Lernkartei Grundlagen CJ (Seite 7 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 hydraulic pumps are in operation when...

electrical power is switched on

the engine is running

a subsystem is activated

the reservoir is pressurised with bleed air

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

at the wing root

in the horizontal stabilizer leading edge

downstream the pylon precooler

in the engine nacelle leading edge

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 right tank fuel supply line

The right fuel boot pump has failed

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

The left fuel boost pump has failed

More than one:

Pressing the LH ENG FIRE light ...

trips the associated generator field relay open

closes the left engine bleed air valve

arms the electrical circuits for operation of the engine fire extinguisher bottles

closes the left hydraulic firewall shutoff valve

closes the left fuel firewall shutoff valve

The hydraulic system pressure is limited to...

500 psi

1000 psi

1500 psi

2000 psi

There is more than one correct answer!

Where can the different TCAS modes be selected?

On the upper radio tuning unit

On the ATC control panel

On the TCAS control panel

On the lower radio panel

To simulate a windshield overheat condition place the rotary TEST knob to W/S TEMP and set the...

WINDSHIELD BLEED AIR knobs to OFF

WINDSHIELD BLEED switch to HI or LOW

WINDSHIELD BLEED AIR knobs to MAX

WINDSHIELD BLEED switch to OFF

To simulate a winshield overhieat condition place the rotary TEST knob to W/S TEMP and set the

WINDSHIELD BLEED switch to HI or LOW

WINDSHIELD BLEED AIR knobs to OFF

WINDSHIELD BLEED switch to OFF

WINDSHIELD BLEED AIR knobs to MAX

Have a look at the PFD.

Which reversion control should be used?

AHRS ; REV

DADC ; REV

MFD ; REV

According to certification, the speedbrakes must be retracted prior to ...

50 feet GND

50 feet MSL

200 feet GND

200 feet MSL

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

the engine inlet and generator inlet anti-ice system

the cabin to pressurise the aeroplane

the de-ice boots

The ailerons are operated by...

pneumatic pressure

wires

hydraulic actuators

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)

The outside check starts...

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

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

on the left side

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

During normal operation, the mode for controlling cabin pressure is...

Isobaric mode

MANUAL mode

AUTO mode

The FUEL LOW LEVEL R annunciator illuminates.

Mark the correct statements.

more than one correct answer!

(Nur eine Anwort im Video markiert

passenger safety switch is set PASS SAFETY

passenger safety switch is set to SEAT BELT

passenger safety switch is set to OFF

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

Analyse the following situation:

The aeroplane is on ground with both engines running.

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

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

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

There is more than one correct aswer!

The speedbrakes retract automatically if...

a complete electrical failure occurs 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

More than one:

A question concerning the digital pressurisation controller.

If the ADC fails in flight..

the amber controller light illuminates

FL appears in the SET ALT window

the controller remains in the CA AUTO mode

the controller switches to isobaric mode

the controller automatically switches to the EMER mode

There is more than one correct answer!

Mark all possibillities for starting the Williams FJ44-1AP engine...

Battery Start

EPU assisted start

APU assisted start

Crossfeed bleed air start

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

Emergency DC power

Standby battery

Emergency battery

Normal DC power

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

Control valve: NORMAL; Cabin ALT below 8000 ft; DC power available

Control valve: AUTO; Cabin ALT below 13500 ft; DC power available

Control valve: NORMAL; Cabin ALT above 13500 ft; DC power available

Control valve: MANUAL; Cabin ALT below 13500 ft; DC power available

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

There is 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 CAUTION lights illuminate

the MASTER WARNING lights illuminate

the right ENG FIRE light illuminate

What is the maximum cruising flight level of the CJ1+?

FL 390

FL 410

FL 430

FL 450

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 above 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

Wich system utilises hot engine bleed air extracted directly from the compressor?

Wing ice protection

Tail ice protection system

Windshield ice protection system

Engine ice protection system

More than one

To verify that fuel transfer occurs from the right to the left tank, it is necessary to...

ensure, that the left FUEL BOOST ON light illuminates

ensure, that the right FUEL BOOST ON light illuminates

observe that the FUEL TRANSFER annunciator illuminates

monitor the fuel quantity indicators for oppropriate quantity changes

ensure, that both white FUEL BOOST ON annunciators illuminate

In flight, the engines return heated fuel to the tanks.

true

false

Mark the correct statemen

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

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

At a failure of one generator the master warning is activated

A flashing amber caution annunciator indicates a malfunction that requires immediate action

More that one:

What are the pilot actions in case of an Elevator Trim Runaway?

Select FLAPS 15

Pull the PITCH TRIM circuit breaker

Engage AUTOPILOT

Press the AP TRIM DESC button

What is the power supply of the digital air data computers

ADC 1 / ADC 2: Emergency Bus

ADC 1 / ADC 2: Normal DC Bus

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

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

The FRESH AIR position of the AIR SOURCE SELECT knob is used..

to provide fresh air to the windshield

anytime to increase the ventilation of the cabin

for ground use or low altitude unpressurised flights

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

Battery start

EPU assisted start

APU assisted start

Crossfeed bleed air start

Grundlagen CJ

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