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ATA 26

Total questions: 20

Worksheet time: 10mins

Name
Class
Date
1.

APU fire in flight is normally extinguished?

a)

Manually from APU FIRE panel.

b)

Automatically by the FDU.

c)

Automatically when fire handle ispulled.

2.

APU fire on ground is normally extinguished:

a)

From APU FIRE panel.

b)

Automatically.

c)

From EXTERNAL POWER panel.

3.

Can you use the LH fire extinguisher bottlesfor RH engine fire?

a)

Yes.

b)

Yes, if two fire extinguisher bottles of RHengine have been discharged.

c)

No.

4.

Each engine fire loop comprises:

a)

Fan fire detector, core fire detector andpylon fire detector

b)

Fan fire detector and pylon fire detector

c)

Core fire detector only

5.

Engine loop A & B are connected to the FDU:

a)

Serial

b)

Parallel

c)

ARINC 429 bus

6.

In case of smoke detection, the smokedetector activates:

a)

GEN 1 LINE SMOKE, BLOWER FAULT andEXTRACT FAULT lights on.

b)

GEN 1 LINE SMOKE light on.

c)

BLOWER FAULT and EXTRACT FAULTlights on.

7.

Loop failure warning are sent to:

a)

ECAM and CFDS

b)

CFDS only

c)

ECAM and fire panel

8.

The A/C on ground, the APU fire warningsignals are sent to:

a)

ECAM, APU fire panel and externalpower control panel

b)

ECAM, APU fire panel

c)

APU fire panel and external powercontrol panel

9.

The DISCH light on engine fire panel comes onwhen:

a)

The agent has been discharged

b)

Engine fire PB is released out

c)

Fire is on the engine

10.

The fire extinguishing agent pressure ismonitored by:

a)

A pressure switch.

b)

A red light in the cockpit.

c)

A red disk on the pylon.

11.

The fire warning signals are sent to:

a)

ECAM, Engine fire panel and start control panel

b)

Engine fire panel and ECAM

c)

ECAM and start control panel

12.

The lavatory & cargo smoke detectors aremonitored by:

a)

FDU

b)

SDCU

c)

SDF function in CIDS director (enhanceaircraft)

13.

The lavatory fire protection is provided by:

a)

The lavatory automatic extinguishing.

b)

The lavatory smoke detection system.

c)

The lavatory smoke detection system and the waste bin automatic extinguishing.

14.

The number of APU fire detectors is:

a)

Three.

b)

Two, connected in parallel.

c)

Two, connected in serial.

15.

The Test PB on the engine fire panel checksthe integrity of the:

a)

Fire detection loops A & B, FDU,indications and warnings

b)

Squib circuit continuity

c)

Both A & B

16.

Thermal discharge of the APU bottle be detected:

a)

By the FDU.

b)

By the ECAM.

c)

By the red disc indicator.

17.

When the ENG FIRE PB is released out?

a)

Both Squib lights come on and A/C systems are isolated

b)

A/C system are isolated and Fire bottles discharge

c)

Fire bottles discharge

18.

Where is lavatory smoke detector located?

a)

In the ceiling panel, beside the air extraction duct

b)

In the waste bin

c)

In the air extraction duct

19.

Where is the Avionics smoke detectorinstalled?

a)

On the air extraction duct of the avionicsventilation system

b)

On the air inlet duct of the avionicsventilation system

c)

In the Avionics compartment ceiling

20.

Which warning lights are triggered in case ofan avionic smoke detection?

a)

GEN 1 LINE SMOKE light.

b)

BLOWER and EXTRACT FAULT lights.

c)

Both A & B.