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Both engines are running after engine start and the AFT J-BOX LMT annunciator illuminates.

Mark the correct statement!

Do not fly the aeroplane in this condition

A popped start circuit breaker on the aft J-BOX is indicated

The start relay is stuck closed

Do not use the AFT J-BOX, use the FWD J-BOX instead

Do not fly the aeroplane in this condition

A popped start circuit breaker on the aft J-BOX is indicated

The start relay is stuck closed

Do not use the AFT J-BOX, use the FWD J-BOX instead

The MASTER WARNING lights illuminates when...

an amber annunciator illuminates

both the L and R GEN OFF annunciators illuminate amber

any annunciator illuminates

an amber annunciator illuminates

both the L and R GEN OFF annunciators illuminate amber

any annunciator illuminates

Is it possible to select two transmission channels on the audio selector panel simultaneously?

Yes

No

Probably

I dont know

Yes

No

Probably

I dont know

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

8

Which components are furnished with ice detection systems?

windshields and horizontal stabilizer leading edge

wing and nacelle edge

windshields and left leading edge

horizontal stabilizer and engine nacelle leading edge

windshields and horizontal stabilizer leading edge

wing and nacelle edge

windshields and left leading edge

horizontal stabilizer and engine nacelle leading edge

The fasten-seat-belt signs come on when... (more than 1 correct)

passenger safety switch is set to SEAT BELT.

passenger safety switch is set PASS SAFETY.

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

the passenger safety switch is set to OFF.

passenger safety switch is set to SEAT BELT.

passenger safety switch is set PASS SAFETY.

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

the passenger safety switch is set to OFF.

A steady red or steady amber annunciator light extinguishes...

after 88 seconds

when the battery master switch is placed into the ON position

after having corrected the fault, which triggered the warning

after having pushed one of the two master warning lights

after 88 seconds

when the battery master switch is placed into the ON position

after having corrected the fault, which triggered the warning

after having pushed one of the two master warning lights

The ENGINE SYNC switch...

should be ON for single engine operation

must be in the OFF position for take-off and landing

must be in the ON position for tanke-off and landing

should be in the OFF position below 10000 feet

should be ON for single engine operation

must be in the OFF position for take-off and landing

must be in the ON position for tanke-off and landing

should be in the OFF position below 10000 feet

Moving the flap selector lever to any position between 0° and 38°... (more than 1 correct)

energises the hydraulic pump.

energises the hydraulic system loading valve closed.

energises the flap solenoid valve to the selected position.

energises the hydraulic pump.

energises the hydraulic system loading valve closed.

energises the flap solenoid valve to the selected position.

What is the power supply of the digital air data computers?

ADC1: Emergency bus, ADC2: Normal DC bus

ADC1: Emergency bus, ADC2: Emergency bus

ADC1: Normal DC bus, ADC2: Emergency bus

ADC1: Normal DC bus, ADC2: Normal DC bus

ADC1: Emergency bus, ADC2: Normal DC bus

ADC1: Emergency bus, ADC2: Emergency bus

ADC1: Normal DC bus, ADC2: Emergency bus

ADC1: Normal DC bus, ADC2: Normal DC bus

If one igniter fails during engine start...

it results in a "hung start"

the engine still starts normally

it results in a "wet start"

it results in a "hot start"

it results in a "hung start"

the engine still starts normally

it results in a "wet start"

it results in a "hot start"

Inflight assisted engine start is possible with...

power from the battery.

power from the running generator.

power from the battery.

power from the running generator.

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

yes

no

yes

no

The voltage read on the voltmeter with the seletor switch in BATT is sensed from te

left feed bus

crossfeed bus

hot battery bus

right feed bus

left feed bus

crossfeed bus

hot battery bus

right feed bus

The emergency braking system uses...

an engine driven hydraulic pump.

hydraulic pressure from an accumulator.

pneumatic pressure from an accumulator

an electrically driven hydraulic pump.

an engine driven hydraulic pump.

hydraulic pressure from an accumulator.

pneumatic pressure from an accumulator

an electrically driven hydraulic pump.

Which system utilises hot engine bleed air extracted directly from the compressor

Tail ice protection system

Windshield ice protection system

Wing ice protection system

Engine ice protection system

Tail ice protection system

Windshield ice protection system

Wing ice protection system

Engine ice protection system

During climb, the automatic mode of the cabin prssurisation system should not allow the cabin rate of climb to exceed approximately... (... fpm)

600

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 throttle 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

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

before pressing the engine start button, the throttle 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

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

Very hot engine compressor bleed air is extracted from the high pressure compressor and routed to...

the de-ice boots

the cabin to pressurise the aeroplane

the engine inlet and generator inlet anti-ice system

the de-ice boots

the cabin to pressurise the aeroplane

the engine inlet and generator inlet anti-ice system

What happens if the electrical power to the hydraulic System loading valve is interrupted?

The Subsystem are still available

The hydraulic power is lost

The HYDR PRESS ON annunciator illuminates

The HYDR FLOW LOW annunciator illuminates

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

The Subsystem are still available

The hydraulic power is lost

The HYDR PRESS ON annunciator illuminates

The HYDR FLOW LOW annunciator illuminates

Entering the cockpit for the Cockpit Safety Inspection the pilot is confronted with the situation below.

Mark any switch which is in the wrong switch position.

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

Look at the picture

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?

After gear up the landing lights cut off automatically

all landing lights remain on, according to switch position

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

After gear up the landing lights cut off automatically

all landing lights remain on, according to switch position

Entering the cockpit for the cockpit safety inspection the pilot is condronted with the depicted situation below.

Mark any switch which is in the wrong switch position.

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

While waiting for the take-off clearence, the DOOR SEAL annunciator illuminates.

For safety reasons the flight should be cancelled and the aeroplane should return to the ramp for a technical inspection.

This is normal, if the service air pressure is below 23 psi

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

For safety reasons the flight should be cancelled and the aeroplane should return to the ramp for a technical inspection.

This is normal, if the service air pressure is below 23 psi

Placing the battery switch in EMER with the generators on the line ...

still provides charging power to the battery

powers the emergency bus with the battery

should result in the battery voltage remaining at 29 volts.

causes loss of power to the emergency bus since the generators are on the line

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

still provides charging power to the battery

powers the emergency bus with the battery

should result in the battery voltage remaining at 29 volts.

causes loss of power to the emergency bus since the generators are on the line

The maximum cabin altitude limit valve automatically prevents the cabin altitude from exceeding ...

8000 feet (+/- 1500 feet)

10000 feet (+/- 1500 feet)

13000 feet (+/- 1500 feet)

15000 feet (+/- 1500 feet)

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

8000 feet (+/- 1500 feet)

10000 feet (+/- 1500 feet)

13000 feet (+/- 1500 feet)

15000 feet (+/- 1500 feet)

Mark the location of the electric control panel.

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

How many fuel quick drains are installed on the CJ1+ in total?

Commandes clavier:

= tourner,

= avant/arrière,

= faire défiler

8

Active frequencies are displayed in ...

amber

white

green

red

amber

white

green

red

There are more than one correct answer!

Regarding the engine fire-detection test, by placing the rotary TEST knob to FIRE WARN...

the left ENG FIRE light illuminate

the MASTER WARNING lights illuminate

the right ENG FIRE light illuminate

the MASTER CAUTION lights illuminate

the left ENG FIRE light illuminate

the MASTER WARNING lights illuminate

the right ENG FIRE light illuminate

the MASTER CAUTION lights illuminate

How long does it usually take to align the AHRS on ground?

AHRS 1: 45 seconds AHRS 2: 35 seconds

AHRS 1: 35 seconds AHRS 2: 45 seconds

AHRS 1: 35 seconds AHRS 2: 35 seconds

AHRS 1: 45 seconds AHRS 2: 45 seconds

AHRS 1: 45 seconds AHRS 2: 35 seconds

AHRS 1: 35 seconds AHRS 2: 45 seconds

AHRS 1: 35 seconds AHRS 2: 35 seconds

AHRS 1: 45 seconds AHRS 2: 45 seconds

Mark the correct statement concerning the emergency brake system.

the brake pedals should be depressed during the emergency braking

it is allowed to taxi to the ramp with the emergency brake system in use

differential braking is possible

multiple pulls of the emergency brake handle might result in brake loss

the brake pedals should be depressed during the emergency braking

it is allowed to taxi to the ramp with the emergency brake system in use

differential braking is possible

multiple pulls of the emergency brake handle might result in brake loss

the engine fire extinguisher bottle pressure check is part of the exterior inspection.

this statement is...

true

false

true

false

The windshield rain removal system...

uses engine anti-ice bleed air

uses service bleed air

uses windshield bleed air

is designed for high speed operation

uses engine anti-ice bleed air

uses service bleed air

uses windshield bleed air

is designed for high speed operation

The start sequence is normally terminated at approx.

45 % N2

Have a look on the PFD. The Radar Altitude is...

300

How long does it take to correct a fuel imbalance of 120 pounds?

6 min

Analyse the following situation:

The aeroplane is on ground with both engines running.

The AIR CONDITIONING switch is moved to AUTO and the green COMPRESSOR ON light does not illuminate.

This is normal if the cabin temperature is below the selected temperature

This indicates a system failure of the air conditioning system and requires further pilot actions.

This is normal if the cabin temperature is below the selected temperature

This indicates a system failure of the air conditioning system and requires further pilot actions.

Grundlagen CJ

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Grundlagen CJ

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