Lernkartei Grundlagen CJ (Seite 1 von 13)

Karten	500
Lernende	42
Sprache	English
Kategorie	Technik
Stufe	Andere
Erstellt / Aktualisiert	14.06.2019 / 12.09.2020
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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

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.

Look at the picture

Mark the correct statements

The pitit tubes are anti-iced by bleed air

only the static ports and the angle of attack vane are electrically anti-iced

all pitot/static ports are electrically anti-iced

all electrical heaters are switched on by a single switch

the angle of attack vane heater can be turned on individually

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

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.

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

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

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)

Mark the location of the electric control panel.

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

8

Active frequencies are displayed in ...

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

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

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

this statement is...

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

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.

Ignition during normal engine start is activated by...

pressing the engine start button

turning the IGNITION switches on

moving the thrust lever to IDLE

There are more than one correct answer!

A question concerning the digital pressurisation controller.

If the ADC fails in flight...

the controller remains in the CA AUTO mode

the amber controller light illuminates

the controller automatically switches to the EMER mode

FL appears in the SET ALT window

the controller switches to isobaric mode

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: Normal DC Bus

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

Transmission via COM2 is selected on...

the Flight Management System (FMS)

the Audio Control Panel (ACP)

either of the two Radio Tuning Units (RTUs)

Which components are furnished with ice detection systems?

Windshields and horizontal stabilizer leading edge

Windshields and left wing leading edge

Horizontal stabilizer and engine nacelle leading edge

wing and nacelle leading edge

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

the subsystems are still available

The HYD PRESS ON annunciator illuminates

The HYD FLOW LOW annunciator illuminates

Hydraulic power is lost

Mark the correct statements. (More than 1 correct answer)

The pitot tubes are anti-iced by bleed air

Only the static ports and the angle of attack vane are electrically anti-iced

All pitot/static ports are electrically anti-iced

All electrical heaters are switched on by a single switch

The angle of attack vane heater can be turned on individually

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 remainon, according to switch position

While waiting for the take-off clearance, 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.

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

powers the emergency bus with the battery

should result in the battery voltage remaining at 29.0 volts

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

Transmission via COM2 is selected on...

the Flight Management System (FMS)

the Audio Control Panel (ACP)

either of the two Radio Tuning Units (RTUs).

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

8000 feet (+- 1500ft)

10000 feet (+- 1500ft)

13000 feet (+- 1500ft)

15000 feet (+- 1500ft)

The aileron trim tab is operated by...

a mechanical trim knob on the throttle control quadrant

changing the angle of the aileron fence

a hydraulically operated trim tab motor

an electrically operated trim tab motor

Mark the air distribution settings which are typically used at night or in unusually cold air.

Antwort: Die 2 Kästchen auf der rechten Hälfte wie im Bild bereits markiert.

Active frequencies are displayed in...

amber

white

green

red

Wing leading edge overheat is indicated by a...

flashing WING ANTI-ICE annunciator light plus MASTER CAUTION lights

steady WING ANTI-ICE annunciator light

flashing WING ANTI-ICE annunciator light

steady WING ANTI-ICE annunciator light plus MASTER CAUTiON light

Inflight starter assisted engine start is possible with...

power from the running generator

power from battery

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

Mark the annunciators associated with the hydraulic system...
(There is more than one correct answer)

Antwort wie im Bild bereits markiert.

During windmilling operation, the maximum allowable operating oil consumption for the FJ44-1AP engine is...

0.1 quart per hour

0.8 quart per hour

0.8 gallon per hour

0.1 gallon per hour

Grundlagen CJ

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