5.1 Electronic Instrument Systems Flashcards

1
Q

the earliest air speed indicator (ASI) consisted of what

A

a flexible bamboo strip

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2
Q

what period saw major advancements in instrumentation

A

WW1 and the first air mail delivery in the 1920’s

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3
Q

instrumentation in an aircraft provides what

A

information about its position and speed

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4
Q

the front instrument panel contains what

A

all instruments needed to fly the aircraft safely and is positioned directly in the pilots eye line

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5
Q

basic six arrangement (instruments) create a “picture” of an aircrafts flight condition

A
  • Airspeed Indicator
  • Attitude Director Indicator (ADI)
  • Altimeter
  • Turn & Bank Indicator or Coordinator
  • Horizontal Situation Indicator (HSI)
  • Vertical Speed Indicator
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6
Q

the basic T instrument layout makes the dials easy to read and helps the pilot to establish the aircraft’s attitude and position

A

.

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7
Q

all aircraft instrument layouts conform to standards set by who

A

ICAO

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8
Q

There are four key indicators in the T arrangement, they are

A

Airspeed Indicator
Attitude Direction Indicator (ADI)
Altimeter
Horizontal Situation Indicator (HSI)

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9
Q

electronic Instrument Systems (EIS) have many advantages over their analogue predecessors including

A

exchange of images between units in the case of display failure. removal of “clutter” on screen

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10
Q

some other advantages of EIS over analogue include

A
  • Coloured displays
  • fewer components are needed
  • all display units for EIS are the same type
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11
Q

there are many different EIS, including

A

Electronic Flight Instrument System (EFIS)
Engine Indicating and Crew Alerting System (EICAS)
Electronic Centralised Aircraft Monitoring (ECAM)

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12
Q

displays are interchangeable, which improves

A

redundancy

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13
Q

Required data is transmitted digitally by ARINC 429 buses:

A

Via display data buses to CPU-controlled CRT or LCD
Via digital data buses to a printer for a hard-copy printout
In digital form to a radio transmitter, which sends data to a ground receiver

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14
Q

calculations in the system are made by what

A

CPU (central processing unit)

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15
Q

electronic units are interconnected by what

A

digital data buses

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16
Q

Reading the indication in bright sunlight used to be more difficult on Engine Instrument Display System (EIDS) monitors than on analogue indicators. what was the solution to this ?

A

brighter, more modern displays

17
Q

the EFIS displays are controlled by what panels

A

EFIS control panels and lighting/loudspeaker control panels

18
Q

(GGs) graphics generators transmit video signals to what

A

display units (DUs)

19
Q

(SSPs) source select panels and centre display control panel supply what

A

additional controls for the display system

20
Q

a modern electronic attitude and direction indicator (EADI) displays

A

Pitch and roll information
Ground speed
Airspeed
Flight director information
Glide slope and localiser deviation
Numerous warning and status message

21
Q

the numerous warning and status messages displayed on EADI include

A

pitch and roll mode
navigation aid selected
radio altitude
altitude alert
decision height

22
Q

EHSI stands for

A

electronic horizontal situation indicator

23
Q

A modern EHSI presents a selectable and dynamic colour display of the aircraft’s position and heading in relation to the navigation aids around it

A

.

24
Q

Electronic horizontal situaton indicator
(EHSI)

EHSI items displayed include:

A

Magnetic heading
Radio steering commands for VOR or ILS
Way points, airports, and nav aids
Distance to go
ILS steering info

25
Q

EHSI can be switched by pilot to display either

A

a conventional full compass rose or just the portion of the compass rose ahead of the aircraft, commonly called the ARC or “SECTOR Display”.

26
Q

If an EHSI or EADI display fails

A

a composite mode on the remaining display shows combined elements of both displays

27
Q

Electronic Centralised Aircraft Monitor (ECAM) is a system used by who

A

Airbus
engine parameters need to be displayed continuously .
top display shows system status messages, warnings and corrective actions
lower screen shows pictorial diagrams of systems

28
Q

Engine Indicating and Crew Alerting System (EICAS) is a system used by who

A

BOEING
the lower screen is usually blank during normal flights
and the upper screen displays primary engine parameters

29
Q

in both EICAS and ECAM warnings are accompanied by

A

master warning lights
the two systems are becoming more alike on modern aircraft

30
Q

older aircraft used CRT for their displays and have now been supplemented by

A

LCD as they are brighter
Liquid crystal

31
Q

LCD have several advantages over CRT including

A

more robust
produce far less heat
require lower and simpler power supply
are brighter

32
Q

All EIS have brightness set initially by the pilot then they adjust automatically by

A

using photocells, to adapt to the ambient light levels in the cockpit

33
Q

An MCDU multi-function control display unit are used as

A

primarily as an interface between the pilot and the flight management system
they also act as an interface to the on-board maintenance system

34
Q

In case of total failure of the EIS what is implemented

A

a standby artificial horizon, airspeed indicator and altimeter are fitted in view of both pilots

35
Q

what does EIS use for its displays

A

Cathode ray tube (CRT)
and
Liquid crystal display (LCD)

36
Q

EIS allows manual transfer of displays

A

PFD with ND
secondary ECAM with ND