AGK 3

34問 • 1年前

Via

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問題一覧

The commands are indicated by "V" bars.

single-cue system.

The commands are displayed on two separate command bars, one for pitch and one for roll.

double-cue system.

It maneuvers the airplane to satisfy the computed commands of the flight director.

autopilot.

It is a component of the autopilot system which manages engine power in all modes with the auto pilot engaged.

auto-thrust system.

It controls power, and by extension airspeed, from takeoff to touchdown, activating the auto-throttle switches brings the thrust levers to life, on takeoff, they advance the thrust to the computed takeoff value automatically so the pilot can concentrate on flying the airplane instead of setting the power.

auto-throttle.

They are critical part of any comprehensive speed control system that is why pilots must maintain situational awareness especially during approach to make sure that the auto-throttle system is engaged to prevent speed decay.

auto-throttle.

An aircraft collision avoidance system designed to reduce the incidence of mid-air collisions between aircraft.

TCAS.

TCAS means

traffic collision avoidance system.

It monitors the airspace around an aircraft for the other aircraft equipped with a corresponding active transponder, independent of air traffic control, and warns pilots of the presence of other transponder-equipped aircraft which may present a threat of mid-air collision (MAC).

TCAS.

TCAS II issues the following types of aural annunciations:

All of the above.

Target symbol for other traffic is

hollow cyan (light blue) or white diamond.

Target symbol for proximate traffic is

solid cyan (light blue) or white diamond.

Target symbol for intruders (i.e. aircraft which trigger a TA) is

solid yellow or amber circle.

Target symbol for threats (i.e. aircraft which trigger the RA) is

solid red square.

When a TA is issued, pilots are

instructed to initiate a visual search for the traffic.

When the RA is issued, pilots are

expected to respond immediately.

A system designed to alert pilots if their aircraft is in immediate danger of flying into the ground or an obstacle.

GPWS.

Mode for excessive descent rate

"SINK RATE" "PULL UP"

What is mode "TERRAIN" "PULL UP" for?

excessive terrain closure rate.

Altitude loss after takeoff or with a high power setting mode is

"DON'T SINK"

The "TOO LOW - TERRAIN" "TOO LOW - GEAR" "TOO LOW - FLAPS" mode is for

unsafe terrain clearance.

Excesive deviation below glideslope mode is

"GLIDESLOPE"

The "BANK ANGLE" mode is

excessively steep bank angle.

Windshear protection mode is

"WINDSHEAR"

A system that provides aural and visual warning to the crew as an aircraft approaches a preselected altitude during climb or descent.

altitude alert system.

A system that provides the flight crew with sufficient information and alerting to detect a potentially hazardous terrain situation and so the flight crew may take effective action to prevent a CFIT event.

Terrain Avoidance and Warning System (TAWS).

A safety net that automatically provides a distinctive warning to pilots when the aeroplane is, based only on the radio altimeter reading and terrain closure rates derived thereof, in potentially hazardous proximity to terrain.

TAWS.

A function looks ahead of the aircraft along and below its lateral and vertical flight path and provides suitable alerts if a potential CFIT threat exists.

Forward Looking Terrain Aviodance (FLTA) function.

A function of TAWS uses the aircraft's current position and flight information as determined from a suitable navigation source and airport database to determine if the aircraft is hazardously below the normal (typically 3 degree) approach path for the nearest runway as defined by the alerting algorithm.

A Premature Descent Alert (PDA) function.

A safety net in which a (Hard) Warning indicates that the aircraft is in dangerous situation and immediate action is required and an Alert (or soft warning) indicates an abnormal status in relation to terrain which invites prompt review and a possible change of flight path or aircraft configuration.

TAWS.

The basic type/s of aircraft propeller are 1. Fixed Pitch Propeller. 2. Constant Speed Propeller. 3. Ground Adjustable Propeller.

1,2,3

The angle of attack of this type of propeller is set at installation and cannot be changed during aircraft operation. They are only efficient in one stage pf flight at a given airspeed and RPM.

Fixed pitch propeller.

It is also called a variable pitch propeller and have baldes that can be rotated around their long axis to change the pitch of the blades. The propeller pitch can be controlled of set by the pilot. and it can provide peak performance at any phase of flight.

Constant speed propeller.

the pitch can only be adjusted on the ground while the engine is not running. This type can be optimize in its performance for current payload and flying conditions.

Ground adjustable propeller.

CPL HUMAN PERFORMANCE AND LIMITATIONS (1)

Via · 78問 · 1年前

CPL HUMAN PERFORMANCE AND LIMITATIONS (1)

78問 • 1年前

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CPL HUMAN PERFORMANCE AND LIMITATIONS (2)

Via · 81問 · 1年前

CPL HUMAN PERFORMANCE AND LIMITATIONS (2)

81問 • 1年前

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CPL Radio Telephony (1)

Via · 100問 · 1年前

CPL Radio Telephony (1)

100問 • 1年前

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CPL Radio Telephony (2)

Via · 100問 · 1年前

CPL Radio Telephony (2)

100問 • 1年前

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CPL Radio Telephony (3)

Via · 20問 · 1年前

CPL Radio Telephony (3)

Met 1

Met 1

Met 2

Met 2

Met 3

Met 3

Met 4

Met 4

Met 5

Met 5

Met 6

Met 6

Met 7

Met 7

Met 8

Met 8

Human Performance 3

Human Performance 3

Met 9

Met 9

Met 10

Met 10

AGK 1

AGK 1

AGK 2

AGK 2

AGK 3

AGK 3

問題一覧

The commands are indicated by "V" bars.

single-cue system.

The commands are displayed on two separate command bars, one for pitch and one for roll.

double-cue system.

It maneuvers the airplane to satisfy the computed commands of the flight director.

autopilot.

It is a component of the autopilot system which manages engine power in all modes with the auto pilot engaged.

auto-thrust system.

auto-throttle.

An aircraft collision avoidance system designed to reduce the incidence of mid-air collisions between aircraft.

TCAS.

TCAS means

traffic collision avoidance system.

TCAS.

TCAS II issues the following types of aural annunciations:

All of the above.

Target symbol for other traffic is

hollow cyan (light blue) or white diamond.

Target symbol for proximate traffic is

solid cyan (light blue) or white diamond.

Target symbol for intruders (i.e. aircraft which trigger a TA) is

solid yellow or amber circle.

Target symbol for threats (i.e. aircraft which trigger the RA) is

solid red square.

When a TA is issued, pilots are

instructed to initiate a visual search for the traffic.

When the RA is issued, pilots are

expected to respond immediately.

A system designed to alert pilots if their aircraft is in immediate danger of flying into the ground or an obstacle.

GPWS.

Mode for excessive descent rate

"SINK RATE" "PULL UP"

What is mode "TERRAIN" "PULL UP" for?

excessive terrain closure rate.

Altitude loss after takeoff or with a high power setting mode is

"DON'T SINK"

The "TOO LOW - TERRAIN" "TOO LOW - GEAR" "TOO LOW - FLAPS" mode is for

unsafe terrain clearance.

Excesive deviation below glideslope mode is

"GLIDESLOPE"

The "BANK ANGLE" mode is

excessively steep bank angle.

Windshear protection mode is

"WINDSHEAR"

A system that provides aural and visual warning to the crew as an aircraft approaches a preselected altitude during climb or descent.

altitude alert system.

Terrain Avoidance and Warning System (TAWS).

TAWS.

A function looks ahead of the aircraft along and below its lateral and vertical flight path and provides suitable alerts if a potential CFIT threat exists.

Forward Looking Terrain Aviodance (FLTA) function.

A Premature Descent Alert (PDA) function.

TAWS.

The basic type/s of aircraft propeller are 1. Fixed Pitch Propeller. 2. Constant Speed Propeller. 3. Ground Adjustable Propeller.

1,2,3

The angle of attack of this type of propeller is set at installation and cannot be changed during aircraft operation. They are only efficient in one stage pf flight at a given airspeed and RPM.

Fixed pitch propeller.

Constant speed propeller.

the pitch can only be adjusted on the ground while the engine is not running. This type can be optimize in its performance for current payload and flying conditions.

Ground adjustable propeller.