M15c20

16問 • 9ヶ月前

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問題一覧

The APU fire protection system

has a single fire bottle that has to be discharged by operating the associated fire handle.

On what principle dose a Systron Donner fire wire works?

gas pressure

On a twin engine turbo fan powered aircraft, there are usually

two bottles one or both can fire into either engine

The kidde system fire detection system is work on the principle of

Resistance change

Each fire detector system must be constructed and installed so that:

it will withstand the vibration,inertia,and other loads to which it may be subjected in operation

when checking the weight and pressure of an engine fire bottle, the ambient temperature should be taken into account because

The pressure increases at higher ambient temperature

A Fire detection system that operates on the rate of temperature rise:

Thermocouple system.

What is the function of a Fire detection system? to

activates a warning device in the event of a powerplant fire

The three fire requirements to happen are:

Fuel ,heat and oxygen

When fitting a continuous- loop type fire detector You should ensure that there is a minimum bend radius of

1”and 8” spacing is Between support as a general standard, the clamps securing the wire to the nacelles or engine are used purely for support. not insulation

Fire extinguishers work by

displacing oxygen

The extinguishant used in gas turbine fire bottles is

dry powder

A thermocouple detection system initiates a fire warning when

any of the individual detectors reaches a predetermined temperature

When cartridge electrical connectors are disconnected

the cartridge must be removed according manufacturer.

The most effective method for extinguishing aircraft fires involves using:

a chemical compound that combines with the oxygen to prevent it from combining with the fuel

One of the requirements for a fire detection system is that

the detector circuitry must operated directly from the aircraft electrical system

mod5 training

mod5 training

M6c1

M6c1

M6c2

M6c2

M6c3

M6c3

M6c4

M6c4

M6c5

M6c5

M6c6

M6c6

M6c7

M6c7

M6c8

M6c8

M6c9

M6c9

M6c10

M6c10

M6c11

M6c11

M7c1

M7c1

M7c2

M7c2

M7c3

M7c3

M7c4

M7c4

M10c1

M10c1

M7c5

M7c5

問題一覧

The APU fire protection system

has a single fire bottle that has to be discharged by operating the associated fire handle.

On what principle dose a Systron Donner fire wire works?

gas pressure

On a twin engine turbo fan powered aircraft, there are usually

two bottles one or both can fire into either engine

The kidde system fire detection system is work on the principle of

Resistance change

Each fire detector system must be constructed and installed so that:

it will withstand the vibration,inertia,and other loads to which it may be subjected in operation

when checking the weight and pressure of an engine fire bottle, the ambient temperature should be taken into account because

The pressure increases at higher ambient temperature

A Fire detection system that operates on the rate of temperature rise:

Thermocouple system.

What is the function of a Fire detection system? to

activates a warning device in the event of a powerplant fire

The three fire requirements to happen are:

Fuel ,heat and oxygen

When fitting a continuous- loop type fire detector You should ensure that there is a minimum bend radius of

1”and 8” spacing is Between support as a general standard, the clamps securing the wire to the nacelles or engine are used purely for support. not insulation

Fire extinguishers work by

displacing oxygen

The extinguishant used in gas turbine fire bottles is

dry powder

A thermocouple detection system initiates a fire warning when

any of the individual detectors reaches a predetermined temperature

When cartridge electrical connectors are disconnected

the cartridge must be removed according manufacturer.

The most effective method for extinguishing aircraft fires involves using:

a chemical compound that combines with the oxygen to prevent it from combining with the fuel

One of the requirements for a fire detection system is that

the detector circuitry must operated directly from the aircraft electrical system