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EMB-135BJ > Crew Alerting System > Flashcards

Crew Alerting System Flashcards

0
Q 
The Primary component of the avionics integration system is the:
A) IC-600
B) DAU
C) ADC
D) FADEC
A

A) IC-600

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1
Q

The crew alerting system includes the following components:
_____________ ___________
_____________ ___________
_____________ ___________

A 
2 - IC 600 (integrated computers)
2 - Data Acquisition Units
1 - Central Maintenance Computer (CMC)
5 - Cathode Ray Tubes (CRT)
2 - Radio Management Units (RMU)
1 - Aural Warning Unit (2 channels)
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2
Q

The No. 1 DAU provides data for the ______ engine and ______ airplane systems.

A

1

Forward

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3
Q

The No. 2 DAU provides data for the ______ engine and ______ airplane systems.

A

2

Aft

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4
Q

Which of the following is true regarding the DAU:

A) The DAU has only one channel
B) The DAU has two channels (A&B) that are fully redundant
C) The DAU has two channels (A&B) that are not fully redundant

A

C) The DAU has two channels (A&B) that are not fully redundant

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5
Q

Channel _____ of the DAU is the primary channel and channel _____ serves as the standby information source.

A

A

B

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6
Q

List the 5 CRT displays that provide information to the flight crew:

A

2 PFDs
2 MFDs
1 EICAS

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7
Q

The _________ can be used as a backup display to the main display panels.

A) EFIS
B) FMS
C) RMU
D) ADC

A

C) RMU

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8
Q

How many system pages can be displayed on the MFD?

A) 4
B) 5
C) 6
D) None

A

B) 5

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9
Q

The MFD can be used through the reversionary panel as a backup display for the _______ and the ________

A

PFD

EICAS

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10
Q

Upon powering up the aircraft, the MFD will present the:

A) Takeoff page
B) Electrical page
C) Hydraulic page
D) Fuel page

A

A) Takeoff page

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11
Q

What are the three levels of EICAS messages?
__________
__________
__________

A

Warnings

Cautions

Advisories

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12
Q

Which messages cannot be scrolled out of the screen?

A) Warnings
B) Cautions
C) Advisories
D) All of the above

A

A) Warnings

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13
Q

Advisory messages will automatically stop blinking after _____ seconds.

A

5

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14
Q

The number of messages that can be displayed at one time on the EICAS screen is ____.

A

15

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15
Q

The _____ is the primary flight instrument.

A

PFD

16
Q

Gear, flap and spoiler indications are presented on the _______.

A

EICAS

17
Q

A red “X” on the captain’s PFD, MFD, and EICAS is an indication of:

A) IC-600 #1 failure
B) IC-600 #2 failure
C) IRS failure
D) CRT failure

A

A) IC-600 #1 failure

18
Q

A red “X” on the first officer’s PFD and MFD is an indication of __________ failure.

A

IC-600 #2 failure

19
Q

A failure of only the first officer’s MFD screen is likely an indication of:

A) IC-600 #2 failure
B) ADC failure
C) CRT failure
D) IRS failure

A

C) CRT failure

20
Q

Selection of the ADC reversionary button is indicated by a _______ presentation on both PFDs.

A

ADC 1/2

21
Q

Selecting the IRS reversionary button is indicated by _______ and _______ presentation on the PFDs and a ______ presentation on the MFDs.

A

ATT 1/2

Mag 1/2

HDG 1/2

22
Q

List the 5 messages presented on the PFD and MFD when selecting the SG reversionary button.

A 
ATT 1/2
SG 1/2
ADC 1/2
Mag 1/2
HDG 1/2
23
Q

The _________ display gives analogue engine indications and some system parameters, including flap, landing gear, spoilers, and trim positions, fuel quantity, APU information, and pressurization information

A

EICAS

24
Q

List the conditions that will activate a takeoff configuration warning when the takeoff config button is pressed:

A 
Flaps out of position
Parking Brake Set
T/O Performance not set
Pitch Trim set out of limits
Spoiler Position
25
Q

Takeoff inhibition logic is in effect from V1 minus ______ knots accelerating and lasts until climbing above a radio altitude of _____ feet. During approach, the landing inhibition logic begins when the aircraft descends below a radio altitude of _____ feet and ends when the aircraft is on the ground for ____ seconds or more or after 1 minute.

A

15

400

200

3

26
Q

The Aural Warning Unit (AWU) has:

A) One channel
B) Two channels
C) Two main channels and one backup channel

A

B) Two channels

27
Q

The AWU is powered by one _________ bus and one _______ DC bus.

A

Essential

Main

EMB-135BJ (32 decks)

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