Lernkartei Grundlagen CJ (Seite 4 von 13)

Karten	500
Lernende	42
Sprache	English
Kategorie	Technik
Stufe	Andere
Erstellt / Aktualisiert	14.06.2019 / 12.09.2020
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The left hydraulic pump fails. In this case... (more than 1 correct)

the PWR BRK LOW PRESS annunciator illuminates.

the right pump is capable to operate all subsystems.

the subsystems operate slower.

the pilot should land as soon as practical.

When using external power for more than 30 minutes...

the battery automatically disconnects.

disconnect the battery by removing the connector plug.

disconnect the battery via the battery switch.

disconnect the battery via the battery disconnect switch.

What is the reason for pressurising the hydraulic reservoir with bleed air? (more than 1 correct)

Tp prevent foaming of the hydraulic fluid.

To pressurise the hydraulic system.

To ensure positive fluid flow to the pumps.

Pressing the ENG FIRE light...

closes the associated generator field relay.

stops the hydraulic pump.

closes the respective fuel firewall shutoff valve.

discharges the fire extinguishing bottle.

AHRS alignment is possible in flight.

false

true

How many battery powered engine starts are permitted per hour?

3

When both throttles are advanced above approximately 90% N2 on ground...

the cabin starts to climb to approx. 200 ft above field elevation with a ROC of 100 fpm

the cabin descends to approx. -200 ft below field elevation with a ROD of 100 fpm.

the cabin altitude remains constant, until the maximum differential of 8.6 psi is reached.

What is the correct configuration for the first engine start with external power?

Battery switch BATT, generators OFF, battery connected

Battery switch BATT, generators GEN, battery connected

Battery switch BATT, generators GEN, battery disconnected

Battery switch BATT, generators OFF, battery disconnected

Prior to takeoff, the digital pressurisation controller is normally set to...

take-off elevation.

destination elevation plus 200 feet.

planned cruising altitude or planned cruising flight level.

take-off elevation minus 200 feet.

destination elevation.

During the preliminary cockpit preparation the pilot has to check de AIR SOURCE SELECT knob.

What is the correct position?

BOTH

L

FRESH AIR

EMER

OFF

Differential braking is not available....

if the system loading valve is not energised

when using the emergency brake

if both engine-driven hydraulic pumps fail

with anti-skid INOP

The fasten-seat-belt signs come on when...

(more than one answer correct)

passenger safety switch is set to SEAT BELT

the inertia switch (G-Switch) of the emergency battery senses a g-force of "5 g" or more

passenger safety switch is set PASS SAFETY

the passenger safety switch is set to OFF

After Take-off the gear is being retracted by moving the gear lever to the "gear up" position.

What effect does this action have on the landing lights?

All landing lights remain on, according to switch position

After gear up the landing lights cut off automatically

What is the correct configuration for the first engine start with external power?

Battery switch BATT, generators GEN, battery disconnected

Battery switch BATT, generators OFF, battery disconnected

Battery switch BATT, generators OFF, battery connected

Battery switch BATT, generators GEN, battery connected

How many fuel quick draings are installed under each wing?

1

2

3

4

5

The standby HSI is displayed automatically...

when one generator fails

when the R AHRS switch is placed in AUTO

when both generators fail

when the battery switch is placed to emergency position

The flight mission is EDDW --> EDDS

EDDW ELEV 14'

EDDS ELEV 465'

After Start: Which altitude is entered by CM2 in the digital pressurisation controller?

700 feet

Have a look at the PFD.

Which reversion control should be used?

MFD REV

AHRS REV

DADC REV

The main gear tyres are automatically deflated,...

if a certain temperature is exceeded

if a certain pressure is exceeded

when the aeroplane reaches its parking position

if a certain density is exceeded

The pilot wants to switch on the entry lights, but there is no green ENTRY light switch illumination. What are plausible reasons?

(There is more than one answer correct)

Battery disconnected

Battery OVERTEMP

Hot battery bus failure

Battery discharged

Mark the location of the pressurisation control Panel.

Antwort wie markiert.

A question concerning the digital pressurisation controller.

If the ADC fails in flight...

(More than one answer correct)

FL appears in the SET ALT window

the controller switches to isobaric mode

the amber controller light illuminates

the controller remains in the CA Auto mode

the controller automatically switches to the EMER mode

During landing gear extension...

the loading valve is not affected

the hydraulic loading valve is energised closed

the HYD PRESS ON annunciator extinguishes

the hydraulic loading valve is energised open

Active frequencies are displayed in...

white

amber

green

red

Cabin pressurisation is normally regulated by...

controlling the amount of air entering the cabin

controlling the amount of air escaping the cabin

What is the reason for pressurising the hydraulic reservoir with bleed air?

(More than one answer correct)

To pressurize the hydraulic system

To ensure positive fluid flow to the pumps

To prevent foaming of the hydraulic fluid

The MASTER WARNING light illuminates when...

an amber annunciator illuminates

both the L and R GEN OFF annunciators illuminate amber

any annunciator illuminates

Which components are furnished with ice detection systems?

Windshields and horizontal stabilizer leading edge

Wing and nacelle leading edge

Windshields and left wing leading edge

Horizontal stabilizer and engine nacelle leading edge

What is the power supply of the Digital Air Data Computers?

ADC 1: Emergency Bus; ADC 2: Normal DC Bus

ADC 1: Emergency Bus; ADC 2: Emergency Bus

ADC 1: Normal DC Bus, ADC 2: Emergency Bus

ADC 1: Normal DC Bus, ADC 2: Normal DC Bus

Is there any time limit for landing light operation on ground?

No

Yes

Mark the correct statement concerning ENGINE START?

Before moving the thrust levers to IDLE, the N2 must have reached more than 8%

Before pressing the engine start button, the throttles must be moved from OFF to IDLE

the start sequence is terminated at approx. 60% N2

The start-up should be aborted, if no ITT rise occurs immediately after ignition

How can you open the generators power relay?

Generator switch to RESET

Generator switch to OFF

Generator switch to GEN

The pressure of the engine fire extinguisher bottles can be checked...

on the direct reading gauges in the right nose baggage compartment

on the direct reading gauges in the aft baggage compartment area

on the direct reading gauges in the main wheel well

on the bottel pressure indicator, located on the lower right hand side of the instrument panel

How long does it take to correct a fuel imbalance of 160 pounds?

8 min

During climb, the automatic mode of the cabin pressurisation system should not allow the cabin rate of climb to exceed approximately...

600 fpm

What is the power supply of the "standby HSI"

Standby Battery

Normal DC Power

Emergency battery

Emergency DC Power

Pressing an ENG FIRE light...

closes the associated generator field relay

stops the hydraulic pump

discharges the fire extinguishing bottle

closes the respective fuel firewall shutoff valve

On the annunciator panel, the annunciator extinguishes...

when the malfunction is corrected

when exceeding a time limit

when pressed

when the master warning system is reset

The left Hydraulic Pump fails. In this case..

the right pump is capable to operate all subsystems

the pilot should land as soon as practical

the subsystems operate slower

the PWR BRK LOW PRESS annunciator illuminates

Have a look at the PFD.

The Decision eight is ...

300 ft

Grundlagen CJ

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