15 Powerplant

ATA 70 – Powerplant

15 Powerplant

50問 • 5ヶ月前ATA 70 – Powerplant

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通報

問題一覧

On ground the start sequence is automatically aborted:

in case of hot start, hung start, stall or no light up

During an automatic start on ground, the sequence is:

Ignition by N2 > 16%, HP fuel valve opening by N2 > 22% ; start valve closure by N2>50%

Thrust reversers are actuated by:

hydraulic actuators: green for engine 1 – yellow for engine 2

The FADEC is electrically supplied by:

self powered above 12% N2

In manual mode, when the thrust levers are between the CLB detent and IDLE:

each position of the levers corresponds to an N1

What is the EGT limit at TOGA power setting:

950ºC during 5 min. (10 min. on 1 engine)

What is the maximum continuous oil temperature:

140ºC

The max continuous oil temp. limit maybe exceeded, what is the limit, and under what conditions?

155ºC for less than 15 min.

What is the minimum starting oil temperature:

-40ºC

What is the minimum oil quantity (ECAM indications):

9.5 qts + estimated consumption (0.5 qt/hr)

What is the minimum oil pressure at ground idle:

13 psi

What is the maximum N1:

104%

What is the maximum N2:

105%

What is the maximum N2 for starter engagement:

20%

What is the maximum starter operating time: (4 consecutive cycles of)

2 min. followed by 20 sec. of no operation

Starter cooling time requirements are:

15 min. cooling time after 4 cycles of 2 min.

The maximum reverse thrust may be used down to:

70 knots (idle reverse down to A/C stop)

What is the maximum allowable FLEX TEMP?

ISA + 53ºC

Reduced thrust is permitted:

if corrected temp. is lower than Tmax FLEX (ISA + 53ºC)

In manual thrust, in cruise, the pilot should limit the N1. What is the limit?

displayed MAX CLB N1, minus 1.9 %

Is the MAX CRUISE N1 displayed on upper ECAM:

At Toulouse (500 ft): Tref is 29ºC, outside air temp. is 36ºC and you found a corrected flex temp of 33ºC. Is it possible to use FLEX thrust for take-off?

EGT indication becomes red on E/W display when EGT is higher than:

950ºC

What is the FADEC:

is a digital engine control system that performs complete engine management.

The FADEC system is:

self powered above 12% N2 with AC power when N2 is below 12%

What device provides direct closure of the HP shut-off valve?

the master switch at OFF position

Which valve ensures an adequate fuel flow:

the fuel metering valve of the HMU

Is the engine still supplied in case of fuel filter CLOG?

Yes, by by-passing the fuel filter (by-pass) valve)

Cranking may be manually selected by setting:

b. with Master Sw. to OFF, the MODE selector to CRANK and MAN START pb to ON

During an automatic starting sequence, the pack valves close when:

IGN/START is selected

During an automatic starting sequence:

start valve closes at N2>50%

Maximum EGT during engine starts is:

725ºC

The FADEC automatically selects continuous ignition in the following cases:

ignition delay during start, flameout detected or EIU failure while engine running.

How is the oil cooled?

by the engine fuel/oil heat exchanger and the servo fuel heater

Oil pressure indicator becomes red when pressure is lower than:

13 psi

In A/THR Mode the thrust computed by the FMGC is limited:

by the ECU (with the TLA)

The thrust reverser activation condition are:

aircraft on the ground and thrust lever between reverse idle detent and max reverse

REV green appears on the N1 indicator when:

the reverse doors are fully deployed

Reverse deployment requires TLA – 3º, signal from the SEC's. One reverse will be lost if:

c. a or b

The low pressure rotor (N1) consist of:

a front Fan (1 stage) – 4 stage booster – 4 stage LP turbine

A/THR can be engaged:

automatically when pilot initiates a take-off or a go-around or if there is an alpha floor detection after T/O and down to 100ft (RA) on landing

In flight, if the instinctive disconnect pb is pressed for more than 15 sec., the A/THR including alpha floor is definitely lost:

Right

At take-off, as soon as the power is set (FLEX or TOGA):

ATS function is engaged but not active

After a FLEX TO, you have an engine failure and you want to select MCT:

you set the throttle levers out of the FLEX/MCT detent (to TOGA or CLB detent) then back to FLEX/MCT position

Pressing the ENG. FIRE pb switch (on the ENG fire panel) causes the closure of:

fuel LP valve

ASYM amber message (FMA) means:

one thrust lever is set out of climb notch (both engines running)

MCT amber message (in the left part of the FMA) means:

throttles are not in MCT position after engine failure in flight

“LVR CLB” flashes white on FMA, if the throttles are not in CL position when:

the A/C is above the altitude of thrust reduction

The thrust limit is computed by:

the ECU according to the thrust lever position

On ground the automatic start sequence is:

start valve and LP fuel valve opens, ignition starts when N2 > 16%, HP fuel valves open when N2 > 22% when N2 > 50%, start valve closes and igniter off

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CPL Radio Telephony (2)

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CPL Radio Telephony (3)

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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

POF 1

POF 1

POF 2

POF 2

POF 3

POF 3

FPP 1

FPP 1

NAV 1

NAV 1

NAV 2

NAV 2

OP 1

OP 1

OP 2

OP 2

OP 3

OP 3

OP 4

OP 4

OP 5

OP 5

OP 6

OP 6

OP 7

OP 7

OP 8

OP 8

OP 9

OP 9

OP 10

OP 10

OP 11

OP 11

OP 12

OP 12

OP 13

OP 13

OP 14

OP 14

IR Gleims 1

IR Gleims 1

IR Gleims 2

IR Gleims 2

IR Gleims 3

IR Gleims 3

IR Gleims 4

IR Gleims 4

IR Gleims 5

IR Gleims 5

Meteorology

Meteorology

AGK

AGK

Met 2

Met 2

AGK 2

AGK 2

AGK 3

AGK 3

AGK 4

AGK 4

Avee 1

Avee 1

Bob 1

Bob 1

Miko 1

Miko 1

Dan

Dan

Ivan

Ivan

Avee 2

Avee 2

Bob 2

Bob 2

Miko 2

Miko 2

Dan 2

Dan 2

Ivan 2

Ivan 2

Final

Final

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2 Auxiliary Power Unit

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3 Communications

3 Communications

4 Electrical System

4 Electrical System

5 Indicating / Recording Systems

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5 Indicating / Recording Systems

6 Fire Protections

6 Fire Protections

7 Flight Controls

7 Flight Controls

8 FMGS Navigation

8 FMGS Navigation

9 Fuel System

9 Fuel System

10 Hydraulic System

10 Hydraulic System

11 Ice and Rain

11 Ice and Rain

12 Landing Gear

12 Landing Gear

13 Oxygen – Emergency Equipment

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13 Oxygen – Emergency Equipment

14 Pneumatic System

14 Pneumatic System

16 Safety

16 Safety

17 Smoke (Fire Protection)

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17 Smoke (Fire Protection)

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問題一覧

On ground the start sequence is automatically aborted:

in case of hot start, hung start, stall or no light up

During an automatic start on ground, the sequence is:

Ignition by N2 > 16%, HP fuel valve opening by N2 > 22% ; start valve closure by N2>50%

Thrust reversers are actuated by:

hydraulic actuators: green for engine 1 – yellow for engine 2

The FADEC is electrically supplied by:

self powered above 12% N2

In manual mode, when the thrust levers are between the CLB detent and IDLE:

each position of the levers corresponds to an N1

What is the EGT limit at TOGA power setting:

950ºC during 5 min. (10 min. on 1 engine)

What is the maximum continuous oil temperature:

140ºC

The max continuous oil temp. limit maybe exceeded, what is the limit, and under what conditions?

155ºC for less than 15 min.

What is the minimum starting oil temperature:

-40ºC

What is the minimum oil quantity (ECAM indications):

9.5 qts + estimated consumption (0.5 qt/hr)

What is the minimum oil pressure at ground idle:

13 psi

What is the maximum N1:

104%

What is the maximum N2:

105%

What is the maximum N2 for starter engagement:

20%

What is the maximum starter operating time: (4 consecutive cycles of)

2 min. followed by 20 sec. of no operation

Starter cooling time requirements are:

15 min. cooling time after 4 cycles of 2 min.

The maximum reverse thrust may be used down to:

70 knots (idle reverse down to A/C stop)

What is the maximum allowable FLEX TEMP?

ISA + 53ºC

Reduced thrust is permitted:

if corrected temp. is lower than Tmax FLEX (ISA + 53ºC)

In manual thrust, in cruise, the pilot should limit the N1. What is the limit?

displayed MAX CLB N1, minus 1.9 %

Is the MAX CRUISE N1 displayed on upper ECAM:

At Toulouse (500 ft): Tref is 29ºC, outside air temp. is 36ºC and you found a corrected flex temp of 33ºC. Is it possible to use FLEX thrust for take-off?

EGT indication becomes red on E/W display when EGT is higher than:

950ºC

What is the FADEC:

is a digital engine control system that performs complete engine management.

The FADEC system is:

self powered above 12% N2 with AC power when N2 is below 12%

What device provides direct closure of the HP shut-off valve?

the master switch at OFF position

Which valve ensures an adequate fuel flow:

the fuel metering valve of the HMU

Is the engine still supplied in case of fuel filter CLOG?

Yes, by by-passing the fuel filter (by-pass) valve)

Cranking may be manually selected by setting:

b. with Master Sw. to OFF, the MODE selector to CRANK and MAN START pb to ON

During an automatic starting sequence, the pack valves close when:

IGN/START is selected

During an automatic starting sequence:

start valve closes at N2>50%

Maximum EGT during engine starts is:

725ºC

The FADEC automatically selects continuous ignition in the following cases:

ignition delay during start, flameout detected or EIU failure while engine running.

How is the oil cooled?

by the engine fuel/oil heat exchanger and the servo fuel heater

Oil pressure indicator becomes red when pressure is lower than:

13 psi

In A/THR Mode the thrust computed by the FMGC is limited:

by the ECU (with the TLA)

The thrust reverser activation condition are:

aircraft on the ground and thrust lever between reverse idle detent and max reverse

REV green appears on the N1 indicator when:

the reverse doors are fully deployed

Reverse deployment requires TLA – 3º, signal from the SEC's. One reverse will be lost if:

c. a or b

The low pressure rotor (N1) consist of:

a front Fan (1 stage) – 4 stage booster – 4 stage LP turbine

A/THR can be engaged:

automatically when pilot initiates a take-off or a go-around or if there is an alpha floor detection after T/O and down to 100ft (RA) on landing

In flight, if the instinctive disconnect pb is pressed for more than 15 sec., the A/THR including alpha floor is definitely lost:

Right

At take-off, as soon as the power is set (FLEX or TOGA):

ATS function is engaged but not active

After a FLEX TO, you have an engine failure and you want to select MCT:

you set the throttle levers out of the FLEX/MCT detent (to TOGA or CLB detent) then back to FLEX/MCT position

Pressing the ENG. FIRE pb switch (on the ENG fire panel) causes the closure of:

fuel LP valve

ASYM amber message (FMA) means:

one thrust lever is set out of climb notch (both engines running)

MCT amber message (in the left part of the FMA) means:

throttles are not in MCT position after engine failure in flight

“LVR CLB” flashes white on FMA, if the throttles are not in CL position when:

the A/C is above the altitude of thrust reduction

The thrust limit is computed by:

the ECU according to the thrust lever position

On ground the automatic start sequence is:

start valve and LP fuel valve opens, ignition starts when N2 > 16%, HP fuel valves open when N2 > 22% when N2 > 50%, start valve closes and igniter off