M11c5⚡️

51問 • 5ヶ月前

ユーザ名非公開

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問題一覧

Instantaneous Vertical Speed Indicator (IVSI) is able to indicate change in vertical sped rapidly because it

incorporates accelerometers

An attitude indicator uses a

Vertical gyro

An alpha vane

measure aircraft angle of attack

Glass cockpit on a modern transport aircrafts will use

LCD screens

An altimeter contains a capsule which has

static pressure fed to the outside of it

An aeroplane gyroscope spinning on a vertical axis will be sensitive to

pitch and roll

An altimeter big handle points to 6 and the small handle points to 2, so the altimeter indicating

2600ft

An encoding altimeter

sends the altitude digitally to the ATC via transponder mode C

The directional gyro is checked every 15 minutes for

drift

An aircraft airspeed indicator has

pitot to the capsule and static to the outside of the capsule

On modern transport A/C the hydraulic system parameters are digitalized for interface with other system, the primary purpose for this

display on the EFIS in the flight deck

Air data computer has

pitot pressure and static pressure

The altitude is the vertical distance between the aircraft and see- level the barosetting therefore is

QNH

An ADF incorporates

both sense and loop antennas

SELCAL is used to

monitor the ground signals

Weather radar is a

microwave system

altitude data provided by transponder is

Mode C

Radio altimeter will measure all aircraft

heights above the ground level up to 2500ft,only

In a GPS system the aircraft equipment is the

user segment

The VOR bearing information is indicated on

Radio Magnetic Indicator RMI

An Instrument Landing System consists of

localizer, glideslope and marker beacons

A non-directional beacon (NDB) is used by

Automatic direction finder

An Inertial navigation system uses

three gyros and two accelerometers

ACARS uses

VHF or SATCOM systems

VHF communication is a

line of sight transmission system

Marker beacon antenna is located

on the underside of the aircraft

If the flight director roll command bar is right of center during a localize approach, the pilot needs to

fly the aircraft to the right

ACARS is primarily for communication between the aircraft and

the maintenance base

Distance Measuring Equipment (DME) measures

The slant distance from the ground to aircraft

The outer marker beacon indication color is

blue

The standard VOR system provides

bearing information only

VHF navigation is used by

VOR and the ILS

Each ring laser gyro in an internal reference system uses

two laser beams

SATCOM can be used for

data and voice transmission

For long rang communication the

HF system is used

Autopilot annunciation is on the

Primary flight display, PDF

The VHF NAV and COM system has a range which is

greater if the aircraft is at higher altitude

On the aircraft that does not have a glass cockpit, dual VOR equipment’s are indicated on

the Horizontal Situation Indicator: the (HSI) and RMI

Why does an audio panel have push-buttons to enable listening to NAV receiver

all navigation beacons also transmit audio Morse code indents

The new emergency locator transmitter regulatory requirement for digital information transmission is on

406 MHZ

The instrument landing system, ILS, is turned on the

VHF NAV receiver same as the VOR

power supply for the emergency locator transmitter (ELT) comes from

an internal lithium battery pack

A ‘Squake’ code is applicable to

the transponder mode A

The maximum radio altimeter track altitude is

2500 ft

Radio altimeter system can be self-tested

both on the ground and in the air

If the battery fail on the ground (INS system)

a red warning light appear on the MSU and horn sound

The middle marker modulation is keyed with

ultimate dots and dashes

The output of an autopilot system are

the server

The localizer system after approach guidance to the runway in term of

the horizontal plane

For an IRS system to pass the alignment system performance test the

altitude entered must be within given limits of the latitude computed by IRU

The instrument that displays the flight director commands is known as

flight director indicator (FDI) and attitude director indicator

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問題一覧

Instantaneous Vertical Speed Indicator (IVSI) is able to indicate change in vertical sped rapidly because it

incorporates accelerometers

An attitude indicator uses a

Vertical gyro

An alpha vane

measure aircraft angle of attack

Glass cockpit on a modern transport aircrafts will use

LCD screens

An altimeter contains a capsule which has

static pressure fed to the outside of it

An aeroplane gyroscope spinning on a vertical axis will be sensitive to

pitch and roll

An altimeter big handle points to 6 and the small handle points to 2, so the altimeter indicating

2600ft

An encoding altimeter

sends the altitude digitally to the ATC via transponder mode C

The directional gyro is checked every 15 minutes for

drift

An aircraft airspeed indicator has

pitot to the capsule and static to the outside of the capsule

On modern transport A/C the hydraulic system parameters are digitalized for interface with other system, the primary purpose for this

display on the EFIS in the flight deck

Air data computer has

pitot pressure and static pressure

The altitude is the vertical distance between the aircraft and see- level the barosetting therefore is

QNH

An ADF incorporates

both sense and loop antennas

SELCAL is used to

monitor the ground signals

Weather radar is a

microwave system

altitude data provided by transponder is

Mode C

Radio altimeter will measure all aircraft

heights above the ground level up to 2500ft,only

In a GPS system the aircraft equipment is the

user segment

The VOR bearing information is indicated on

Radio Magnetic Indicator RMI

An Instrument Landing System consists of

localizer, glideslope and marker beacons

A non-directional beacon (NDB) is used by

Automatic direction finder

An Inertial navigation system uses

three gyros and two accelerometers

ACARS uses

VHF or SATCOM systems

VHF communication is a

line of sight transmission system

Marker beacon antenna is located

on the underside of the aircraft

If the flight director roll command bar is right of center during a localize approach, the pilot needs to

fly the aircraft to the right

ACARS is primarily for communication between the aircraft and

the maintenance base

Distance Measuring Equipment (DME) measures

The slant distance from the ground to aircraft

The outer marker beacon indication color is

blue

The standard VOR system provides

bearing information only

VHF navigation is used by

VOR and the ILS

Each ring laser gyro in an internal reference system uses

two laser beams

SATCOM can be used for

data and voice transmission

For long rang communication the

HF system is used

Autopilot annunciation is on the

Primary flight display, PDF

The VHF NAV and COM system has a range which is

greater if the aircraft is at higher altitude

On the aircraft that does not have a glass cockpit, dual VOR equipment’s are indicated on

the Horizontal Situation Indicator: the (HSI) and RMI

Why does an audio panel have push-buttons to enable listening to NAV receiver

all navigation beacons also transmit audio Morse code indents

The new emergency locator transmitter regulatory requirement for digital information transmission is on

406 MHZ

The instrument landing system, ILS, is turned on the

VHF NAV receiver same as the VOR

power supply for the emergency locator transmitter (ELT) comes from

an internal lithium battery pack

A ‘Squake’ code is applicable to

the transponder mode A

The maximum radio altimeter track altitude is

2500 ft

Radio altimeter system can be self-tested

both on the ground and in the air

If the battery fail on the ground (INS system)

a red warning light appear on the MSU and horn sound

The middle marker modulation is keyed with

ultimate dots and dashes

The output of an autopilot system are

the server

The localizer system after approach guidance to the runway in term of

the horizontal plane

For an IRS system to pass the alignment system performance test the

altitude entered must be within given limits of the latitude computed by IRU

The instrument that displays the flight director commands is known as

flight director indicator (FDI) and attitude director indicator