ENGINE VAKIFBANK

Question

The thrust reverser may be deployed.

Answer 1

In flight when the thrust lever is at idle

Answer 2

When either radio altimeter is sensing less than 10 feet altitude

Answer 3

When the air/ground safety sensor is in the ground mode

Answer 4

Insıde the HMU

Answer 5

Between the Fırst and Second Stage of the engine driven fuel pump

Answer 6

Downstream of the HPSOV

Answer 7

Mobil Jet 1

Answer 8

Mobil Jet 2

Answer 9

Aeroshell 300

Answer 10

Integrated drive generator (IDG) manual disconnect circut receives arm signal

Answer 11

The fuel control panel logic receives signal and monitors the fuel spar valve position and the engine START LEVER switch position for operation of the Spar Valve Closed light

Answer 12

The EEC receives reset signal which allows chanels A and B to alternate between active and standby modes of operation

Answer 13

Airplane bleed data, or the amaunt of bleed air the airplane takes from the engine comes from the display electronic units (DEUs)

Answer 14

T12 for current ambient temparature When the airplane has been in flight for 5 minutes the EEC uses T12 and TAT (from the ADIRUs)

Answer 15

Pt for ambient total pressure is supplied by the air data İnertial reference units (ADIRUs)

Answer 16

Take – off

Answer 17

Thrust Reverse

Answer 18

Ground ıdle

Answer 19

hydraulic control unit

Answer 20

control valve module

Answer 21

engine accessory unit

Answer 22

it increases the stall magrin of high LPC

Answer 23

It helps the engine to reach the idle RPM during engine stall

Answer 24

Helps to prevent stall of high pressure compressor (HPC) during ENG Start and acceleration.

Answer 25

between 5 to 30 min.

Answer 26

between 10 to 60 min

Answer 27

between 10 to 30 min

Answer 28

the eng fail message come on

Answer 29

the box around the digital display changes tor ed

Answer 30

automatic control of the engine should be lost

Answer 31

partially open

Answer 32

fully closed.

Answer 33

start switch-GRD position

Answer 34

start switch-CON position

Answer 35

start switch-FLT position

Answer 36

2 roll type

Answer 37

2 ball type

Answer 38

1 ball type, 1 roller type

Answer 39

the NO:5 bearing supports the turbine rotor aft end inside the turbine frame and takes the radial loads.

Answer 40

the NO:1 ball bearing is a thrust bearing which carries hte axial loads generated by LP rotor system

Answer 41

the NO:3 ball bearing is a thrust bearing which carries the axial loads generated by the low pressure rotor system to the frame.

Answer 42

Hydraulic control unit

Answer 43

Control valve module

Answer 44

engine accessory unit

Answer 45

approximately 21 quarts

Answer 46

approximately 23 quarts

Answer 47

approximately 25 quarts

Answer 48

between 5 to 30 min.

Answer 49

between 10 to 60 min.

Answer 50

between 10 to 30 min.

Answer 51

there are 2 ignition exciters attached on the combustion chamber and they convert 28 V DC current to 115 V AC so provide the fuel to be ignited.

Answer 52

these components attached on the generator phase lines sense resistance difference between phases.

Answer 53

it makes igniter plugs active by converting 115 V AC to high voltage

Answer 54

start lewer or fire handle

Answer 55

the EEC uses N2 speed and T25 data to control the transient bleed valve(TBV)

Answer 56

the high pressure compressor (HPC) 9 th stage bleed air that goes into the stage 1 low pressure turbine (LPT) nozzles through the TBV during engine starting

Answer 57

the EEC sends a no dispatch if control current to the TBV EHSV is out of range and EEC in dual channel operation

Answer 58

silver band nozzles are instaled in position 7/8 and 14/15.this nozzle higher fuel flow supplies a stronger spray

Answer 59

"blue band nozzles are the standart nozzle.they are installed in all positions excluding position 7/8 and 14/15"

Answer 60

silver band nozzle are the standart nozzle.they are installed in all positions including position 7/8 and 14/15

Answer 61

eng start switch in GRD position

Answer 62

eng start switch in FLT position

Answer 63

eng start switch in CON position

Answer 64

For a wet motoring the ENGİNE START lever is normally move the IDLE at the 20 % of N1

Answer 65

For a wet motoring the ENGİNE START lever is normally move the IDLE at the 20 %N2

Answer 66

As soon as setting the ENGINE START rotary selector to the GRD position

Answer 67

LPT is used to turn the HPC rotor and the accessory drive

Answer 68

LPT is used to turn the fan and booster rotor

Answer 69

LPT is used to drive the oil and fuel pumps

Answer 70

The REVERSER light illuminates when the thrust reverser is commanded to deploy and extinguishes when itis fully deployed.

Answer 71

The REVERSER light illuminates when in case of malfunction isolation valve or directional control valve

Answer 72

The REVERSER light illuminates when the left and right translating sleeve position signal ( from the LVDT ) are not in range

Answer 73

interlock pawl lockout mechanism prevents simultaneous actuation of the forward and reverse thrust levers

Answer 74

when the forward thrust lewer is not at idle the pawl locks the reverse thrust lever at the STOW position

Answer 75

the reverse thrust iterlock solenoid is energized when both T/R sleeves are deployed lower than 60%

Answer 76

To send Thrust lever position indication to secondary engine display

Answer 77

To send thrust lever angle as an analog input to EEC

Answer 78

To send thrust lever failure information to DEU

Answer 79

to provide smooth air flow for the wing

Answer 80

to provide extra electrical power to the EEC alternator

Answer 81

to provide electrical power to AC transfer bus 1 and 2 on emergency conditions

Answer 82

Fan booster and HPT rotors

Answer 83

Fan and HPC rotors

Answer 84

HPC and HPT rotors

Answer 85

transforms electrical signals from engine sensors into hydraulic pressure

Answer 86

transforms electrical signals from the EEC into hydraulic pressure

Answer 87

sends hydraulic pressures back to the EEC as feedback for closed loop control

Answer 88

Scavenge Oil Filter

Answer 89

Supply Oil Filter

Answer 90

3 of the chip detectors

Answer 91

it is a double shafted turbo prob jet engine with axial flow

Answer 92

it is double shafted turbo fan engine with axial flow

Answer 93

it is a double shafted jet engine with radial flow

Answer 94

a single stage fan and nine stage booster sections

Answer 95

a single stage fan and two stage booster sections

Answer 96

a single stage fan and three stage booster sections

Answer 97

The EEC sends a dispatch signal if control current to the VSV EHSV is out of range and EEC in single channel operation

Answer 98

The EEC uses the LVDTs to monitor the position of the VSV actuators.Right VSV actuators LVDT sends an electrical signal to channel A of the EEC.The left actuators LVDT sends an electrical signal to channel B

Answer 99

The EEC sends a no dispatch signal to the DEUs if VSVs is in the correct position but VSV position signal is out of range on active EEC channel

Answer 100

16 fuel nozzles with blue color band are installed around the combustion chamber case

Answer 101

the surface of the combustion chamber receives cooling air from the LPC discharge air flow

Answer 102

the combustion section is between the high pressure compressor ( HPC ) and the low pressure turbine ( LPT )

Answer 103

if a fault occurs in the normal mode control is automatically transferred to the soft alternate mode

Answer 104

if the hard alternate mod the EEC used N2 as the controlling parameter

Answer 105

engine thrust limit protection is provided in both the normal and hard alternate modes

Answer 106

to heating of non operating engine

Answer 107

to prevent corrosion

Answer 108

to prevent unwanted metarials in the powerplant

Answer 109

By moving the applicable start lever to ''CUTOFF'' position when N' reaches 55%. Continue to motor the engine for 60 seconds to purge the engine of the residual fuel before set the applicable Start Switch to the OFF position

Answer 110

By moving the applicable start lever to ''CUTOFF'' position continue to motor engine for 60 seconds to purge the engine of the residual fuel before set the applicable Start Switch to the ''OFF'' position

Answer 111

By setting the applicable Start Switch to the ''OFF'' position.Continue to motor the engine for 60 seconds to purge the engine of the residual fuel before put the applicable Start lever to the ''CUTOFF'' position

Answer 112

it is heated by using 5th stage air

Answer 113

it is heated by using 9th stage air

Answer 114

there is no heating for spinner cone

Answer 115

The green NO FAULTS DETECTED light comes on if there are no faults found

Answer 116

The fault memory will also erase when the T/R operates 5 times with faults

Answer 117

the EAU FAULT light comes on if there is an internal EAU failure

Answer 118

it can be done for not more than 10 days-30 days-90days

Answer 119

EEC electrical gear box located on the dual-channel AC transfer bus-feed.

Answer 120

Start AC transfer bus-feed during the EEC, 12-15% N2 cycle begins when the EEC alternator feeding

Answer 121

Start EEC fed during the AC Transfer Bus 1, Bus 2 to normally fed AC transfer

Answer 122

VSV, VBV, TBV

Answer 123

N2 at any time during the flight idle speed has dropped below the value.

Answer 124

N2 is a fault indication system.

Answer 125

Exceedance of a N2 (N2 Max value is exceeded] has status

Answer 126

Thrust reverser'larin, aircraft or on the ground 10 feet, until it falls to the ground prevents the opening of.

Answer 127

Translating sleeve until it is fully opened, thrust prevents the opening of reverser'larin.

Answer 128

Both thrust reverser translating sleeves prevents the admission of gas until 60% open position.

Answer 129

Full deployed

Answer 130

Model, N1 trim, ByPass Ratio

Answer 131

Flight Cycle

Answer 132

Oil filter bypass light illuminates

Answer 133

Red pop-out indicator comes out

Answer 134

No action required

Answer 135

Flash for 10 seconds then continously

Answer 136

Only flush

Answer 137

Only illuminate

Answer 138

Silver band is normal nozzles

Answer 139

Silver band have a higher fuel flow

Answer 140

Silver band same as blue band

Answer 141

greater than %60

Answer 142

greater than %20

Answer 143

greater than %50

Answer 144

Translating sleeve

Answer 145

Locking actuator

Answer 146

Lock Pawl mechanism

Answer 147

Electrically by EEC

Answer 148

Automatically

Answer 149

Mechanically by EEC

Answer 150

Hydraulically

Answer 151

Pneumatically

Answer 152

Fuel pressure

Answer 153

5 second wait

Answer 154

10 second wait

Answer 155

30 second wait

Answer 156

Low pressure compressor discharge air

Answer 157

Not cooling

Answer 158

Cooled ambient air

Answer 159

Oil Quantity

Answer 160

Spar valve and ENG valve close

Answer 161

Outflow valve close

Answer 162

Overboard valve close

Answer 163

Prevent on HPC stall during eng start and acceleration

Answer 164

Prevent surge

Answer 165

Prevent wet start

Answer 166

LH and RH exciters feed from 115v ac transfer bus

Answer 167

Both exciters feed from STBY BUS

Answer 168

LH exciter 115v ac transfer bus, RH exciter 115 v ac STBY Bus

Answer 169

For damage

Answer 170

Lightning strike

Answer 171

Monitors leakage

Answer 172

Prevent oil leakage during removel of a component of the oil distrubition sys

Answer 173

Overboard through oil

Answer 174

Single elements

Answer 175

Two elements One for CHN a one for CHN B

Answer 176

One channel

Answer 177

ID Plug contain

Answer 178

Write in AMM

Answer 179

We chance on the CDU

Answer 180

115v to high voltage

Answer 181

28v to 115

Answer 182

115v to 28v

Answer 183

Change the 115v ac to 24v dc

Answer 184

28v dc to 115v

Answer 185

115v ac to 28v dc

Answer 186

Hyd. System B only

Answer 187

Hyd. System A only

Answer 188

LH T/R Sys A RH T/R Sys B

Answer 189

1 fan + 3 stages

Answer 190

Engine fire

Answer 191

During stall

Answer 192

Both engine speeds on at above idle

Answer 193

PT is not valid

Answer 194

Automatically

Answer 195

T2 is not valid

Answer 196

Low pressure pump

Answer 197

High pressure pump

Answer 198

Oil cooler

Answer 199

Kinetic energy

Answer 200

Changes the energy of hot gases into a mechanical energy

Answer 201

1 fan and 3 booster stage

Answer 202

4-8 O'clock position

Answer 203

6-7 O'clock position

Answer 204

8-10 O'clock position

Answer 205

Engine strut

Answer 206

Analog to digital (thrust lever angle)

Answer 207

Digital to analog

Answer 208

Analog to analog

Answer 209

Metal mesh

Answer 210

Plastic filter

Answer 211

Disposable paper filter

Answer 212

not more than 90 days

Answer 213

not more than 180 days

Answer 214

not more than 1 year

Answer 215

the highlight box around the digital readouts will be automatically reset when the airplane is on the ground

Answer 216

If there is an exceedance the highlight box around the digital readouts will be red when the airplane is on the ground and both EECs de-energized

Answer 217

Whit reset buttons reset the all current exceedance data's from primary engine display

Answer 218

it increases the stall margin of highpressure compressor (HPC) during engine start, acceleration

Answer 219

it helps the engine to reach the idle RPM during engine stall

Answer 220

it increases the stal lmargin of low pressure compressor(LPC) during engine start or acceleration

Answer 221

2 stages of LPC and 9 stages HPC

Answer 222

1 stage fan, 4 stages of HPC, 5 stages LPC

Answer 223

3 stages of LPC and 9 stages of HPC

Answer 224

engine manufacture data & engine bypass ratio

Answer 225

engine performance & engine wet weight

Answer 226

regulatory agency data & engine manufacture data

Answer 227

manual drive pad no transfer gearbox

Answer 228

horizontal drive shaft connected to transfer gearbox

Answer 229

vertical drive shaft connected to N1 rotor •

Answer 230

on the outboard fan cowl

Answer 231

on the inboard fan cowl

Answer 232

on the inboard reverser cowl

Answer 233

here are 9 serial connected thermocouples in the system, there are exhaust gas temperature to their

Answer 234

there are 8 serial connected probes in the system, there are exhaust gas temperature to M528 (EAU) box

Answer 235

there are 8 parallel connected probes in the system, there are temperature to EEC

Answer 236

they operate with the opening of high pressure turbine active clearance control system

Answer 237

compared with the feedback of TBV, VSV operates coming from HMU

Answer 238

compared with the feedback of VSV, VBV operates with coming from HMU

Answer 239

during the engine acceleration decrease (LPC) low pressure control stall margin

Answer 240

during the engine start of acceleration increase (HPC) high pressure control low pressure stall margin

Answer 241

VBV prevents the LPC deceleration

Answer 242

hydraulic isolation valve

Answer 243

sync shaft

Answer 244

engine accessory unit (EAU)

Answer 245

15 seconds after the start lever is moved to IDLE during ground

Answer 246

15 seconds after the start valve opens during ground

Answer 247

no automatic shutdown

Answer 248

pilot switch off the lifgt pushing on the switch goess off, this light also comes ENG control light comes on

Answer 249

if it goes off pushing to the switch it is in soft ALTERNATE work

Answer 250

if it comes on more than 15 seconds there comes from ADIRU and it goes to the HARD ALTERNATE other EEC to HARD ALTERNATE mode

Answer 251

it consists of 1 stage fan, 4 stage boosters, 5 stage high pressure compressors

Answer 252

it consists of 4 stage LPC

Answer 253

it consists of 1 stage fan, 4 stage HPC, 5 stage LPC

Answer 254

has 3 channels in every flight leg

Answer 255

has 1 channel if it is inoperative, EEC

Answer 256

has 2 channels when 1 is alternate

Answer 257

they convert 28 V DC to 115 V AC

Answer 258

they convert 115 V AC to 15.000-20.000 V DC

Answer 259

these components mounted a generator difference between lines

Answer 260

range of motion of a reverse thrust

Answer 261

range of motion of start lever

Answer 262

range of motion of thrust lever

Answer 263

supply oil filter starter

Answer 264

scavenge oil filter started to clogging

Answer 265

scavenge and oil filter started to clogging

Answer 266

supply oil filter starter

Answer 267

with fuel from the low pressure fuel pump

Answer 268

with fuel from the servo fuel heater

Answer 269

red pop-out indicator comes out before the bypass valve

Answer 270

the supply oil filter bypass valve opens and ...

Answer 271

the supply oil filter bypass valve opens

Answer 272

when start lever in CUT-OFF position

Answer 273

if EGT is above the red line limit

Answer 274

if N1 > % 15, EEC gains its electrical power from ...

Answer 275

usually gains its electrical power from aircraft electric system

Answer 276

if N2 > % 15, EEC gains its electrical power

Answer 277

it prevents oil to go from oil tank

Answer 278

warm if there is leak in oil system

Answer 279

it causes amber light

Answer 280

ambient (P0)

Answer 281

master maintenance

Answer 282

aural warning module

Answer 283

opens starter valve, closes engine bleed air valve

Answer 284

opens starter valve, closes engine bleed air valve and selected igniters are energized

Answer 285

opens starter valve, closes engine bleed air valve and selected igniters are energized when engine start lever in IDLE

Answer 286

HPSOV is in only transit position

Answer 287

HPSOV is in open and commanded open position

Answer 288

HPSOV is in only transit ...

Answer 289

N1, N2 and start EGT on ground

Answer 290

N1, N2 and 5 minute limit

Answer 291

N1, N2 and fuel

Answer 292

servo fuel heater

Answer 293

engine oil/fuel heat exchanger

Answer 294

IDG oil cooler

Answer 295

Low by-pass tip bir motordur

Answer 296

High by-pass tip bir motordur

Answer 297

Medium by-pass tip bir motordur

Answer 298

Fan frame üzerine bağlanmıştır

Answer 299

Fan case bağlanmıştır

Answer 300

Fan frame mid-box structure arka yüzeyine bağlanmıştır

Answer 301

High Pressure Compressor (HPC) arka statoru üzerine bağlıdır

Answer 302

Combustion case’nin dış yüzeyine bağlıdır

Answer 303

Türbin frame üzerine bağlıdır

Answer 304

Inlet cowl, thrust reverser cowl, fan cowl şeklinde sıralanmıştır

Answer 305

Inlet cowl, fan cowl, thrust reverser cowl şeklinde sıralanmıştır

Answer 306

Fan cowl, thrust reverser cowl, inlet cowl şeklinde sıralanmıştır

Answer 307

HPT ve HPC rotor

Answer 308

Fan, Booster rotor ve LPT rotor

Answer 309

Fan ve HPT rotor

Answer 310

Akiskanlarin türbinlere ve kompresörlere gitmesini önlemektir

Answer 311

Farkli türlerdeki akiskanlarin (yakit,yag,hidrolik vs.) birbirlerine karismalarini önleyerek disariya atilmalarini saglamaktir

Answer 312

Akiskanlarin sicak bölgelere gitmesini önlemek ve komponent kaçaklarini gözlemleyebilmektir

Answer 313

N1 saftindan alir

Answer 314

N2 saftindan alir

Answer 315

Fan saftindan alir

Answer 316

Sistemde 9 adet birbirine seri baglanmis olan thermocouple bulunur. Bu proplar egzos sicakligini HMU'ya iletirler

Answer 317

Sistemde birbirine paralel bagli 8 adet prop bulunur. Bu proplar egzos gaz sicakligini EEC'ye iletirler

Answer 318

Sistemde birbirlerine seri bagli 8 adet prop bulunur. Bu proplar, egzos gaz sicakligini M528(EAU) box'a iletirler

Answer 319

9 kademeden olsmaktadir ve kendisine gelen havanin basincini artirarak, havayi yanma odasina (combustor)gönderir

Answer 320

Havanin hizini artirir ve bu hava splitter vasitasiyla Primary ve Secondary olarak ikiye ayrilir

Answer 321

Tek kademeden olusmaktadir ve yanma odasindan çikan gazlarin enerjisini mekanik enerjiye çevirerek HPC rotorun ve accessory drive'in dönmesini saglar

Answer 322

High Pressure Compressor'lerin (HPC) çıkışı

Answer 323

High Pressure Compressor'lerin (HPC) girişi

Answer 324

Low Pressure Compressor'lerin (LPC) girişi

Answer 325

High Pressure Compressor'lerin (HPC) çıkışı

Answer 326

High Pressure Compressor'lerin (HPC) girişi

Answer 327

Low Pressure Compressor'lerin (LPC) çıkışı

Answer 328

Motor N2 devri, belirlenen en alt limitten daha asagiya düsürmüstür

Answer 329

EEC devre disi kalmistir

Answer 330

VSV ve VBV sistemi devre disi kalmistir

Answer 331

Uçus esnasinda herhangi bir anda N2 idle speed degerinin altina düsmüstür

Answer 332

N2 indikasyon sisteminde bir ariza vardir

Answer 333

Bir N2 exceedance (Max N2 degerinin asilmasi) durumu vardir

Answer 334

N1 şaftındaki vibrasyon değerini

Answer 335

N2 şaftındaki vibrasyon değerini

Answer 336

N1 veya N2 şaftındaki en yüksek vibrasyon değerini

Answer 337

Standby Battery Bus

Answer 338

Transfer Bus 1

Answer 339

Transfer Bus 2

Answer 340

EEC, AVM, DEU'lere bilgi gönderir

Answer 341

Yalniz EEC'ye bilgi gönderir

Answer 342

Yalniz AVM'ye bilgi gönderir

Answer 343

Secondary Display Unit'deki N2 gauge'in üzerindeki amber lamba yanar

Answer 344

Start Valve kapanir, ignition kesilir

Answer 345

Burner Staging Valve kapaliya gider

Answer 346

Start Valve

Answer 347

Sistemde 3 adet chip dedectör bulunur. Hepsi birbirlerinin aynisidir.Manyetik partikülleri miknatis özellikleri sayesinde tutarlar, manyetik olmayan talaslari tutmak için ise birer tane süzgeçleri vardir

Answer 348

Sistemde 2 adet chip dedectör vardir, bulardan biri ön yatak bölgesinden dönen motor yagini süzer. Diger dedectör ise arka yatak yaglama dönüsünde bulunur. Chip dedectörler birbirinin yerine asla takilamazlar

Answer 349

Sistemde 3 adet chip dedectör bulunur. Motora göre en önde bulunan 1 ve 2 nolu yataklardan dönen yagi süzer. Orta siradaki dedectör 3 nolu yataktan dönen yagi süzer, en arkadaki dedectör ise 4 ve 5 nolu yataklarin dönüs hattindadir

Answer 350

Thrust reverse kontrol modülü

Answer 351

Engine Accessory Unit (EAU)

Answer 352

Üst hidrolik actuator'de bulunan LVDT

Answer 353

Yalniz 4. kademe havasi kullanilir

Answer 354

Yalniz 9. kademe havasi kullanilir

Answer 355

4. kademe ve/veya 9. kademe havasi kullanilir

Answer 356

VBV'ler VSV'lerin feedback'ine göre HMU'dan gelen yakit basinciyla çalisirlar

Answer 357

VSV'ler VBV'lerin feedback'ine göre HMU'dan gelen yakit basinciyla çalisirlar

Answer 358

HP Turbine Active Clerance Control (HPTACC) sisteminin açilmasiyla çalisirlar

Answer 359

Bu sensör High Pressure Turbine statörlerinin açilarinin degistirilmesini saglar. Motorun egzos çikisina monte edilmistir

Answer 360

Bu sensör High Pressure Turbine Clerance Control sisteminin çalismasi için gerekli sinyalleri üretir. Motorun 3. istasyonuna monte edilmistir

Answer 361

Bu sensör 5. compressör kademesi üzerine monte edilmistir. Nose Cowl Anti Ice sisteminin dogru degerlerde çalismasini saglar

Answer 362

Motor thrust degerlerini degistirmek, kablo ayarlari yeniden yapmakla saglanir

Answer 363

EEC üzerine monte edilen'Rating Plug' diger bir tipiyle degistirildiginde motorun thrust rejimi degisir

Answer 364

FMC CDU üzerindeki klavye kullanilarak maksimum thrust degistirilebilir

Answer 365

VSV ve VBV sistemlerinin çalismasi için gerekli yakit basincini ayarlar

Answer 366

Güçlü bir yakit sprayi saglayarak motorda flameout rikini önler

Answer 367

Yanma odasina giden yakit akis oran bilgisini EEC'ye bildirir

Answer 368

Santrafuj tiplidir

Answer 369

Dişli tiplidir

Answer 370

Impeller tiplidir

Answer 371

Iki kademelidir

Answer 372

Tek kademelidir

Answer 373

Hydromechanical Unit (HMU] arka yüzeyine bağlanmıştır

Answer 374

N1 > %15 ise EEC alternator'den saglar

Answer 375

N2 > %15 ise EEC alternator'den saglar

Answer 376

Her zaman uçak elektrik sisteminden sağlar

Answer 377

Yoktur. Start EGT limiti asarsa pilot tarafindan motor durdurulur

Answer 378

Vardir. Start EGT limiti asilirsa EEC tarafindan yakit akisi ve ignition durdurulur

Answer 379

Vardir. Start EGT limiti asilirsa DEU'lar tarafindan yakit akisi durdurulur

Answer 380

P12 sensor

Answer 381

PT25 sensor

Answer 382

T12 sensor

Answer 383

Basüstü paneldeki EEC switch ON yapilmissa

Answer 384

Start lever CUTOFF pozisyonda ise

Answer 385

Start switch GRD pozisyonda ise

Answer 386

EEC’ye sistemlerin ne kadar hareket edip etmedikleri bilgilerini lineer veya açısal olarak verirler

Answer 387

Sistemlerin hareket bilgilerini dijital olarak DEU’lara verirler

Answer 388

Primary Engine Display Unit üzerinde sistemlerin hareket miktarlarını görmemizi sağlarlar

Answer 389

Valve açık durumda

Answer 390

Valve açığa veya kapalıya gidiyor

Answer 391

Valve kapalı durumda

Answer 392

Piezoelektrik sensör

Answer 393

Thermocouple sensör

Answer 394

Platin Element sensör

Answer 395

Pilot switch'e basar ve sönüp sönmedigi kontrol edilir, ayrica ENG CONT lambasi yaktirir

Answer 396

ADIRU'den gelen bilgilerde hata olabilir ve 15 sn'den fazla yanarsa, HARD ALT. moduna geçer ve diger EEC'yide HARD ALT moduna aliriz

Answer 397

Switch'e basildiginda sönüyorsa SOFT Alternate'dir ve HMU devreye girer

Answer 398

TBV, BSV, HPTACC

Answer 399

VBV, VSV, LPTACC

Answer 400

TBV, HPTACC

Answer 401

EEC basinç bilgisini kendi üzerinde bulunan bir porttan alir fakat sicaklik bilgisi alamaz

Answer 402

EEC kendi üzerinde olusan bir porttan basinç bilgisini alirkaen, motor üzerinde bulunan T12 ve CIT sensörlerinden de sicaklik bilgisi alir

Answer 403

EEC bu durumda devreden çikar ve HMU o ana kadar yasanmis en güzel bilgilerle motoru çalisir durumda tutmaya çalisir

Answer 404

Total air temperature ve outside ambient pressure

Answer 405

VSV TBV'lerin konum bilgilerini gönderir

Answer 406

CIT ve EGT bilgilerini gönderir

Answer 407

Normalde basinç bilgisi T12 sensörden, hava sicaklik bilgisi ise radio altimetre'den alinir

Answer 408

Normal sartlarda basinç ve toplam hava sicaklik bilgisi ADIRU vasitasiyla alinir. Bu bilgi iletisimin kopmasi halinde basinç bilgisi P0 portundan tein edilir. Hava sicaklik bilgisi ise TAT probe ve T12 sensör ile T25 sensörden alinir

Answer 409

EEC'ye basinç bilgisi barometrik altimetreden gelir, sicaklik bilgisi ise T3 sensörden alinir

Answer 410

Görevi, motor yagini isitirken motora gelen yakiti sogutmaktir. Motorun fan bypass kismina saat 6:00 pozisyonunda baglanmistir

Answer 411

HMU üzerine monte edilmistir, sicak motor yagi ile soguk yakit arasinda isi transferini saglar

Answer 412

3 nolu yakit tankinin içine monte edilmis olan bu komponentin görevi; isinan hidrolik sivisinin, soguk olan yakitla isi transferi yapmasini saglamaktadir

Answer 413

Servolar motor fan case'i üzerine monte edilmislerdir. HMU'dan gelen senslere göre çalisarak N1 ve N2

Answer 414

EEC içinde bulunurlar, HMU'dan gelen senslere göre çalisirlar ve 2 kanaldan DEU'lara feedback blgisi

Answer 415

HMU içinde bulunurlar, EEC'den gelen emirlere göre; VBV, VSV, HPTACC, LPTACC sistemlerini çalistirirlar

Answer 416

Ambient Pressure, STA 0 isatasyonundan

Answer 417

Dinamic Pressure, Pitot tüplerden

Answer 418

Ambient Pressure, EEC üzerinden

Answer 419

Secondary Engine Display üzerinde yakıt akış miktarını gösterebilmek için

Answer 420

HMU içerisindeki FMV’den EEC’nin kendisine gelen feedback bilgisini alamıyorsa

Answer 421

Primary Engine Display üzerinde yakıt akış miktarını gösterebilmek için

Answer 422

EEC üzerinde kayıtlı olan son üç bacak arızaları olduğu

Answer 423

EEC üzerinde kayıtlı olan son on bacak arızaları olduğu

Answer 424

EEC üzerinde kayıtlı olan ENGINE CONTROL yaktıran arızalardır

Answer 425

EEC üzerinde kayıtlı olan son üç bacak arızaları olduğu

Answer 426

EEC üzerinde kayıtlı olan son on bacak arızaları olduğu

Answer 427

EEC üzerinde kayıtlı olan ENGINE CONTROL yaktıran arızalardır

Answer 428

HPTACC, LPTACC

Answer 429

VSV, VBV, TBV

Answer 430

BSV, REVERSE THRUST

Answer 431

HPTACC, LPTACC

Answer 432

VSV, VBV, TBV

Answer 433

Yerde meydana gelmiş arızayı

Answer 434

Birinci uçuş bacağında meydana gelmiş arızayı

Answer 435

Son bacakta meydana gelmiş arızayı

Answer 436

Can tiplidir

Answer 437

Cannular tiplidir

Answer 438

Annular tiplidir

Answer 439

'CONT' pozisyonunda her iki buji kesintisiz ateslemeye hazir hale gelir. 'FLT' pozisyonunda ise

Answer 440

'FLT' pozisyonuna aldigimizda her iki buji ateslemeye hazir hale gelir, ignition sellector switch'in islevi kalmaz

Answer 441

'FLT' pozisyonunda, start valf ve spar valve açilir, sag buji stby AC Bus'tan beslenir

Answer 442

Her motor için 1 Start Lever bulunur. Cut Off pozisyonundan IDLE pozisyonuna alindiginda;spar valve ile HPSOV'e açilma emrini verir. Diger görevi ise EEC'ye ignition bilgisi göndermektir

Answer 443

Start Lever'lar çekildiginde, motor üzerindeki; yakit, hidrolik ve pneumatic sistem valfleri kapanir, Generator besleme voltaji kesilir

Answer 444

ON ve OFF pozisyonu olan Start Lever'lar DEU'lari enerjileyerek start valfin açilmasini saglarlar

	Erstellt von GlideSlope localizer vor fast 4 Jahre

Nächster

ENGINE VAKIFBANK

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