M11c3

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問題一覧

Passenger windows in a large transport category aircraft normally have

two load-bearing panes

The power supply to a cargo loading system is available

only when the cargo door is fully open.

Seat track cut-outs on large passenger carrying aircraft, provide for various seat spacing, usually in

one inch increments.

The primary structural components that make up a wing on a large metal constructed aeroplane are

skin, spar, ribs, stringers.

Wing-mounted engine pylons are attached to the

front spar only.

During steady flight, the upper skin of a wing is

in compression.

The ‘web’ of a wing spar is designed primarily to withstand

shear load.

empennage configuration must the vertical stabiliser be constructed to be strongest.

A high horizontal stabiliser (‘T’ tail)

On a modern transport aircraft, the structural members of a stabiliser structure (spars, ribs, skin panels) are most likely to be constructed of

carbon and/or glass fibre composites.

Mass balance on a control surface is provided to

prevent control surface flutter.

Aerodynamic balance of control surfaces is normally carried out by

arranging some surface area forward of the hinge line.

A mass attached to the leading edge of a control surface is for

flutter control.

is a type of engine pylon sometimes called a ‘stub wing’

Aft fuselage engine mount

Hinged engine cowlings are normally divided into two types. These are

hot section and cold section cowlings

If an engine cowling is constructed of composite materials, metal strips fitted to the surface of the cowling is for

lightning protection.

Doors that close the fuselage from the inside are called

plug- type doors.

Dummy windows are made of………..of aluminium alloy plate.

one layer

The construction of the type of joint in which the upper skin panel overlaps the lower skin panel is called

lap joint.

The largest load on the aircraft construction

landing gears.

One of the main requirements that the door of the aircraft should have is

the door must be opened and closed from the inside and outside.

Scratches on aircraft windows which is less than 0.254 mm (.010inces) deep is called

light scratches.

The main lengthwise members in a wing truss are

the spar.

Fitting external tanks to the wing tips helps to prevent

induce drag.

An overweight landing is one in which the aircraft has

too much kinetic energy on landing.

One purpose of a rib is to

maintain the correct contour of an aerofoil covering.

A spar is tapered from root to tip because

bending moment is greatest at the root.

Cabin doors and emergency exits are normally sealed by

inflatable rubber seals.

Acrylic sheets should be stored

vertically

A wing that does not need any external struts or braces is known as a

cantilever

The lower wing surface is usually made from aluminium alloy

2024.

in pressurized aeroplane cabins There are two types of leakage in an aircraft pressure vessel

controlled and uncontrolled.

The doors in the pressurized cabin can be divided into two groups

plug-type doors and non plug-type doors

Firewalls usually made of stainless steel, titanium or thermoplastics, in order to

limit the propagation of fire

Air pressure sealing system is

to make it possible to use pressurizes cabins.

For comfortable cabin conditions the air in the cabin should be maintained between

21°C and 27°C

The bolted wing attachment is mainly used in

small aircrafts

The radome is a cone-shaped structure made from

fiberglass

are used to make up the framework of the wing

Ribs

Most wing spars are built up from aluminum alloy

7075

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問題一覧

Passenger windows in a large transport category aircraft normally have

two load-bearing panes

The power supply to a cargo loading system is available

only when the cargo door is fully open.

Seat track cut-outs on large passenger carrying aircraft, provide for various seat spacing, usually in

one inch increments.

The primary structural components that make up a wing on a large metal constructed aeroplane are

skin, spar, ribs, stringers.

Wing-mounted engine pylons are attached to the

front spar only.

During steady flight, the upper skin of a wing is

in compression.

The ‘web’ of a wing spar is designed primarily to withstand

shear load.

empennage configuration must the vertical stabiliser be constructed to be strongest.

A high horizontal stabiliser (‘T’ tail)

On a modern transport aircraft, the structural members of a stabiliser structure (spars, ribs, skin panels) are most likely to be constructed of

carbon and/or glass fibre composites.

Mass balance on a control surface is provided to

prevent control surface flutter.

Aerodynamic balance of control surfaces is normally carried out by

arranging some surface area forward of the hinge line.

A mass attached to the leading edge of a control surface is for

flutter control.

is a type of engine pylon sometimes called a ‘stub wing’

Aft fuselage engine mount

Hinged engine cowlings are normally divided into two types. These are

hot section and cold section cowlings

If an engine cowling is constructed of composite materials, metal strips fitted to the surface of the cowling is for

lightning protection.

Doors that close the fuselage from the inside are called

plug- type doors.

Dummy windows are made of………..of aluminium alloy plate.

one layer

The construction of the type of joint in which the upper skin panel overlaps the lower skin panel is called

lap joint.

The largest load on the aircraft construction

landing gears.

One of the main requirements that the door of the aircraft should have is

the door must be opened and closed from the inside and outside.

Scratches on aircraft windows which is less than 0.254 mm (.010inces) deep is called

light scratches.

The main lengthwise members in a wing truss are

the spar.

Fitting external tanks to the wing tips helps to prevent

induce drag.

An overweight landing is one in which the aircraft has

too much kinetic energy on landing.

One purpose of a rib is to

maintain the correct contour of an aerofoil covering.

A spar is tapered from root to tip because

bending moment is greatest at the root.

Cabin doors and emergency exits are normally sealed by

inflatable rubber seals.

Acrylic sheets should be stored

vertically

A wing that does not need any external struts or braces is known as a

cantilever

The lower wing surface is usually made from aluminium alloy

2024.

in pressurized aeroplane cabins There are two types of leakage in an aircraft pressure vessel

controlled and uncontrolled.

The doors in the pressurized cabin can be divided into two groups

plug-type doors and non plug-type doors

Firewalls usually made of stainless steel, titanium or thermoplastics, in order to

limit the propagation of fire

Air pressure sealing system is

to make it possible to use pressurizes cabins.

For comfortable cabin conditions the air in the cabin should be maintained between

21°C and 27°C

The bolted wing attachment is mainly used in

small aircrafts

The radome is a cone-shaped structure made from

fiberglass

are used to make up the framework of the wing

Ribs

Most wing spars are built up from aluminum alloy

7075