E195 Flashcards
(82 cards)
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.
2
Q
The FADEC is power by ?
A
Above approximately 50% N2 the FADEC is powered by the Permanent Magnet Alternator (PMA).
3
Q
The FADEC protect the engine start in ground for ?
A
Hung start.
– Hot start.
– No light-off
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
5
Q
MAX HWIND CATII
A
25KT
6
Q
MAX CWIND CATII AND LVTO
A
15KT (AD)
7
Q
MAX CWIND TO/LAND DRY
A
25KT
8
Q
MAX CWIND TO/LAND WET
A
20/15 KT
9
Q
MAX CWIND TO/LAND CONTAMINATED GROOVE OR NO
A
10 AND NO GROOVED 5 KT
10
Q
MAX CWIND TO/LAND RWY < 1700M x 40M OR LESS DRY
A
15KT
11
Q
MAX CWIND TO/LAND RWY < 1700M x 40M OR LESS
A
5KT
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
13
Q
Max differential pressure
A
8.4psi
14
Q
Max negative differential pressure……….
A
-0.5
15
Q
Min autopilot use
A
OFF: 50ft below DA MDA ON: ACCELERATION ALT OR 400 AGL
16
Q
ENGINE START TIME LIMIT
A
1.30m(90Sec) ground
2m(120sec) flight
17
Q
Max speed for windshild wipers
A
250 ad
253 Embraer
18
Q
Max speed for direct vision window
A
160 kt
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.
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.
21
Q
Max differential over pressure
A
8.8psi
22
Q
Max itt ground start
A
740 degrees
23
Q
Max itt in flight start
A
875 degrees
24
Q
Max itt
A
960 degrees
25
Max oil temp
155 degrees
26
Min valeu for last min change in the loadsheet
225kg
27
GP Seq modes for LOC app
Heading-V/L-NAV
28
Cabin masks deploy at ?
Between 14.000 and 14.750 ft
29
Diferença trim load e-perf
0.3 max
30
Bleed source priority
On-side
Off-side
Apu
31
Apu. Fuel consume
2kg/min
32
Contaminated runway is
25% full of steady water with 3mm or 1/8pol or rwy with snow or slush
33
Flight by wire components?
```
3 p-ace (elevator)
2 sf-ace(slat flap)
1 hs-ace(horizontal stabilizer
3 s-ace spoilers
4 FCM flight control modules
```
34
Who much time the flight by wire battery less?
15min
35
Takeoff pitch single engine ?
Pith 8
36
When ground spoilers retract after landing
Below 45kt after 5s
37
With CWIND limit for aileron jammed
10kt cross wind
38
Speed tape shows the speed ahead in who much time ?
10’s
39
The altitude tape shows the altitude ahead in how much time
6s
40
How much miles for CB deviation
25nm
41
When do wee do de appr 1 callout
1000 AFE
42
Engine fail above v1 call outs
```
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
Takeoff briefing sequence
```
CRM
WEATHER
NOTAMS
AIRPORT DIAGRAM(seto)
SID
REJECTED TAKEOFF
AIRPORT BRIEFING
TOW
```
44
approach briefing sequence
```
QRH
ATIS
START
IAC
AIRPORT DIAGRAM
AIRPORT BRIEFING
PERFORMANCE
FUEL
NOTAMS
UP TO DATE WEATHER
SPECIAL MEL DDPM
```
45
When the TCAS RA become inhibit
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
PILOT INCAPACITATION FLOW
- 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
Pilot incapacitation speech
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
What to do in a elevator jammed in takeoff run ?
Use elevator trim to rotate
49
Memory Itens !!
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
Dual EFB fail
QRH additional procedure
Request chart introduction from ATC
51
EPERF sequence for MTOW calculation
```
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
Minimums for Takeoff below 350 RVR
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
IDG amber light means?
high oil temp or low oil press in the associated IDG
54
Cockpit commands that require confirmation of both pilots?
```
2 IDGs
2-Fire Handles
2-Start Stop Switch’s
2-Thrust Levers
Aileron DISC
Elevator DISC
```
55
Runway lights Distances...
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
SDU OPS
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
14. 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
CGH OPS
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
The fire protection system provides fire detection and extinguishing capabilities for?
– Engines
– APU
– Cargo Compartments
– Lavatories
59
ENGINE FIRE PROTECTION SYSTEM
– Engine fire detection;
– Engine fire extinguishing and;
– Continuous Built-In Tests to detect internal faults.
60
Anytime the fire handle is pulled it
– the engine fuel shutoff valve
– the engine hydraulic shutoff valves
– the engine bleed air shutoff valve
– the cross bleed shutoff valve.
61
CAS Message or red bottom light is the correct indication for fire ?
– the engine fuel shutoff valve
– the engine hydraulic shutoff valves
– the engine bleed air shutoff valve
– the cross bleed shutoff valve.
62
When the APU FIRE EXTINGUISHER button is pressed the system?
– 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
Who much time without APU EMER STOP pushbutton has been pressed, the APU fire extinguisher pushbutton illuminates ?
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
On ground, the APU will automatically shut down ...
10 seconds after the fire condition is present.
65
cargo compartments on the E-JETS are?
Class C
66
Number of smoke detector in each compartment?
The forward cargo compartment has four smoke detectors. The aft cargo compartment has three smoke detectors.
67
The Cargo Fire Extinguishing System is comprised of?
– One high-rate extinguisher bottle and;
| – One low-rate extinguisher bottle.
68
CARGO COMPARTMENT FIRE EXTINGUISHING - WITH MESSAGE
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
CARGO COMPARTMENT FIRE EXTINGUISHING - WITHOUT MESSAGE
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
AC system is composed
– Two integrated drive generators (IDGs).
– One auxiliary power unit (APU) generator.
– One inverter.
– One ram air turbine (RAT).
– One AC external power unit.
71
DC system is composed
– Two NiCd batteries.
– Three transformer rectifier units (TRU)s.
– One DC external power input.
72
IDG 1 (2) OIL display when?
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
Automatic IDG disconnection occurs when?
Automatic IDG disconnection occurs when manual disconnection is not performed, and the IDG oil temperature reaches 366°F (185.6°C).
74
RAT TIME REQUIRE FOR SUPPLY AC/DC ESS BUSs and min speed to work?
8s,and 130kt
75
batteries supply essential loads for?
10min
76
Numbers off ICCs
Left Integrated Control Center (LICC).
– Right Integrated Control Center (RICC).
– Emergency Integrated Control Center (EICC).
– Auxiliary Integrated Control Center (AICC).
77
To config
Flaps
Trims green
Parking brake
Spoilers
78
How to declare mayday
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
For how long the cargo low rate fire extinguishing bottle remains?
75 minutes for airplanes with 60- minute diversion time allowed.
80
Max fuel capacity
13100kg
81
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?
6
82
Go around callout OEI ?
Go around flaps check thrust!
