Rotate - Manually adjusts brightness of CRT display.
3. Alpha/Numeric Keys
 Push - Enters selected character into the scratchpad.
4. Miscellaneous Keys
 CLR Key - Push to clear data in the scratchpad.
 “/” Key - Used as a data separator.
 SP Key - Not used.
5. Message Light
 MSG - Illuminates when the FMS generates a message displayed in
the scratchpad.
 OFST - Illuminates when the airplane is flying a parallel offset of the
active flight plan.
 DSPY - Illuminates when the current display is not related to the active
flight plan leg or current performance mode.
 FAIL - Illuminates when the MCDU has stopped6. Function Keys
 DIR INTC
 NAV RAD - Selects NAV RADIO page for tuning VOR, ADF, and ILS.
 PERF -
 INIT -.
 TO/APPR -
 F-PLN -
 PROG -
 FIX -
 SEC F-PLN -
 REF
ENG OUT
Menu
Page
ATC
Up/Down
f-pln init

18
Q

how to operated the EIS control

A
  1. MINIMUMS Knob
     RA - Sets RA bug on PFD altitude tape by rotating the inner collar.
     BARO - Sets BARO bug on PFD altitude tape by rotating the inner
    collar.
     Push - Resets PFD DH alert and silences the aural warning.
  2. MAP Switch
     Push - Selects MAP display on ND. Non-flight plan waypoints, airports,
    navaids, weather radar data and bearing pointers are displayed.
  3. MAG/TRUE Button
     Push - Selects MAG or TRUE reference for heading/track indicator on
    the ND MAP display.
  4. VOR Switch
     Push - Selects VOR display on ND.
  5. TCAS Switch
     Push - Selects dedicated TCAS display on ND with 10 NM auto range
    and 2 NM range ring.5. TCAS Switch
     Push - Selects dedicated TCAS display on ND with 10 NM auto range
    and 2 NM range ring.
  6. BAROSET Knob
     QFE/QNH - Selects altitude above station (QFE) or altitude above sea
    level(QNH) by rotating inner collar. Value is displayed on PFD.
     Pull - Selects standard baroset (29.92 or 1013.2 Hp). Value is displayed
    on PFD.
  7. IN/HP Button
     Push - Changes BAROSET value in inches of mercury or hectopascals.
  8. INCR/DECR Switch
     Push - Controls MAP range from 10 to 640 NM on ND.
  9. VOR/ADF Switches
     Push - Controls bearing pointer display on ND.
  10. ARPT Switch Push - Selects non-flight plan airports normally not displayed on ND.
  11. VOR/NDB Switch
     Push - Selects display of non-tuned VORs, DMEs, VOR/DMEs, or nondirectional
    beacons on ND. Tuned stations are not deselectable thru
    this switch.
  12. WPT Switch
     Push - Selects display of non-flight plan waypoints on ND.
  13. DATA Switch
     Push - Selects display of waypoint data on ND consisting of an
    identifier, crosstrack deviation, and waypoint constraint data.
  14. APPR Switch
     Push - Selects APPROACH mode display on ND.
  15. TRFC Switch
     Push - Selects full time TCAS display on ND.
  16. PLAN Switch
     Push - Selects PLAN mode display on ND.17. WX/TERR Switch
     Rotate - Adjusts weather radar display brightness.
     Push - Turns on/off weather radar display. EGPWS terrain is displayed
    when weather radar is not selected.
19
Q

different displays available on EIS control panel

A
  1. BRT Knob
     Rotate - Adjusts respective DU brightness. Turning fully
    counterclockwise through a detent turns off respective DU.
  2. ND Switch
     Push - With 1 or more DUs inoperative, causes the existing SD to
    become an ND.
  3. CONSEQ/STATUS/MISC Switch
     Push - Displays respective CONSEQUENCE, STATUS,
    or MISCELLANEOUS page on SD.
  4. System Cue Switch (6)
     Push - Displays applicable system (ENGINE, HYDRAULIC,
    ELECTRIC, AIR, FUEL or CONFIGURATION) synoptic page on SD.
20
Q

Source Input control panel

A
  1. AIR DATA Switch
     Push - Selects off-side ADIRU source for DUs. Switch illuminates
    amber.
     Pushing again restores normal, on-side ADIRU sources.
  2. IRS Switch
     Push - Selects off-side IRS. Switch illuminates amber. IRS 2 or IRS
    AUX message is displayed on the PFD.
     Pushing again restores normal, on-side IRS.
  3. FLT MGT Switch
     Push - Selects off-side FMS source for DUs. Switch illuminates amber.
     Pushing again restores normal, on-side FMS sources.
  4. VOR/APPR Switch
     Push - Selects off-side radio system. Switch illuminates amber.
     Pushing again - restores normal, on-side radio sources.
  5. EIS SOURCE Selector
     1 - Normal position for Captain’s side.
     2 - Captain uses VIA-2 output for EIS. CAPT ON 2 light illuminates
    amber. If First Officer’s selection is 1, F/O ON 1 light will illuminate
    amber.

Boeing 717 (20 decks)

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