Warning Systems

39問 • 1年前

問題一覧

The annunciator lights and gauge indications are the primary means of informing the crew of airplane status

B. FALSE

Airplane crew alerting is provided by the EICAS function of the Airplane Information Management System and Warning Electrocnic System

A. TRUE

EICAS Advisory message TCAS and amber TCAS FAIL is displayed on both NDs when,

A. If TCAS failed

EICAS Advisory message TCAS OFF and amber TCAS OFF is displayed on both NDs when,

C.BothA&B

The EICAS operates the

C. Master Caution lights, Warning Alerts, Caution Alerts, Advisory alerts

System alerts are classified as

D. Time critical warnings, Warnings, Caution and advisories

What does this indicate

C. Severe descent rate

Select the correct statement regarding TAIL STRIKE alert message

D. All of the above

Select the correct statement regarding time critical PULL UP warning,

A. It is displayed on the PFD, Master warning lights illuminate and an associated voice warning is heard

Pushing a master warning light reset switch, after the WINDSHEAR alert,

B. Extinguishes the lights

What does this indicate

B. The engine failure has occurred during the take off roll

If the air speed decreases into the minimum speed region, independent stick shakers vibrate the control columns and the master warning lights illuminate

B. FALSE

EICAS Red warning level alert messages require immediate crew awareness and corrective action and are displayed on the PFD

B. FALSE

Pushing the master warning light reset switch silences the aural siren for all warnings other than those associated with config gear, stabilizer, and cabin altitude.

B. FALSE

Select the correct statement

C. The OVERSPEED message remains displayed until the airspeed is reduced below VMO/MMO

Pushing the master warning light reset switch silences the overspeed warning siren extinguishes the master warning lights

B. FALSE

The aural fire bell is sounded for

D. All of the above

Select the correct statement

A. The caution alert tone, consisting of series of beeps in rapid succession sounds once for each caution level alert

EICAS Communication messages

B. direct crew attention to normal communication conditions

In order to differentiate Advisory level alert message from the Caution alert messages

D. The advisory alert messages are indented one space

Which amongst this is an Advisory level alert message

C. EQUIP COOLING OVRD

Advisory level alert messages

C. Are displayed amber, lowest priority alert messages indented one space, and can be canceled or recalled by pushing CANC/RCL switch

Select the correct statement regarding communication messages

C. Are displayed white, prefaced with white dot and cannot be canceled by pushing CANC/RCL switch

The medium level communication alert messages are

A. Appear on the first available line above displayed memo messages

The EICAS communication messages are classified as

D. All of the above

Memo messages

C. displayed below any displayed communication alert message

The cancel/recall switch on the DSP is used to

C.BothA&B

Warning level alert messages

B. Can not be cancelled

Pushing the cancel/recall switch a second time

D. All of the above

Select the correct statement regarding status messages

A. A STATUS cue appears below EICAS message display area to inform about new status messages

STATUS messages are intended to provide crew with information, to initiate immediate crew actions

B. FALSE

The following EICAS messages are displayed when an intentional engine shutdown is carried out by crew using fuel control cutoff switch or a fire switch.

A. TRUE

During ground engine start, new caution and advisory level alert messages are inhibited

A. Until start is aborted

During Take Off, the STATUS cue inhibit is cancelled, when

C. 30 minutes after lift off

The takeoff inhibit for communication alerts and aural chime remains effective until reaching

A. 400 feet R.A or 20 Secs after rotation

If a fire warning occurs after the aircraft has crossed the V1

D. All of the above

The takeoff configuration warning function is armed when the ground speed exceeds V1

B. FALSE

During Take Off, the landing configuration warning CONFIG GEAR, the Master WARNING lights & Siren are

A. inhibited until reaching 825 feet R.A or approx. 150 Secs from landing gear unlock for retraction

If this message appears prior to departure, it indicates

D. All of the above

Airplane General

Airplane General

Air Systems

Air Systems

Anti-Ice, Rain

Anti-Ice, Rain

Automatic Flight

Automatic Flight

Communications

Communications

Electrical

Electrical

Engines, APU

Engines, APU

Fire Protection

Fire Protection

Flight Controls

Flight Controls

Flight Instruments, Displays

ユーザ名非公開 · 41問 · 1年前

Flight Instruments, Displays

41問 • 1年前

ユーザ名非公開

Flight Management, Navigation

ユーザ名非公開 · 72問 · 1年前

Flight Management, Navigation

Fuel

Fuel

Hydraulics

Hydraulics

Landing Gear

Landing Gear

問題一覧

The annunciator lights and gauge indications are the primary means of informing the crew of airplane status

B. FALSE

Airplane crew alerting is provided by the EICAS function of the Airplane Information Management System and Warning Electrocnic System

A. TRUE

EICAS Advisory message TCAS and amber TCAS FAIL is displayed on both NDs when,

A. If TCAS failed

EICAS Advisory message TCAS OFF and amber TCAS OFF is displayed on both NDs when,

C.BothA&B

The EICAS operates the

C. Master Caution lights, Warning Alerts, Caution Alerts, Advisory alerts

System alerts are classified as

D. Time critical warnings, Warnings, Caution and advisories

What does this indicate

C. Severe descent rate

Select the correct statement regarding TAIL STRIKE alert message

D. All of the above

Select the correct statement regarding time critical PULL UP warning,

A. It is displayed on the PFD, Master warning lights illuminate and an associated voice warning is heard

Pushing a master warning light reset switch, after the WINDSHEAR alert,

B. Extinguishes the lights

What does this indicate

B. The engine failure has occurred during the take off roll

If the air speed decreases into the minimum speed region, independent stick shakers vibrate the control columns and the master warning lights illuminate

B. FALSE

EICAS Red warning level alert messages require immediate crew awareness and corrective action and are displayed on the PFD

B. FALSE

Pushing the master warning light reset switch silences the aural siren for all warnings other than those associated with config gear, stabilizer, and cabin altitude.

B. FALSE

Select the correct statement

C. The OVERSPEED message remains displayed until the airspeed is reduced below VMO/MMO

Pushing the master warning light reset switch silences the overspeed warning siren extinguishes the master warning lights

B. FALSE

The aural fire bell is sounded for

D. All of the above

Select the correct statement

A. The caution alert tone, consisting of series of beeps in rapid succession sounds once for each caution level alert

EICAS Communication messages

B. direct crew attention to normal communication conditions

In order to differentiate Advisory level alert message from the Caution alert messages

D. The advisory alert messages are indented one space

Which amongst this is an Advisory level alert message

C. EQUIP COOLING OVRD

Advisory level alert messages

C. Are displayed amber, lowest priority alert messages indented one space, and can be canceled or recalled by pushing CANC/RCL switch

Select the correct statement regarding communication messages

C. Are displayed white, prefaced with white dot and cannot be canceled by pushing CANC/RCL switch

The medium level communication alert messages are

A. Appear on the first available line above displayed memo messages

The EICAS communication messages are classified as

D. All of the above

Memo messages

C. displayed below any displayed communication alert message

The cancel/recall switch on the DSP is used to

C.BothA&B

Warning level alert messages

B. Can not be cancelled

Pushing the cancel/recall switch a second time

D. All of the above

Select the correct statement regarding status messages

A. A STATUS cue appears below EICAS message display area to inform about new status messages

STATUS messages are intended to provide crew with information, to initiate immediate crew actions

B. FALSE

The following EICAS messages are displayed when an intentional engine shutdown is carried out by crew using fuel control cutoff switch or a fire switch.

A. TRUE

During ground engine start, new caution and advisory level alert messages are inhibited

A. Until start is aborted

During Take Off, the STATUS cue inhibit is cancelled, when

C. 30 minutes after lift off

The takeoff inhibit for communication alerts and aural chime remains effective until reaching

A. 400 feet R.A or 20 Secs after rotation

If a fire warning occurs after the aircraft has crossed the V1

D. All of the above

The takeoff configuration warning function is armed when the ground speed exceeds V1

B. FALSE

During Take Off, the landing configuration warning CONFIG GEAR, the Master WARNING lights & Siren are

A. inhibited until reaching 825 feet R.A or approx. 150 Secs from landing gear unlock for retraction

If this message appears prior to departure, it indicates

D. All of the above