Indicating and Recording Flashcards

1
Q

Electronic Instrument System EIS comprised by:

A

6 Display Units DUs. DUs full cathode raytubes and identical

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2
Q

Electronic Instrument System EIS:

A

Electronic Flight Instrument System EFIS; Electronic Centralized Aircraft Monitor ECAM

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3
Q

ECAM comprised by:

A

Engine / Warning Display E/WD; System Display SD

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4
Q

Display Management Computers – 3. Sensors:

A

NAV Data/ ADIRS data – DMC 1,2,3

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5
Q

Each DMC has

A

2 independent channels

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6
Q

2 identical FWCs :

A

Red warnings, amber cautions, alert messages, memos, aural alerts, synthetic voice messages

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7
Q

ECAM/ND XFR: allows ECAM system display to be shown on

A

Either the Captain’s or FO’s ND

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8
Q

DMC sw in AUTO:

A

DMC3 supplies data for both ECAM DUs

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9
Q

Pulling barometric knob will set

A

QNH pressure

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10
Q

Flight data recording system:

A

Flight data interface and management unit, digital flight data recorder DFDR, linear accelerometer LA

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11
Q

Digital Flight Data Recorder DFDR -

A

25h, underwater locator beacom

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12
Q

If PFD – if bank angle exceeds 45º, all PFD symbols disappear, except for

A

Attitude, speed, heading, altitude, and vertical speed

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13
Q

Between 30º up and 10º down, markers set every

A

2,5º

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14
Q

Pitch attitude and roll angle protection symbols represent max bank

A

67º and max pitch 30ºup and 15ºdown

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15
Q

Side slip blue if EO, config 1, 1+F, 2,3, or full (beta target) >1.3 EPR or difference ENG EPR

A

> .25

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16
Q

Airspeed scale- speed trend arrow – predicted speed in

A

10 sec (at constant rate); pointer appears if rate of change >2kt; pointer disappears if rate of change < 1kt or FMGC fail

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17
Q

Blue triangle = selected speed from FCU

A

Magenta triangle -

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18
Q

Managed speed

A

Green Mach number when current speed > M 0.5

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19
Q

Speed protection symbol VMO +4kt / MMO +

A

0.006 overspeed

20
Q

VLS – minimum selectable speed – top of amber strip -

A

Indication 1 sec after airborn – disappears upon touchdown

21
Q

Alpha protection speed =

A

Top of black and amber strip along speed scale. AOA= Alpha protection active

22
Q

Alpha protection speed =

A

Top of black and amber strip along speed scale. AOA= Alpha protection active

23
Q

Alpha Max Speed = top of red strip along speed scale=

A

speed maximum AOA acft in pitch normal law

24
Q

VMAX = the lowest of

A

VMO, MMO, VLE, VFE

25
Q

Vsw – stall warning only in

A

Pitch alternate / pitch direct law – top of red and black strip

26
Q

PFD symbols – 1=V1 / 0=

A

VR /

27
Q

VFE max = bottom of

A

Red and black strip

28
Q

VFE orange = VFE next – only

A

Below 20,000ft

29
Q

S speed = flap in

A

position 1

30
Q

0 green =

A

Flap in position 1

31
Q

0 green = green dot= best

A

Lift-to-drag ratio. It appears when acft in clean configuration

32
Q

Managed DES speed =

A

Upper speed range

33
Q

Acft flies in this range for profile =

A

Managed target / lower speed range

34
Q

Altitude display pulses if

A

Acft below transient level alt not selected; acft above trans alt knob not set; acft below 2,500ft if transition level not available

35
Q

Vertical deviation circle – also on PROG MCDU – displayed from

A

TOD to MAPT altitude

36
Q

Brown horizontal landing elevation (at destination) shown from

A

800ft radio alt until 80kt decelerating if QNH is selected

37
Q

Ground reference Ribbon – LFE -

A

<570 ft radio alt

38
Q

Vertical speed scale – first inertial data – should it fail -

A

Barometric source

39
Q

Bird = FPV -

A

HDG / TRK / VS FPA selected

40
Q

FPA = difference between

A

Horizon and FPV

41
Q

When will Flt Director bars flash for 10 sec and remain steady?

A

Reversion manual/auto – HDG / VS; capture selected flt level already ALT capture; loss of LOC or GS in LAND mode at first AP/FD engangement

42
Q

Localizer and Glide Slope deviation scales:

A

Displayed as soon as LS is pressed

43
Q

Grid track – when switch in true reference and latitude

A

> 65º north or < 65ºsouth

44
Q

CSTR pb on -

A

FL MORA displayed

45
Q

ILS APP message on ND:

A

“ILS on MCDU and FMS flight phase in DES, APPR, GO AROUND

FMS phase CRZ <250NM”

46
Q

Windshier in Auto for

A

Protection

47
Q

Engine thrust is constant and speed is controlled by

A

Varying the aircraft pitch attitude.