Cartes mémoires Grundlagen CJ (Seite 11 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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The start sequence is normally terminated..

at approximately 45% N2

by moving the throttle lever to IDLE

by pressing the START DISG button

by placing the IGNITION switch to OFF

A master warning can only be reset by...

the PIC

pushing one of teh two master warning lights

correcting the fault, which triggered the warning

pulling the corresponding circuit breaker

With the FUEL BOOST switches in the OFF position, the boost pumps operate automatically when lefrt or right FUEL TRANSFER is selected

true

false

If a complete DC electrical failure occure, regardless of the AIR SOURCE SELECT knob position, pneumatic air is supplied..

as if in BOTH position because FCVs fail closed

as if in BOTH position because of PRSOVs fail closed

as if in BOTH position because PRSOVs fail open

If a complete DC electrical failure occurs, regardless of the AIR SOURCE SELECT knob position, pneumatic air is supplied...

as if in BOTH position because of PRSOVs faul closed

as if in BOTH position because FCVs fail closed

as if in BOTH position because PRSOVs fail open

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

The HYD FLOW LOW annunciator illuminates

Hydraulic power is lost

The HYD PRESS ON annunciator illuminates

The subsystems are still available

More than one:

The speedbrakes retract automatically if...

either throttle is advanced above 90% N2 during normal operation

both hydraulic pumps fail during flight

both hydraulic pumps fail during ground operation

a complete electrical failure occurs during flight

Mark the correct statement

With the control lock engaged, the secendary flight controls are locked

The engines can be started with the control lock engaged

The airplane should not be towed with the control lock engaged

With the control lock engaged, the primary and secondary flight controls are locked

More than one:

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

the MASTER CAUTION lights to illuminate

the MASTER WARNING light to illuminate

the right ENG FIRE light illuminate

the left ENG FIRE light illuminate

How many battery powered enginge starts are permitted per hour?

3

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

Mark any switch wicht is in the wrong switch position

1

2,3,4

5

6

7

If hydraulic power is lost...

the flaps operate with the backup eletrical system, but extend and retract at a reduced rate

the flaps cannot be extended

there is no effect on wing flap operation

a split flap condidtion could result if the flaps are lowered

The minimum temperature for a battery powered engine start is...

(...) °C

-18

During cruise flight, the R FUEL BOOST ON annunciator illuminates without any action by the crew.

What could possibly be the reason?

Low fuel pressure in the tank fuel line supply

The fuel quantity in the right tank has dropped below 160 lbs

The right fuel boost pump has failed

the left fuel boost pump has failed

Mark the correct statement concerning the windshield ice protection system

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

The windshield bleed air shutoff valve is designed fail safe closed

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

The WINDSHIELD BLEED AIR selectors vary the airflow to the windshields

The start sequence is normally terminated at approx...

(...) % N

45

More than one:

Which of the following pressure controller modes use DC power?

Isobaric mode

MANUAL mode

AUTO mode

A master warning can only be reset by...

pulling the corresponding circuit breaker

the pilot in command

pushing one of the two master warning lights

correcting the fault, wich triggered the warning

The BLD AIR O'HEAT annunciator indicates an overheat condition...

in the horizontal stabilizer leading edge

downstream of the pylon precooler

at the wing root

in the engine nacelle leading edge

A battery powered engine start is intended on SEP 18th

Wind is no factor.

Mark the correct statement.

The right engine has to be started first

The leeward enginge has to be started first

The windward enginge has to be started first

The left enginge has to be started first

Mark the correct statement

A failure of both generators at the same time triggers the master warning

A flashing amber annunciator indicates a malfunctions that requires immediate action

At a failure of one generator the master warning is activated

A steady amber caution annunciator can be extinguished by pressing one of the two amber caution lights

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

600

With the FUEL BOOST switches in the OFF position, the boost pumps operate automatically when left or right FUEL TRANSFER is selected.

This statement is..

true

false

What is the power supply of the standby flight display

Emergency DC power

Standby battery

EMergency battery

Normal DC power

With the throttles set to IDLE, the landing gear retracted and anti-ice swith ON, the FADEC maintains approx..

70% N2

57% N2

40% N2

23% N2

The wings crossflow shutoff valve...

is designed fail safe open

provides protection for either wing in case its corresponding engine failed

enables anti-icing of an inoperative

automatically opens in case of an engine failure

More than one:

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

To ensure positive fluid flow to the pumps

To prevent foaming of the hydraulic fluid

To pressurise the hydraulic system

There is more than one correct answer!

Mark the correct statements.

AHRS 1 uses normal DC power

AHRS 2 operates on Emergency DC power

AHRS 1 operates on Emergency DC power

AHRS 2 uses normals DC power

More than one:

The FUEL LOW LOVEL R annunciator illuminates.

Mark the correct statement:

According to precedure, the pilot should activate the left fuel boost pump

According to precedure, the pilot should activate the both fuel boost pumps

The remaining fuel in the right tank is 185+- 15 pounds or less

the total remaining fuel is 185+- 15 pounds or less

According to precedure, the pilot should activate the right fuel boost pump

The outside check starts...

in front of the left engine, standing between the engine and the trailing edge

on the left side

in front of the right engine, standing between the engine and the trailing edge

with the right engine from the front side of the right wing

More than one:

Nosewheel steering is operative...

on ground, with the gear retracted.

in flight, with the gear extended

in flight, with the gear retracted

on ground, with the gear extended

There is more than one correct answer!

Where can the different TCAS modes be selected?

On the lower radio control panel

On the upper radio tuning unit

On the ATC control panel

On the TCAS control panel

Pilots must be using headsets when the overhead audio speaker is inhibited.

true

false

More than one:

The landing gear uplocks are...

mechanically held engaged by springs

hydraulically disengaged

pneumatically disengaged

The windshield rain removal system...

uses winshield bleed air

is designed for high speed operation

uses engine anti-ice bleed aire

uses service bleed air

During flight one engine fails.

An engine restart accomplished with the start button...

is a generator assisted start

is a battery start

is prohibited

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

take-off elevation minus 200 feet

planned cruising altitude or planned crusising FL

destination elevation plus 200 ft

take-off elevation

take-off elevation plus 200 ft

PDF

Radar Altutude is

200

The wings crossflow shutoff valve...

is designed fail safe open

automatically opens in case of an engine failure

enables anti-icing of an inoperative

provides protection for either wing in case its corresponding engine failed

On the annunciator panel, the annunciator extinguishes ...

when exceeding a time limit

when the malfunction is corrected

when the master warning system is reset

when pressed

Grundlagen CJ

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