Chapter 6: Cockpit Electronics Flashcards

1
Q

what does electronic flight instrument system (EFIS) consist of?

A

upper: electronic attitude and direction indicator (EADI)

lower: electronic horizontal situation indicator (EHSI)

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2
Q

what does EADI screen display?

A

attitude in pitch and roll

flight director bars, ILS glideslope, localiser deviation

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3
Q

at what height will EADI display radio altitude in digital/analog format?

A

digital: 1000 - 2500 ft

analog: below 1000ft

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4
Q

colour code for display feature of EADI

A

warning - red
caution - amber
earth - brown
sky - blue
engaged modes - green
ILS deviation pointer - purple
flight bar - purple/green

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5
Q

colour code for precipitation im mm/hr

A

black: 0 - 1
green: 1 - 4
yellow: 4 - 12
red: 12 - 50
purple: above 50

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6
Q

colour code for turbulence

A

white

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7
Q

what does a electronic horizontal situation indicator do?

A

display flight navigational information, 9 modes

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8
Q

modes of EHSI

A

1) map
2) ctr map
3) plan
4) full VOR/ILS
5) exp VOR/ILS
6) exp nav/full nav

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9
Q

what is EICAS?

A

engine indication & crew alerting system

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10
Q

what does the EICAS display on both upper and lower screen?

A

upper screen: primary display (EPR, N1, EGT)

lower: secondary display (abnormal engine ops)

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11
Q

2 page of the EICAS

A

operational page: during flight

maintenance page: for fixing, only on ground

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12
Q

what is ARINC?

A

aeronautical radio incorporated

provide standard guidelines for electronic systems

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13
Q

2 common data bus standard of ARINC

A

ARINC 429 & 629

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14
Q

what is BITE?

A

built in test equipment

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15
Q

purpose of BITE

A

provide fault detection/isolation & operational verification after defect repair

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16
Q

how does BITE work?

A

defect sensed > sends control signal to isolate defect

17
Q

systems that BITE works on

A

EICAS
VHF & HF comms radio
altimeter
transponder

18
Q

operating modes for electronic centralised aircraft monitoring (ECAM)

A

normal, advisory, failure, manual

19
Q

what is FMS?

A

flight management system

20
Q

purpose of FMS

A

reduce crew workload, achieve best fuel economy

21
Q

what does the FMS do?

A

guides the aircraft navigation vertically & laterally to achieve planned altitude

22
Q

what does the FMS need to operate?

A

navigational data from systems like VOR ILS DME

23
Q

how does the flight crew link with the FMS?

A

control display unit (CDU)

24
Q

what does the CDU consist of?

A

1) screen
2) line select keys
3) annuciators
4) alpha-numeric numbers
5) function and mode keys