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SIMULATOR > E195 > Flashcards

E195 Flashcards

1
Q

The FADEC have any protection for in flight engine start ?

A

The FADEC has no protection for hot starts, hung starts or failure to light off for in flight engine starts.

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2
Q

The FADEC is power by ?

A

Above approximately 50% N2 the FADEC is powered by the Permanent Magnet Alternator (PMA).

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3
Q

The FADEC protect the engine start in ground for ?

A

Hung start.

– Hot start.

– No light-off

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4
Q

MTOW AND MLDW E195 AR , LR , 190

A

AR:52.290/45.800
LR:50.790/45.000
190:51.800/44.000

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5
Q

MAX HWIND CATII

A

25KT

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6
Q

MAX CWIND CATII AND LVTO

A

15KT (AD)

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7
Q

MAX CWIND TO/LAND DRY

A

25KT

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8
Q

MAX CWIND TO/LAND WET

A

20/15 KT

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9
Q

MAX CWIND TO/LAND CONTAMINATED GROOVE OR NO

A

10 AND NO GROOVED 5 KT

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10
Q

MAX CWIND TO/LAND RWY < 1700M x 40M OR LESS DRY

A

15KT

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11
Q

MAX CWIND TO/LAND RWY < 1700M x 40M OR LESS

A

5KT

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12
Q

EMBREAR 190/195 ALTITUDES

A 
410 capability 
330 apu electrical
310 single pack
300 apu start
210 apu engine assist start
200 use of flap
150 apu bleed supply
100 max takeoff alt
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13
Q

Max differential pressure

A

8.4psi

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14
Q

Max negative differential pressure……….

A

-0.5

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15
Q

Min autopilot use

A 
OFF:
50ft below DA
MDA
ON:
ACCELERATION ALT OR 400 AGL
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16
Q

ENGINE START TIME LIMIT

A

1.30m(90Sec) ground

2m(120sec) flight

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17
Q

Max speed for windshild wipers

A

250 ad

253 Embraer

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18
Q

Max speed for direct vision window

A

160 kt

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19
Q

The T/O DATASET MENU on the MCDU must be set to ENG

A

when OAT is between 5ºC and 10ºC and;

• there is any possibility of encountering visible moisture up to 1700 ft AFE.

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20
Q

The TO DATASET MENU on the MCDU must be set to ALL in the following cases:

A

when OAT is below 5ºC and;

• if there is any possibility of encountering visible moisture up to 1700 ft AFE.

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21
Q

Max differential over pressure

A

8.8psi

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22
Q

Max itt ground start

A

740 degrees

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23
Q

Max itt in flight start

A

875 degrees

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24
Q

Max itt

A

960 degrees

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25
Q

Max oil temp

A

155 degrees

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26
Q

Min valeu for last min change in the loadsheet

A

225kg

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27
Q

GP Seq modes for LOC app

A

Heading-V/L-NAV

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28
Q

Cabin masks deploy at ?

A

Between 14.000 and 14.750 ft

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29
Q

Diferença trim load e-perf

A

0.3 max

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30
Q

Bleed source priority

A

On-side
Off-side
Apu

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31
Q

Apu. Fuel consume

A

2kg/min

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32
Q

Contaminated runway is

A

25% full of steady water with 3mm or 1/8pol or rwy with snow or slush

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33
Q

Flight by wire components?

A 
3 p-ace (elevator)
2 sf-ace(slat flap)
1 hs-ace(horizontal stabilizer
3 s-ace spoilers
4 FCM flight control modules
34
Q

Who much time the flight by wire battery less?

A

15min

35
Q

Takeoff pitch single engine ?

A

Pith 8

36
Q

When ground spoilers retract after landing

A

Below 45kt after 5s

37
Q

With CWIND limit for aileron jammed

A

10kt cross wind

38
Q

Speed tape shows the speed ahead in who much time ?

A

10’s

39
Q

The altitude tape shows the altitude ahead in how much time

A

6s

40
Q

How much miles for CB deviation

A

25nm

41
Q

When do wee do de appr 1 callout

A

1000 AFE

42
Q

Engine fail above v1 call outs

A 
V1
Engine fail,fire
Check thrust
Reserve or no reserve
Rotate
Positive climb
Gear up
Nav
Checked
FLCH,FMS SPEED VFS
checked
Activate engine out
Confirm
Confirmed 
Flaps 0 after takeoff checklist
Speed check flaps 0
After takeoff checklist complete
Set con
My controls and atc qrc or qrh checklist ...
43
Q

Takeoff briefing sequence

A 
CRM
WEATHER
NOTAMS
AIRPORT DIAGRAM(seto)
SID
REJECTED TAKEOFF
AIRPORT BRIEFING 
TOW
44
Q

approach briefing sequence

A 
QRH
ATIS
START
IAC
AIRPORT DIAGRAM
AIRPORT BRIEFING 
PERFORMANCE 
FUEL
NOTAMS
UP TO DATE WEATHER 
SPECIAL MEL DDPM
45
Q

When the TCAS RA become inhibit

A

The TCAS automatically reverts to TA ONLY mode and inhibits RAs for altitudes below 900 ft AGL during descent, or below 1000 ft during climb.

46
Q

PILOT INCAPACITATION FLOW

A
  • VOAR/NAV/COMM
  • Where to go?
  • Cmte ta tudo bem?
  • START ICCCC
  • MAY DAY 3X
  • REQUEST WEATHER CONDITIONS TO CLOSE AIRPORT
  • 7700 !!
  • DECIDE WHERE TO GO AND REQUEST DCT IAF(hold)
  • ADVISE MIN AWAY FROM FREQ
  • CMS(incapacitation,medic onboard,extra crew)
  • Company(incapacitation,tell where I decide to land,good?,puch truck,ambulance)
  • Prepare captain and TEST BRIEF WITH CMS
  • SPEECH
  • FREQ-POB,AUTONOMIA,CARGA PERIGOSA)avisar TWR azul vai parar na pista
  • Prepare the aircraft for land (CAPTAIN SIDE TOO)
  • Do ALL THE BRIEFING , CHECKLISTS AND CALLOUTS IN LOUD VOICE
  • STOP ON THE RUNWAY,PARKING BRAKE ,PA, TURN ON APU , AFTERLANDING CHECKLIST, TURN OFF ENGINES , PARKING CHECKLIST
  • HELP THE CAPTAIN
47
Q

Pilot incapacitation speech

A

Senhoras e senhores clientes , aqui é seu primeiro oficial igor para comunica-los que estamos retornando ao aeroporto ….. tendo em vista que nosso comandante não esta se sentindo apto a continuar o voo. Segurança e o nosso valor principal e portanto devido as normas da empresa não será possível dar continuidade ao nosso voo. Em nome da azul peço desculpas aos transtornos e após o nosso pouso nossa equipe de solo ira prestar os demais cuidados a todos. Muito obrigado pela sua atenção

48
Q

What to do in a elevator jammed in takeoff run ?

A

Use elevator trim to rotate

49
Q

Memory Itens !!

A

Cockpit/Cabin Smoke/Fumes

Oxygen Masks ………………………………….. ON, EMER

Crew Communications ……………………… Establish

CABIN ALTITUDE HI

Oxygen Masks …………………………………………. ON, 100%

Crew Communications …………………………….. Establish

Jammed Control Column - Pitch

ELEVATOR DISCONNECT Handle………….Pull

Working Pitch Control ………………………….Identify & Assign PF

Jammed Control Wheel - Roll

AILERON DISCONNECT Handle …………… PULL

Working Roll Control …………………………… Identify & Assign PF

Trim Runaway

AP/TRIM DISC Button ……………………….. PRESS and HOLD

Nosewheel Steering Runaway

STEER DISC Switch ………………………….. PRESS

EGPWS / Windshear Recovery Maneuver

Thrust……………………………………………MAX (Press TO/GA) Autothrottles …………………………………Disengage Autopilot ……………………………………….Disengage Bank Angle ……………………………………Wings Level Pitch:

EGPWS ……………………………………………Pitch 20º Limited to PLI Windshear………………………………………..Fly FD command Speed Brakes ………………………………..FULL CLOSE Gear/Flaps …………………………………….. Maintain configuration until terrain clearance is assured

TCAS Maneuver

Autopilot…………………………………………………………….Disconnect

FPV ……………………………………………………Fly into FLY-TO ZONE

FD OFF …………………………………………………………………..Request

50
Q

Dual EFB fail

A

QRH additional procedure

Request chart introduction from ATC

51
Q

EPERF sequence for MTOW calculation

A 
TO-1
ESC-OFF
MACTOW-18.0
Static TO
Send via ACARS the MTOW with the ATIS information used 
Ex.
MTOW 44243 - M

Ref: Dim manual

52
Q

Minimums for Takeoff below 350 RVR

A

Refer to AIP , no takeoff should be attempted with RVR -350 if the airport doesn’t have stop bars lights installed in all runway holding. In Brazil only SBGR have !

53
Q

IDG amber light means?

A

high oil temp or low oil press in the associated IDG

54
Q

Cockpit commands that require confirmation of both pilots?

A 
2 IDGs
2-Fire Handles 
2-Start Stop Switch’s 
2-Thrust Levers
Aileron DISC
Elevator DISC
55
Q

Runway lights Distances…

A

Each Runway Edge Light(REL) - 200ft(60m) if a crossing taxiway or runway should not exceed 400ft(120m)
And they should be min 2ft(0.6m) to 10ft(3m)
From the actual runway edge.

For an instrument runway, install yellow runway edge lights on the last 2000 ft(610m) or one-half the runway length, whichever is less.

RCLL pr RCL - Runway center Line
RCL are spaced at 50ft(15m) with deviation of maximum of 2.5ft(0.7m) from the real runway center.
From 3000ft(915m) to 2000(610m) RCL goes to yellow and in the last 1000(305m) red

56
Q

SDU OPS

A

After parking checklist EPERF and send via acars

Rwy 20 TO

Preparação:

  • Inserir na DEP/APP SPEEDS V2+10 até 1.500ft;
  • Decolar com FMS Speeds;
  • Decolar com VNAV e LNAV armados;
  • Iniciar curva a esquerda a 200ft para a proa 155° com bank 15° até 400ft, quando o bank poderá ser aumentado para 25° a 30°;
  • Iniciar retração de flaps a 1.500 ft;
  • O sobrevoo do Morro do Pão de Açúcar não é permitido;
  • O PM notificará o PF quando livre do Morro do Pão de Açúcar para o início da curva a direita seguindo o perfil da SID. Nas saídas com curva á esquerda este callout não é necessário;
  • Contato automático com o controle RIO a 1.500ft (a TWR não informará o horário de decolagem).

DECOLAGEM - EJET RWY 02

  • Iniciar curva a direita a 400ft, no perfil da SID;
  • Decolar com FMS Speeds;
  • Decolar com VNAV e LNAV armados;
  • Gerenciar a necessidade de subir na V2+10;
  • Não ultrapassar a Ponte Rio-Niteroi;
  • Contato automático com o controle RIO a 1.500ft (a TWR não informará o horário de decolagem).

ESTABILIZAÇÃO 300FT !!
Após 400ft pode prosseguir pouso com pane

  1. 4.1.3.1. Restrições
    a. Reporte de Windshear;

b. Componente de vento de cauda superior a 5kt (principal e auxiliar);
c. Componente de vento de través (incluindo rajadas) superior a 15kt;
d. Presença ou reportes de poças de água na pista;
e. Chuva moderada ou forte na área da aproximação final ou sobre a pista;
f. Formação de CB nas trajetórias de decolagem e aproximação a menos de 5nm do aeroporto;
g. Indicador de velocidade não confiável;
h. Inoperância de itens MEL restritivos ao SDU;
i. Perda de 2 geradores dos motores;
j. Qualquer condição que altere a configuração de pouso de FULL FLAPS e respectiva app speed;
k. Abertura automática dos spoilers inoperante;
l. Um motor inoperante exceto conforme descrito em Falha de Motor na Final acima.

57
Q

CGH OPS

A

EPERF MTOW SEND VIA ACARS

If wet runway the takeoff thrust must be the maximum!

Limites

LIMITES DE VENTO:

COMPONENTE DE TRAVÉS:

• 15kt

COMPONENTE DE CAUDA :

  • Seca: 5 Kt
  • Molhada: 0 Kt

B.6. Operação Proibida

  • Inoperância de componentes que comprometam a performance de frenagem:
  • superfície de comando, freio, reverso, etc.
  • Previsão de Wind-shear
  • Pista contaminada
  • Pista molhada:

A. qualquer vento de cauda

B. través: mais de 15 Kt (Azul)

C. redução de potência (Derated ou Flex)

PISTA AUXILIAR – A utilização da pista auxiliar é permitida somente em voos de traslado, sem Clientes a bordo.

EXTRA-FUEL

• Fica como limite de extra-fuel para as aeronaves com destino a CGH 3.000kg acima do MFOD regulamentar_

58
Q

The fire protection system provides fire detection and extinguishing capabilities for?

A

– Engines
– APU
– Cargo Compartments
– Lavatories

59
Q

ENGINE FIRE PROTECTION SYSTEM

A

– Engine fire detection;
– Engine fire extinguishing and;
– Continuous Built-In Tests to detect internal faults.

60
Q

Anytime the fire handle is pulled it

A

– the engine fuel shutoff valve
– the engine hydraulic shutoff valves
– the engine bleed air shutoff valve
– the cross bleed shutoff valve.

61
Q

CAS Message or red bottom light is the correct indication for fire ?

A

– the engine fuel shutoff valve
– the engine hydraulic shutoff valves
– the engine bleed air shutoff valve
– the cross bleed shutoff valve.

62
Q

When the APU FIRE EXTINGUISHER button is pressed the system?

A

– discharges the APU fire bottle.
– shuts down the APU through the APU FADEC.
– closes the APU fuel shutoff valve (SOV).
– displays an EICAS ADVISORY message APU FIREX BTL DISCH.

63
Q

Who much time without APU EMER STOP pushbutton has been pressed, the APU fire extinguisher pushbutton illuminates ?

A

1 minute. Pressing the APU fire extinguisher pushbutton, discharges the extinguisher bottle, shuts down the APU and turns OFF the red striped bar on the APU EMER STOP pushbutton.

64
Q

On ground, the APU will automatically shut down …

A

10 seconds after the fire condition is present.

65
Q

cargo compartments on the E-JETS are?

A

Class C

66
Q

Number of smoke detector in each compartment?

A

The forward cargo compartment has four smoke detectors. The aft cargo compartment has three smoke detectors.

67
Q

The Cargo Fire Extinguishing System is comprised of?

A

– One high-rate extinguisher bottle and;

– One low-rate extinguisher bottle.

68
Q

CARGO COMPARTMENT FIRE EXTINGUISHING - WITH MESSAGE

A

IN-FLIGHT:
High-rate- push the button once
Low-rate- automatic after 1 min

ON-GROUND
High-rate: push the button once
Low-rate: push the button once

69
Q

CARGO COMPARTMENT FIRE EXTINGUISHING - WITHOUT MESSAGE

A

IN-FLIGHT
High-rate: push the button twice
Low-rate: automatic after 1 min

ON-GROUND
High-rate: push the button twice
Low-rate: push the button once

70
Q

AC system is composed

A

– Two integrated drive generators (IDGs).
– One auxiliary power unit (APU) generator.
– One inverter.
– One ram air turbine (RAT).
– One AC external power unit.

71
Q

DC system is composed

A

– Two NiCd batteries.
– Three transformer rectifier units (TRU)s.
– One DC external power input.

72
Q

IDG 1 (2) OIL display when?

A

When IDG oil pressure drops below 140 psi ± 25 psi, or the IDG oil temperature reaches 335°F ± 10°F (168°C ± 5°C), the EICAS message IDG 1 (2) OIL is displayed and an amber led illuminates near the IDG selector knob on the overhead panel. This LED indicates which IDG must be disconnected

73
Q

Automatic IDG disconnection occurs when?

A

Automatic IDG disconnection occurs when manual disconnection is not performed, and the IDG oil temperature reaches 366°F (185.6°C).

74
Q

RAT TIME REQUIRE FOR SUPPLY AC/DC ESS BUSs and min speed to work?

A

8s,and 130kt

75
Q

batteries supply essential loads for?

A

10min

76
Q

Numbers off ICCs

A

Left Integrated Control Center (LICC).
– Right Integrated Control Center (RICC).
– Emergency Integrated Control Center (EICC).
– Auxiliary Integrated Control Center (AICC).

77
Q

To config

A

Flaps
Trims green
Parking brake
Spoilers

78
Q

How to declare mayday

A

Nome da estação chamada;

  • Identificação da aeronave;
  • Natureza da condição de emergência;
  • Intenção do Piloto em Comando;
  • Posição, nível e proa;
  • Qualquer outra informação útil.

MAYDAY MAYDAY MAYDAY, Torre Campinas, Azul 4-2-8-8, perda de motor na decolagem, mantendo rumo da pista subindo para 6 mil pés”

79
Q

For how long the cargo low rate fire extinguishing bottle remains?

A

75 minutes for airplanes with 60- minute diversion time allowed.

80
Q

Max fuel capacity

A

13100kg

81
Q

The emergency/parking brake system has pressure accumulators isolated from both normal hydraulic systems. The accumulators have sufficient pressure to provide how much full brake applications?

A

6

82
Q

Go around callout OEI ?

A

Go around flaps check thrust!

SIMULATOR (1 decks)

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