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D0228NG conversion > FMS > Flashcards

FMS Flashcards

1
Q

What reference datum does the FMS use?

A

WGS-84

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2
Q

what 5 PBN requirements does the FMS satisfy?

A
  1. P-RNAV
  2. B-RNAV
  3. GNSS
  4. SBAS
  5. OCEANIC/REMOTE
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3
Q

in what FMS mode can we fly autopilot coupled non-precision approaches?

A

approach mode

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4
Q

what 3 components make up the basic FMS?

A
  • pedestal mounted control display unit with integrated nav computer
  • configuration module
  • solid state data transfer unit
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5
Q

where does the FMS accept position information from?

A
  • LRN sensors
  • DME
  • VOR
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6
Q

how are flight plans created?

A

using the navigation database which locates waypoints along a route and combines them to form a flight plan

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7
Q

what 8 things does the FMS’s nav database provide info on?

A
  1. navaids
  2. airports
  3. NDB
  4. enroute waypoints
  5. intersections
  6. airways
  7. SIDs
  8. STARs
  9. approaches
  10. runways
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8
Q

what 8 systems does the navigation computer interface with?

A
  • RCU’s
  • AHRS’s
  • ADC
  • DME’s
  • TAWS
  • DCU
  • NAV 1
  • SSDTU
  • fuel flow sensors
  • WOW sensors
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9
Q

what 5 sensors does the navigation computer process data from?

A
  1. DME
  2. VOR
  3. air data
  4. fuel flow
  5. up to 5 LRN sensors
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10
Q

what does the nav database have the capacity to store?

A
  • 200 pilot defined locations
  • 200 pilot defined routes
  • 100 (each) pilot defined alignment points, airports approaches, and runways
  • 100 average sized SIDS/STARS
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11
Q

how does the FMS determine position using DME?

A
  • determines which DME stations are within 300 mile range
  • sequentially tunes each of those stations
  • interrogates each station, corrects distance for slant range using station elevation and aircraft altitude
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12
Q

where does the FMS derive the TAS from?

A

ADC

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13
Q

where does the FMS derive velocity information from?

A

GPS sensor

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14
Q

where does the FMS derive position information from?

A

GPS, DME, VOR

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15
Q

what does the FMS rely on for position information if out of DME range?

A

LRN sensors

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16
Q

what secondary navigational functions are available once the best computed position is obtained?

A
  • course to waypoint
  • ETA
  • distance to waypoint
  • wind
  • groundspeed
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17
Q

what is the configuration module?

A

serially connected EEPROM designed to store config data specific to the aircraft installation

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18
Q

what is the solid state data transfer unit used for?

A

to load nav database revision cycles, TAWS, flight plans and other updates

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19
Q

where is the SSDTU located?

A

service panel on the RH avionics rack

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20
Q

how is the navigation database update provided?

A

on disks directly from universal on a 28 day revision cycle

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21
Q

what does the fuel management function of the FMS accept inputs from?

A

aircraft fuel flow sensors and information supplied by the pilot

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22
Q

is the fuel calculation reliable in fuel flow data mode if one fuel flow sensor fails?

A

no, the calculation is based on 2 fuel flow sensors

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23
Q

what will be displayed on the FMS if an engine is shut down/fails or a fuel flow sensor failure occurs?

A

FUEL FLOW FAIL MESSAGE

digital fuel flow readout will read FAIL on the fuel flow page for the respective engine/fuel flow sensor

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24
Q

what action should we take with regard to the FMS in case of an engine failure?

A

select the FAIL indication and press BACK and ENTER button

this makes sure the fuel calculation takes again the value of the fuel flow sensor in case the engine is restarted

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25
Q

if the fuel flow sensor has failed what should the pilot manually enter for the failed sensor?

A

a reasonable fuel flow value in place of the word FAIL

this will restart fuel calculation and related estimates for the remainder of the trip with the correct values

26
Q

what should we refer to if there is a DATABASE EXPIRED warning on power up?

A

user manual

27
Q

what does an amber MSG annunciation mean?

A

message is to be acknowledged on the MSG page

28
Q

what does a WPT alert mean?

A

steady: lateral waypoint alert
flashing: vertical waypoint flight path angle alert

29
Q

what does a SXTK annunciation mean?

A

FMS in selected crosstrack mode

30
Q

what does FMS HDG annunciation mean?

A

FMS is in HDG mode

31
Q

what does FMS APPR annunciation mean?

A

FMS is in APPR mode

32
Q

what does LNAV annunciation mean?

A

LNAV level of service for SBAS approach is retained

33
Q

what does LNAV/VNAV annunciation mean?

A

LNAV/VNAV level of service for SBAS approach is retained

34
Q

what does LPV annunciation mean?

A

LPV level of service for SBAS approach is retained

35
Q

what does an amber GPS INTEG annunciation mean?

A

RAIM not available or a fault is detected- DME may still be in use

36
Q

what does an amber POS annunciation mean

A

FMS position uncertain alert

37
Q

what does an amber DR annunciation mean?

A

FMS in dead reckoning mode

38
Q

when a valid navigation leg is selected on the FMS, guidance info can be selected for display on the PFD how?

A

selecting FMS with the NAV/BRG SOURCE button o n the PFDCP on the pedestal panel

39
Q

what is 2 dot deflection laterally in en-route mode?

A

5nm

40
Q

what is 2 dot deflection vertically in en-route mode?

A

1500ft

41
Q

what is 2 dot deflection laterally in terminal mode?

A

1nm

42
Q

what is 2 dot deflection vertically in terminal mode?

A

500ft

43
Q

what is 2 dot deflection laterally in approach mode?

A

2 degrees to 0.3nm, then linear

44
Q

what is 2 dot deflection vertically in approach mode?

A

0.25 x glide path angle

45
Q

when a valid navigation leg is selected on the FMS, how can FD lateral steering be selected?

A

LRN button on LH annunciator panel

46
Q

in what plane is steering provided by the FMS in enroute?

A

lateral steering only

an appropriate vertical mode on the autopilot can be selected

47
Q

how do we link approaches into the flight plan and laterally and vertically couple the autopilot?

A

selecting approach mode on the autopilot

48
Q

what waypoints can b used as an approach point to land?

A

any

49
Q

when will an approach automatically activate?

A

with approach mode armed, the aircraft track angle within 15 degrees of the final approach course and the aircraft being within 2nm of FAF

(latter applies for approaches without capture fix only)

50
Q

how do we manually activate an approach using the FMS?

A

from any nav page LSK 3R and ACT APPR

51
Q

what 3 things happen when an approach is manually activated on the FMS?

A
  1. all intervening waypoints from the present FR-TO leg to the first approach waypoint will be sequenced and HSI guidance will be to that waypoint
  2. desired track pointer will be set to the inbound course of the approach
  3. FMS will transition to HDG mode, and the pilot must manually set up the correct approach intercept angle. (normally coincides with ATC vectors)
52
Q

if an approach has been manually activated, what must the pilot do once the intercept angle onto the FAT has been established?

A

press intercept LSK on NAV page 1 to allow interception of the final approach course

53
Q

when is vertical navigation provided?

A

only with FMS in APPR mode

54
Q

is enroute vertical deviation info fed to the FD?

A

no, it is advisory only

55
Q

what is the LPV monitor?

A

an LRU in the LH avionics rack which incorporates a second GPS/SBAS receiver which acts as an additional navigation sensor input the FMS

56
Q

What does the LPV monitor provide with regard to an LPV SBAS approach?

A

the necessary integrity monitoring during the final approach segment

57
Q

what 2 pieces of equipment make it possible to fly SBAS approaches to LPV minima?

A

LP/LPV monitor and the FMS

58
Q

what is correct operation of the LPV monitor indicated by?

A

LOS (level of service) annunciation on the PFD when an LPV approach is selected and armed.

59
Q

what colour is the LPV output on the PFD?

A

Green, this also means LPV LOS is retained

60
Q

what if we lose LPV LOS?

A

FMS MSG annunciator is triggered

61
Q

what if predicted LOS is not available at approach activation?

A

message will alert the pilot that predicted LOS will be unavailable after crossing the FAF although the RNV APPR LOS page may show that it is in use.

a lower LOS should be selected

62
Q

if predicted LOS is not available and selection of a lower LOS is not possible before crossing FAF what happens?

A

no vertical guidance is available and the approach must continue LNAV only

D0228NG conversion (12 decks)

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