BITE Flashcards

1
Q

BITE systems came into practical use with the invention of:

A

digital electronic systems.

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2
Q

Second generation of self-diagnostics equipment incorporates the use of:

A

a centralized monitoring system.

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3
Q

The built-in troubleshooting system on the Boeing aircraft is known as:

A

Central Maintenance Computer System (CMCS)

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4
Q

The Airbus A320 Family aircraft system is called the:

A

Centralized Fault Display System (CFDS)

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5
Q

Third generation BITE systems have become more integrated and allow for:

A

wireless communications of troubleshooting data.

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6
Q

Aircraft like the Boeing 787 and the Airbus A350 can monitor systems, analyze faults, and automatically download maintenance information through the use of:

A

wireless systems such as Local Area Network (LAN), airborne cellular or satellite technologies.

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7
Q

BITE is designed to provide:

A

detection, isolation and operational verification.

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8
Q

The Boeing 757 and 767 aircraft utilizes built-in test equipment on approximately
____ LRUs.

A

50

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9
Q

Simple BITE system may incorporate a go/no-go red or green LED, or a simple two character alphanumeric LED display on:

A

the front of each of the individual LRU’s in the Electronic & Equipment Bay (E&E bay).

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10
Q

More complex systems
use a multi-character
display and monitor
known as a
_____ ______ _____ ______ and is capable of monitoring more than
one LRU at a time.

A

Maintenance Control
Display Panel (MCDP)

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11
Q

The MCDP can be accessed from the:

A

electrical equipment bay or the flight deck using a carry-on unit.

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12
Q

The MCDP can store fault data for up to ___ previous flights.

A

ten

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13
Q

The MCDP monitors what?

A

the flight control computers, flight management computers, and the thrust management computers.

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14
Q

Even more advanced BITE systems incorporate displays activated from the flight deck and may have a means to transmit data from:

A

the aircraft to the ground facility via ACARS.

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15
Q

The _______ ______ ______ ______ is not considered a BITE system, but it is a manager of the individual built in test equipment of the various LRUs located throughout the aircraft.

A

Central Maintenance Computer System (CMCS)

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16
Q

The B-747-400 CMCS is accessed through:

A

one of four control display units (CDUs).

17
Q

Up to ____ faults can be stored in the CMC memory.

A

500

18
Q

From these detected faults, a selection from _____ different fault messages may be displayed on the CDU depending on the system that faulted.

A

6,500

19
Q

There are two CMC’s, Each CMC weights about 17 pounds and has a ____-pin connector on the rear of the unit.

A

300

20
Q

The CMCs are _______ ______ sensitive so the technician must always take the necessary precautions during maintenance.

A

Electrostatic Discharge (ESD)

21
Q

Airbus A320 Family uses the ____ ____ ____ ____ for fault isolation and system analysis.”

A

Centralized Fault Display System (CFDS)

22
Q

The A320 series aircraft CDS utilizes a ____ ____ ____ _____ to input commands, monitor replies, and access fault data of the CFDS

A

Multipurpose Control Display Unit (MCDU)

23
Q

The MCDU is nearly identical to the:

A

CDU used on the Boeing aircraft.

24
Q

There is only one ______ on the A320 series aircraft.

A

CFDIU