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A+ general familiarization > chapter 00/31 > Flashcards

chapter 00/31 Flashcards

1
Q

A321 seat count

A

190

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2
Q

A320 seat count

A

150

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3
Q

The A321 is an A320 with

A

two extra fuselage sections and room for 36 more customers

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4
Q

A319 seat count

A

124

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5
Q

Which A320 variation has the best fuel economy

A

A319

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6
Q

The A320 has a Maximum Take-Off Weight of

A

3600 Nm

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7
Q

The A321 has a Maximum Take-Off Weight of

A

3100 Nm

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8
Q

The A319 has a Maximum Take-Off Weight of

A

4200 Nm

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9
Q

For the vertical stabilizer the reference station is

A

Z = 0

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10
Q

FUSELAGE
The station (STA) number is the distance in millimeters of the
cross-section from a reference point. The reference

A

X = 0

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11
Q

For the horizontal stabilizer the reference station is

A

Y = 0

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12
Q

WING
For wings, the reference station is the wing reference axis that is
located at

A

1868 millimeters (73.54 in) from the aircraft X-axis

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13
Q

The controls of most aircraft systems are located on the

A

overhead panel.

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14
Q

The overhead panel is divided into two main sections:

A

a FWD section including the system panels
an AFT section including mainly the circuit breaker panel.

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15
Q

FCU stands for

A

Flight Control unit

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16
Q

AFS stands for

A

Automatic Flight System

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17
Q

ISIS stands for

A

Integrated Standby instrument system

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18
Q

ECAM stands for

A

Electronic Centralized Aircraft Monitor

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19
Q

MCDU Stands for

A

Multipurpose Control Display Units

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20
Q

Do all airbus have the same door placement ?

A

yes

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21
Q

MTOW stands for

A

Maximum take off Weight

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22
Q

AMM Stands for

A

Aircraft Maintenance Manual

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23
Q

MRO stands for

A

Maintenance Repair Organization

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24
Q

ECP stands for

A

ECAM control panel

25
Q

EFIS stands for

A

Electronic Flight Instrument System

26
Q

The Single Aisle aircraft cockpit instrumentation information is displayed
on how many units ?

27
Q

The EIS(electronic instrument system) is separated into two subsystems:

A
  • Electronic Flight Instrument System (EFIS),
  • Electronic Centralized Aircraft Monitoring (ECAM)
28
Q

DMC 1 supplies

A

both ECAM displays

29
Q

DMC 2 and 3 are available as

A

a backup for Ecam display

30
Q

The Flight Warning Computers (FWCs), heart of the ECAM system,
receive data from:
- the A/C systems to generate

A

Red Warnings

31
Q

FWC Stands for

A

Flight Warning computers

32
Q

The Flight Warning Computers (FWCs), heart of the ECAM system,
receive data from:
- the SDACs to generate

A

Amber Cautions

33
Q

The FWCs then supply:

A

the DMCs for the display of alert messages,
- the attention getters,
- the loudspeakers with aural alerts and synthetic voice messages

34
Q

DMC 1 supplies both ECAM displays and DMC 2 is
also a backup for

A

ECAM displays

35
Q

SDAC stand for

A

System Data Acquisition concentrators

36
Q

The System Data Acquisition Concentrators (SDACs) receive data
from the A/C systems and sends it to the_________________ for display on the_________

A

Display Management
Computers (DMCs)

ECAM display units.

37
Q

Flight parameters are displayed on the

A

PFDs (Primary Flight Display)

38
Q

PFD stands for

A

Primary Flight Display

39
Q

ND stands for

A

Navigation Display

40
Q

e navigation data is
displayed on the

A

NDs (Navigation Display)

41
Q

Outboard of the PFDs, there are control knobs to adjust the _________ of the associated PFD and ND, and to

A

adjust the brightness
turn the displays off.

42
Q

Two EFIS control panels are used to select what is displayed on the

A

EFIS screens

43
Q

(UTC) Stands For

A

Universal Time Coordinated

44
Q

(CFDIU) Stands for

A

Centralized Fault Display Interface Unit

45
Q

A BITE Is

A

A bit (binary digit)

the smallest unit of data that a computer can process and store

46
Q

The SYSTEM
REPORT/TEST function is available on

A

On Ground only

47
Q

PFR stands for

A

Post Flight Record

48
Q

is a ground-based software dedicated to the identification and
the management of unscheduled maintenance.

49
Q

is the main communication means for aircraft
operational staff. It enables the flight crew and the technical staff to
be aware of the aircraft status, to enter aircraft defect and to report
maintenance and servicing actions

50
Q

The Flight Data Interface and Management Unit (FDIMU) has two
primary functions. The first of which is the

A

Flight Data Interface Unit
(FDIU) function

51
Q

FDIMU stands for

A

Flight Data Interface and Management Unit

52
Q

The main functions of the Aircraft Integrated Data System (AIDS) are
to

A

monitor engine condition, APU condition and A/C performance, and
to provide trouble shooting assistance

53
Q

The second main function of the
FDIMU is the

A

DMU function which houses the Aircraft Integrated Data
System (AIDS).

54
Q

FDIU stands for

A

Flight Data Interface Unit

55
Q

DMU stands for

A

Data Management Unit

56
Q

The Data Management Unit (DMU) is the heart of the

A

(AIDS)Aircraft Integrated Data
System

57
Q

AIDS stand for

A

Aircraft Integrated Data
System

58
Q

The EIS and the Centralized Fault Display System (CFDS) computers
are located in the

A

aft avionics rack.

59
Q

SSFDR stands for

A

Solid State Flight Data Recorder

A+ general familiarization (4 decks)

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