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Modul11 Flashcards

1
Q

Dogru akim generatoru DC

A

karbon pine

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2
Q

ATIMS

A

air traffic and information management system

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3
Q

Hms nin amaci

A

Ucaak sistemlerini gozetlemek
Ucak havadayken tsm yapmak

AIRMAN

Hms(healt management system)

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4
Q

Efb nin icinde neler var

A

Aircraft operating manual
Flight crew oper manual
Navigation charts

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5
Q

ATSU mode leri.

Mode S

A

Tansponder air to air

Transponder ground to air data up link

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6
Q

Controller ile pilot arasindaki temasi kim saglar

A

Controller pilot dataLink communication

CPDLC

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7
Q

CPDCL

A

Controller pilot dataLink communication

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8
Q

Cabin intercom data system ana parcasi

A

CSSC

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9
Q

Deu-A

A

Pass service unit(PSU)

CABIN LIGHT

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10
Q

Deu-B

A

Area call panel (ACP)
attendent indication panel(AIP)
hand set
Additional attendent panel(AAP)

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11
Q

Cabin monitoring system

A

Gizli kameralar var

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12
Q

Konusmada oncelik

A 
Emergency
Captain
Purser
Conferance
Miscellenous
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13
Q

MPEG acilimi

A

Motion picture

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14
Q

IMA

A

Integral moduler avionic

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15
Q

IMA

A

Bir computer icine birden fazla computer koyuluyor

Agirlik ve kablo sayisi az

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16
Q

ADCN

A

Avionic data communication network(airbus)

Communucate between IOM and CPIOM

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17
Q

Communucate between IOM and CPIOM

A

ADCN

avionic data communication system

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18
Q

CDN

A

common data network (boeingte)

Comminucate between GPMs

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19
Q

ADFX

A

Avionics full DupleX

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20
Q

Controller Area Network( Can) Bus

A

Dosyayi ilgili yere iletir

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21
Q

Central Maintenance System(CMS) operating modes

A

Normal mode—-on ground and in flight

Interactive mode —–only on ground

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22
Q

AIRMAN

A

Aircraft maintenance analys

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23
Q

BITE TEST

A

Power up
Cyclic test
System test
Spesific test

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24
Q

Data Loading System

A

Auto—download and upload(ucagin sistemine yuklemek)

Manual—-only download

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25
Q

1 candela

A

1 candela power====about 0.981candela

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26
Q

EPSU

A

Emergency lightlarin kendi bataryasi

Emergency lightlar hem AC hem de DC

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27
Q

Yangin tipleri

A 
A class-----wood---su 
B class------gasoline----halon(pylon-engine fuel)
C class------gas------foam
D class -----magnesium-------Dry powder
F class----cooking oil-----dry powder
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28
Q

Fire protection sys amaci

A

Detection

Extinguish

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29
Q

Fire zones

A

Class A—-Visual detection —-No detector
Class B—- Seperate smoke detector system and
— Erisilebilir

Class C—–smoke detector var , erisilemiyor

Class E—–Only cargo Aircraft

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30
Q

Fuel shut off valve

A

Spar valve

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31
Q

Kokpitte yangin sondurucu olarak

A

HALON kullanilir

CO2 kullanilmaz

Halon kabinde kullanilmaz

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32
Q

APU extinguisher sari—kirmizi???

A

Kirmizi gorunmuyor ise —–overpressure (kendi patlamis)

Sari gorunmuyor ise —–kaptan patlatmis

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33
Q

Ic direnci en fusuk batarya

A

Ni-Cad

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34
Q

Şarj yontemleri

A

Constant voltage
Constant current
Pulse

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35
Q

CSD(constant speed drive unit)

A

Generatoru sabit hizda dondurmeyi saglar

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36
Q

IDG

A

Csd+constant generator

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37
Q

Frekans formulu

A

60f=N×x——(Herts)

N=Rpm

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38
Q

Voltage regulators

A 
Carbon pile
Vibrator type
Three-unit
Solid-state
Magnetic Amplifier
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39
Q

Voltage regulator

A

Senses any diff between REFERENCE voltage and GENERATOR OUTPUT voltage

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40
Q

Priority sirasi

A

IDG GEN2
EXTERNAL POWER
APU GEN
OFFSIDE IDG GEN

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41
Q

Sheddable Bus

A

Galley IFE buslari gibi kesilebilir buslardir

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42
Q

Static inverter

A

Emergency durumlarda DC Bat busdan Ac essencial Busi besler

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43
Q

Ac essencial Bus

A

Ac bus 1 den beslenir normalde

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44
Q

Flight director

A

Pfr-ADR

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45
Q

Glide slop acissi

A

2.5–3 derece

1 derece fark olur ise GPWS warning verir

GPWS(ground proximity warning system)

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46
Q

ADF

A

Auto Directional Finder

Non directional beaker

Morse sinyali var

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47
Q

VOR

A

Receive
Decode
Process to other systems

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48
Q

Marker beacon

A

Distance between A/C and runway threshold(alt sinir)

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49
Q

Marker beacon renkleri

A

Inner marker—-white
Middle marker—–amber
Outer marker—-Blue

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50
Q

RA calisma yuksekligi

A

2500 feet altinda

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51
Q

GWPS RA iliskisi

A

GWPS RA dan sinyal alir.

Sesli ve gorsel ikaz var

52
Q

ATC CALISMASI NASIL

A

Ucak-ucak
Ucak-yer

Yazili bilgiler iletilir

53
Q

Tcas zorunlulugu

A

5700 kg ve 19 passenger ustu

54
Q

ATC calismaz ise

A

TCAS calismaz

55
Q

ATC

A

Air traffic controller transponder

56
Q

Fms

A

28 gunde bir

57
Q

OBRM

A

On board replaceable Module

Ucaktaki yukleme bilgisayari

Internal system software

58
Q

ACARS

A

Communication Adressing and Reporting System

59
Q

ACARS nasil calisir

A

MCDU uzerinden yazi gonderilie
Yerden havva-havadan—–yazi yollanir
Auto or Manual
ARINC OR SITA database

60
Q

CVR bulunma şarti

A

5700 kg ustu ve 9 yolcu

61
Q

CVR MOTOR durduktan kac dakka sonra

62
Q

Under water beacon

A

CVR uzerinde bulunur

63
Q

Senchronisation

A

A/p varken devrede

A/ devrede degilken birseye dokunmasak yine var

64
Q

A/p devreden cikma sarti

A

Bozulursa

Side stick red button

65
Q

A/P axis ?

A

Single—lateral stabilisation or wing levelling(roll ekseni)
Two—Roll/Pitch
Three–roll/putch/yaw

66
Q

Small aircraft axiss

A

Single , roll axis

67
Q

QNH
QFE
QNE

A

QNH——A/C—–SEA LEVEL
QFE——–A/C—TERRAIN
QNE——–A/C—-STANDART PRESSURE REFERANCE

68
Q

Controll loop

Control and Actuating Device

A

Verdigimiz hareketi hizliyken sinirlamak gibi gorevleri vardir

69
Q

Inner/outher loop sensorler

A

Inner-own sersors

Outher-navigation sens

70
Q

Yaw daper gorevleri

A

Dutch roll
Turn coordination
Engine fail compensating

71
Q

Statik tikarsa

A

Airspeed
Verticle speed
Altitude

Gider

72
Q

Pito tikanirsa

A

Airspeed gider

73
Q

Mach hesaplamasi

A

Mach=TAS/ LOCAL SPEED OF SOUND

74
Q

Attitude Director Indicator ADI nereden faydalanir

A

Verticle gyro

75
Q

Rate Gyro ne ise yarar

A

3 sens ivme olcumu

Tun and slip
Turn coordination
Auto pilot

76
Q

ATA

A

Air Transportation Association

77
Q

1000 feet de derece

A

2 derece azalir

78
Q

SAT

A

Statik air temperature

Dis sicaklik

79
Q

Pito ile ne hesaplanie

80
Q

Dynamic pressure

A

Pd=1/2(d.vkare)

81
Q

VMO—-velocity max operating
VMM—velocity max mach

Overspeed warningler

A

Vmo-bu deger asilinca kirmizi band

Vmm-ustekinin aynisi , mac kullananlarda var

82
Q

Flux valve

A

True northu gosterir

Manyetik alanin akisini olcerek

83
Q

ICE-T

A

IAS—–INSTRUMENT ERROR CORRECTION++++
ASIR(AIR SPEED INDICATOR READING)

CAS===IAS++++PRESSURE ERROR CORRECTIOM
EAS===CAS++++COMPRESSIBILTY ERROR CORRECTION
TAS===EAS++++DENSITY ERROR CORRECTION

84
Q

Deviation nedir

A

Compass reading ile Earth Magnetic Field arasindaki fark

85
Q

Basic T

A

ASI. ADI. ALT

TURN. HDG. VSI

86
Q

ADI

A

Altitude director indicator

87
Q

Verticle gyro

A

Roll pitch hareketi gosterir

88
Q

ADI ATTITUDE DIRECTOR INDICATOR

A

Primary
Roll pitch yaw

Brown=earth
Blue=sky

89
Q

Standby compass

A

Magnetic north

90
Q

Inclination

A

Pusulasinin kutuplarda yeri gostermesine denir

Agirlik baglanarak duzeltilir

91
Q

Compass ne zaman yanlis goterir

A

Kutuplarda

Variation===magnetic north ile–geographic nort arasi fark

Deviation===sapma (between compass reading and magnetic feeli g)

92
Q

Flux valve

A

Magnetic alani olcelerk DIRECTIONAL GYRO NUN kuzeyi gostermesini saglar

Yoksa biz ayarlariz

93
Q

Stall warning

A

Angle of attcak

Hiz a baglidir

94
Q

Stagnation point

A

Havanin kanada carptigi bolge

95
Q

Angle of attack acisi neresi

A

CHOR ILE RELATIVE WIND arasindaki acidir

96
Q

DRC

A

Direct reading compass

Manyetik kuzeyi gosteirir

Windshield

97
Q

Hareket iletimi

A

Push pull road

Torqu tube

98
Q

Ailerion drop function

A

Aileronlarin simetrik olarak asagi inmesi

99
Q

LAF LOAD ALLEVIATION FUNCTION

ACTIVE LOAD CONTROL

A

Gorevi , verilen kumandayi kolaylastirmak

100
Q

LAF KIM TARAFINDAN GERCEKLESTIRILIR

A

EFCS(ELECTRICAL FLIGHT CONTROL SYSTEM)

101
Q

Active load control

A

Load alleviation function

LAF

102
Q

Servo ciftleri

103
Q

PPU

A

Position Pick-off Units

104
Q

FPPU

A

Flap/slatin. Konumunu bildirie

105
Q

APPU

A

Asymetric ppu. FPPU dan gelen sinyallere bakarak asymetri var mi kontrol eder

106
Q

PPU

A

Lvdt

Rvdt ile sens alir

107
Q

Torque limiter

A

Yuklerden dolayi asiri stressten kontrol yuzeylerini korur

108
Q

Stick shaker inputs ?

A

A/a sensors

Flap/slat position

109
Q

Stall onleme systemleri

A

Stick shaker
Stick pusher
Stall strips

110
Q

Flybywire sistemde kontrol yuzeyleri

A 
Hem mekanik(hydraulic)
Hem de elektriki kontrol edilie
111
Q

Servo jacklerde 3 mode

A

Active—electrical control

Damping==follow surface movement

Centering===neutral positiona hydraulici donusu

112
Q

Offset

A

Demand ile feedback arasindaki fark

Ornegin , flap 4 sectik fakat flap 3 de .

113
Q

Drain check valve

A

Manevra sirasinda kanat ucuna yakit gitmesini engeller

114
Q

Float valve

A

Havalandirma yaparken yakitin vent hattina gitmesini engellemek

115
Q

Rubber check valve

A

Vent hattina yakit girerse onu tanka drain eder

116
Q

Jet pump 2 girisi vardir

A

Booster pump

Tank dibinden (induced flow)

117
Q

Crossfeed valve

A

28 v dc

Pompa bozulursa , bozulan tarafi digeri besler

Normalde kapalidir

118
Q

Cg nasil hesaplanir

A

Mean aerodynamic chor line

119
Q

F=C(1.8)+32
C=(F-32)/1.8
K=C+273.15

120
Q

Mean Sea Level

A 
15 derece
1013 mb
1013hPa
29,92 inHg
14,7 psi
1225gr/mküp
121
Q

X
Y
Z
Stations

A

X-body station
Y-buttock lines
Z-water lines

122
Q

Doubler

A

Reduce stress

123
Q

Truss type structure

A

Only beams

124
Q

Monococ

A

Frame+skin

125
Q

Semi-monococ

A

Stringer-frame-skin

126
Q

Anti-skid system consist

A

Transducer
Control box
Control valve

Modul11 (2 decks)

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