HHH ATA 26-30

HHH ATA 26-30

Professional Development

108 Qs

quiz-placeholder

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HHH ATA 26-30

HHH ATA 26-30

Assessment

Quiz

Science

Professional Development

Easy

Created by

Ha Hoang

Used 1+ times

FREE Resource

108 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The Engine and APU fire protection is done by two sub- systems, they are:

The Fire detection and the Fire extinguishing system.

The Fire detection and the Firefighting system.

The Fire detection and the Fire eliminating system.

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The Fire Detection Unit (FDU) monitors the:

FDU 1 and FDU 2 monitor Engine loops no 1 and APU.

FDU 1 for Engine No.1 and FDU 2 for Engine No.2.

FDU 2 for Engine No1, Engine No 2 and APU.

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The Fire Detection Units (FDU) sends the FIRE and FAULT signals to the:

Flight Warning Computer (FWC).

Cabin Intercommunication Data System (CIDS).

System Data Acquisition Concentrator (SDAC)

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In CEO and NEO aircraft the OVHD (20VU) guarded red FIRE P/B are used to:

Isolate the related systems.

The Engine or APU will shut down.

Isolate the related system, shut down the related system and also arms the extinguishing system.

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Each engine has two fire bottles installed in the pylon and discharge of each bottle is controlled by:

Related red guarded P/B SW.

Related AGENT P/B SW.

Related TEST P/B SW.

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

On ground an APU fire will cause an:

Automatic shutdown of the APU only.

Automatic discharge of the fire bottle only.

Automatic shut down and Auto discharge of the bottle.

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The Avionics Smoke Detection controlled and monitored by:

Avionics Equipment Ventilation Controller (AEVC)

Fire Detection Unit (FDU)

Dedicated fire bottle.

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