Cartes mémoires Grundlagen CJ (Seite 12 von 13)

Cartes-fiches	500
Utilisateurs	42
Langue	English
Catégorie	Technique
Niveau	Autres
Crée / Actualisé	14.06.2019 / 12.09.2020
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An RTU failure is indicated by...

a green frequency display

a red frequency display

a white frequency display

an amber frequency display

More than one:

Mark all possibilities for starting the FJ44-1AP engine....

Battery start

EPU assisted start

APU assisted start

Crossfeed bleed air start

Without generator power, the battery for the STANDBY FLT DISPLAY should at least approx...

half an hour

an hour

one and a half hour

two hours

On the ground, with eiter engine operating below approx. 90% N2...

both outflow valves are closed

both outflow valves are open

Pressing the LH ENG FIRE light... (more than 1 correct)

arms the electrical circuits for operation of the wngine fire extinguisher bottles.

closes the left engine bleed air valve.

trips the associated generator field relay open.

closes the left fuel firewall shutoff valve

closes the left hydraulic firewall shutoff valve.

If wind is a factor, the...

windward engine is started first.

leeward engine is started first.

Flight IDLE schedule is used to..

reduce engine acceleration time

deliver sufficient bleed air for the cabin pressurisation during flight

avoid shock cooling during extended idle operation

avoid engine flame out during flight

The speedbrakes retarcts automatically if... (more than 1 correct)

a complete electrical failure occures during flight.

either throttle is advanced above 90% N2 during normal operation.

both hydraulic pumps fail during flight.

both hydraulic pumps fail during ground operation.

The white HYD PRESS ON annunciator on the annunciator panel...

illuminates when the speedbrakes are fully extended

illuminates while the speedbrakes are extending

illuminates when the speedbrakes are fully retracted

does not illuminate during speed brake operation

What is the power supply of the "Standby HSI"?

Emergency DC power.

Standby battery.

Emergency battery.

Normal DC power.

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

What is the correct position?

L

Both

R

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 fails

with anti skid INOP

There is more than one correct answer!

The fasten seatbelt signs come on when...

passenger safety switch is set to SEAT BELT

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

passenger safety 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 drains are installed under each wing ?

Enter the number

4

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 batter switch is placed to emergency position

The flight mission is EEDW -> EDDS

EDDW ELEV 14`

EDDS ELEV 465´

AFTER START: Which altitude is entered by CM2 in the digital pressurisation controller?

(...)fee

700

Which are the conditions that drop the passenger oxygen masks automatically?

Control Valve MANUAL DROP, Cabin ALT above 13500 ft, DC power available

Control Valve NORMAL, Cabin ALT below 8000 ft, DC power available

Control valve NORMAL, Cabin ALT above 13500 ft, DC power available

Control Valve AUTO, Cabin ALT above 13500 ft, DC power available

Is there any limit for landing light operation on ground?

No

Yes

More than one:

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

Battery disconnected

Battery OVERTEMP

Battery discharged

Hot battery bus failure

Have a look at the PFD.

Which reversion control should be used?

MFD, REV

AHRS, REV

DADC, REV

An RTU Failure is indicated by ...

a white frequency display

an amber frequency display

a red frequency display

a green frequency display

The standby HSI is displayed automatically...

when the R AHRS switch is placed in AUTO.

when one generator fails.

when the battery switch is placed to emergency position.

when both generators fail

Pressing the ENG FIRE light

opens the respective fuel firewall shutoff valve

stops the hydraulic pump

trips the associated generator field reley open

discharges the fire extinguishing bottle

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 start sequence is normally terminated at approx... [%N2]

45

In case of the cabin is overpressurised,...

the CAB ALT warning horn sounds.

the cabin altitude exceeds 10000 feet.

the OVER PRESS annunciator light and the master caution light illuminate.

it can only be recognised on the cabin differential gauge.

The engine fire extinghisher bottles are located in the ...

right nose baggage compartment area

main wheel well

tail cone baggage compartment area

engine nacelles

There is more than one correct answer!

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

Battery disconnected

battery overtemp

hot battery bus failure

battery discharged

What is the power supply of the standby flight display?

Emergency battery.

Emergency DC power.

Standby battery.

Normal DC power.

Mark the correct statement concerning the windshield ice protection system

The winshield bleed air shutoff valve is designed fail safe closed

The WINDSHIELD BLEED AIR selectors vary the airflow to the windshields

With the WINDSHIELD BLEED switch in HI or LOW windshield duct pressure and temperature are monitored

With the WINDSHIELD BLEED switch in HI or LOW windshield duct pressure is monitored

There is more than one correct answer!

A question concerning the digital pressurisation controller.

If the ADC fails in flight...

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 EMRER mode

Which system utilises ot engine bleed air extracted directly from the compressor.

Wing ice protection system.

Engine ice protection system.

Tail ice protection system.

Windshield ice protection system.

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

A master warning can only be reset by...

pushing one of the two master warning lights.

the pilot in command.

correcting the fault, which triggered the warning.

pulling the corresponding circuit breaker.

Active frequencies are displayed in ...

white

amber

green

red

What is the precise indication of the gauges on the electrical panel?

The voltmeter indicates the generator or battery voltage; The ammeter indicate the leoad current of the related generators

The voltmeter indicates the battery voltage only; The ammeter indicate the load current of the batttery

The voltmeter indicates the battery voltage only; The ammeter indicate the loead current of the generators and the battery

The voltmeter indicates the generator or battery voltage; The ammeter indicate the load current of the generators and the battery

Cabin pressurisation is normally regulated by...

controlling the amount of air entering the cabin

controlling the amount of air escaping the cabin

There is more than one correct answer!

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

to pressurise the hydraulic system

to ensure positive fluid flow to the pumps

to prevent foaming of the hyraulic fluid

Grundlagen CJ

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