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Airbus 320 Prova > Airbus > Flashcards

Airbus Flashcards

1
Q

Qual a definição de abnormal atitude?

A

Pitch maior que 25˚ ou abaixo de - 10˚ e bank > 45˚

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2
Q

Call out para Stall at Lift-Off ?

A

“Stall TOGA 15˚”

TOGA,
pitch 15˚
Wings level

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3
Q

Qual a máxima diferença entre altímetro no RNP-AR?

A

100ft

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4
Q

Onde se verifica se aeronave pode realizar RNP-AR?

A

EO

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5
Q

Diferença entre CB verde e preto?

A

Verde é monitorado, triga ECAM após 60 seg e preto não é monitorado.

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6
Q

Envergadura do A320 e A321?

A

35,80 m

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7
Q

Max landing weight A321?

A

79.200kg

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8
Q

Velocidades de Trem?

A

VLE – 280kt ou M.67

VLO ext – 250kt ou M.60

VLO ret – 220kt ou M.54

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9
Q

Quais ações para falha de motor em cruzeiro? STD STRATEGY

A 
All THR Levers to MCT
A/THR OFF
HDG: TURN AND PULL
DETERMINE EO LRC ceiling ALT (REC MAX ON PROG PAGE)
ATC NOTIFY

DESCENT:
SPEED MACH 300/0.78
ALT FCU PULL

WHEN V/S BECOMES LESS THAN -500 FT/MIN
V/S SET -500 FT/MIN AND PULL
A/THR ON
SPD MANAGE

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10
Q

VMO e MMO do A320 e A321?

A

350kt e M .82

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11
Q

Limite de velocidade para abertura da janela?

A

200kt

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12
Q

Pode-se usar SOFT go around quando em single engine?

A

nao

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13
Q

Aeronave pode ser despachada sem TLB?

A

Não pode, segundo MGO CAP 11.

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14
Q

SDU Performance Calculation onde ?

A

QRH

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15
Q

RNP-AR

O que se deve checar para realizar?

A

EO

Nenhum item mel.

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16
Q

STALL RECOVERY

A

STALL, I have control”

Nose down pitch

Asas niveladas

Aplica potência as necessary

Abaixo de 20.000ft – Flap 1

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17
Q

LOSS OF BRAKES

A

REV MAX

Brakes release

Anti skid off ORDER

Brake pedals APPLY

MAX BRK PRESS 1000 psi

If no BRK ACTION

     Parking Brake APPLY
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18
Q

Emergency evacuation

A

FO não precisa confirmar para acionar punhos de fogo no solo

Echo victor Echo victor é no EVACUTION initiate

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19
Q

Pouso mono e pouso normal, tem alguma diferenca?

A

Tudo igual inclusive pode fazer auto landing

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20
Q

OEI GO Around

A

Go around flaps

Flap X

FMA

Positive climb

Gear up

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21
Q

ENG FAILURE: When engine is secure?

A

Caso sem dano – Eng secure após master off

Com dano - Eng secure após AGENT 1 disch

Com fogo – Eng secure após AGENT 2 disch

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22
Q

TEST briefing

A

Tipo de emergência,

Se é para preparar a cabine para Evacuação

Sinais após o pouso (se não for parar sobre a pista, não haverá sinais)

Tempo para pouso (já ter preenchido FMGS para previsão)

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23
Q

Piloto da Azul conecta pode usar o jump seat?

A

Pode desde que esteja identificado com o crachá

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24
Q

Que fase do voo o uso do head set é obrigatório?

A

Do começo das comunições com ATC até 18.000 ft

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25
Q

Qual o call out do emergency descent?

A

Emergency descent

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26
Q

Quantas garrafas de extinção temos em cada motor? e no APU?

A

2 para cada motor

1 para APU.

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27
Q

Como funciona a extincao de fogo no APU?

A

automatica.

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28
Q

Qual o sistema hidráulico responsável pelo nose wheel steering?

A

yellow

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29
Q

Quais os tipos de frenagem no A320 neo?

A

Normal brake, alternate brake com Anti Skid, Alternate brake sem anti skid e parking brake

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30
Q

Mínimo de óleo do motor e como faz?

A

Após ligar o FADEC no painel de manutenção, min 8.9qt + 0.45qt/h com mínimo de 10.6qt

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31
Q

CAT II sem ALS?

A

nao pode

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32
Q

Tail Wind SDU?

A

5 kt seca e molhada

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33
Q

Max tail Wind do A320?

A

15 kt Airbus

10 kt Azul

34
Q

Minimo warm up time do motor?

A

3 minutos

35
Q

Momento correto para ligar a Y pump quando single engine taxi out?

A

após clearance de taxi

36
Q

Voltagem min da bateria na preparação do avião?

A

25,5 V

37
Q

Quando uma pista é considerada contaminada?

A

Mais de 3nm em 25% da pista

38
Q

Galley shed?

A

uando em voo estiver só um gerador alimentando o sistema

39
Q

A/THR operating rate single engine?

A/THR operating rate normal?

A

Idle até MCT

Idle até CL

40
Q

Nome do componente que transforma DC para AC ?

A

Static inverter

41
Q

RAT min speed no eletrical emerg ?

A

100 kt

E stall da hélice < 140 kts

42
Q

Comprimento A320?

A

37.57

43
Q

LOC only, como fazer?

A

Coloca Vapp no FDP

Seleciona o LOC ao invés de APPR

Não seleciona segundo AP

1NM antes do FDP seleciona -3.0FPA e 0.3NM pull

44
Q

ILS CAT II auto land, Durante o roll out que velocidade o PF deve desconectar o AP?

A

taxi speed

45
Q

Emergency descent speech e acoes?

A

PF “Atencão descida rápida, permanecam sentados, remain seated.”

PM - declara emergencia para o controle.
XPDR 7700
usem mascaras usem mascaras, use masks use masks

se nivelado antes do patamar de seguranca
- nivelados por XX minutos

Se nivelado no patamar de seguranca
- Nivelados no patamar de seguranca.

46
Q

Pilot incapacitation?

A

I have controls

40s para desativar o outro sidestick

47
Q

Tasksharing da panes?

A

Memory Itens ou OEB

ECAM

QRH

48
Q

UNREALIBLE AIRSPEED MEMO ITEMS

A

“UNREALIBLE SPEED”

AP, A/THR e FP OFF

15˚ TOGA below THR red

10˚ CLB above THR red and BLW FL100

5˚ CLB ABOVE FL100

Maintain CONF

Se CONF FULL – CONF 3

Speed break retracted

Gear UP

49
Q

STALL AT LIFT-OFF ?

A

“STALL TOGA 15˚”

TOGA,
pitch 15˚
WINGS LEVEL.

50
Q

STALL RECOVERY?

A

“STALL, I have control”

Nose down pitch

Asas niveladas

Aplica potência aos poucos

Abaixo de 20.000ft – Flap 1

51
Q

EMERGENCY DESCENT

A

“EMERGENCY DESCENT”

Máscaras e comunicação

PM – liga signs

PF – Turn and pull

    Turn and pull 

     Pull speed –  

    LEITURA DE FMA

THR levers IDLE e Speed break FULL

PM – Check e declara emergência e 7700

PF – “ATENÇÃO descida rápida, permaneçam sentados, remain seated

52
Q

TCAS MEMO ITEMS

A

“TCAS blue” ou “TCAS, I have control”

AP off

FD off

Follow the green band

53
Q

WINDSHEAR

A

“WINDSHEAR TOGA”

Follow SRS

Mantém configuração

54
Q

EGPWS MEMO ITEMS

A

“PULL UP TOGA”

AP OFF

PITCH PULL UP

Speed break retracted

WINGS LEVEL

MAINTAIN CONFIGURATION UNTIL CLEAR OF OBSTACLES.

55
Q

MEMORY ITEMS, QUAIS SAO ELES?

A

Unreliable airspeed

Loss of brakes
Emergency descent
Stall lift off
Stall in flight

Windshear
EGPWS caution and Warning
TCAS

56
Q

Quando a página de WHEEL SD estará disponível no pouso?

A

Aparece quando o trem de pouso está baixado com a aeronave abaixo de 15.500ft.

57
Q

Qual o range de temperatura do seletor do ar condicionado?

A

A temperatura trabalha com um range que vai de 18oC a 30oC e é selecionável em 7 posições de 2oC cada.

58
Q

Após 6 horas estando a aeronave desenergizada, qual o mínimo de bateria para assegurar uma
carga recomendada pelo fabricante?

A

Após 6hr precisamos fazer o teste da bateria e assegurar um mínimo de 25.5V, o que garante 50% de carga. Se a voltagem da bateria
estiver abaixo de 25.5V um ciclo de recarga utilizando uma fonte externa deve ser feito e requer pelo menos 20 minutos.

If the APU is started on batteries only, it should be started within 30 min after the selection
of batteries to AUTO (35 min after battery selection to AUTO, the battery charge is less than
25 % of maximum capacity

59
Q

APU FIRE TEST LIMITATION?

A

The automatic shutdown of the APU and the discharge of the APU fire extinguisher bottle may occur if the flight crew presses the APU FIRE test pb for
more than 3 seconds.

60
Q

QUANDO LIGAR O APU? (AZUL)

A

The APU start should be delayed until 5 minutes prior to the estimated time of departure or when
doors close, whichever occurs first. The APU may be started earlier in the following conditions:
a. When no external power unit is available;
b. When there’s no ACU available and the cockpit/cabin temperature is above 26°C or at or below
17°C;

61
Q

REFUELING LIMITATIONS

A

DO NOT TEST HF

IF APU SHUTDOWN DURING REFUEL, DO NOT RESTART

BAD WEATHER CONDITIONS

ELECTRICAL STORMS.

The external lighting is not operated (except for NAV & LOGO)

62
Q

REFUELING ON ENGINE RUNNING?

A

FCOM NORMAL PROCEDURES - SUPPLEMENTARY PROCEDURES-FUEL

63
Q

MANUAL START ENGINE, WHEN?

A

After aborting a start, because of:
• Engine stall
• Engine EGT overlimit
• Low start air pressure

64
Q

CROSSBLEED ENGINE START LIMITATION

A

Do not perform the crossbleed engine start procedure during pushback.
Simultaneous use of engine bleed supply and external pneumatic power supply is
prohibited

65
Q

IRS ALIGMENT, EXPLAIN FAST AND FULL ALIGMENT

A

FULL ALIGN - The IR mode selectors must be OFF for more than 5 s. Then, the flight crew sets the IR mode
selectors to the NAV mode

FAST ALIGN - The flight crew sets the IR mode selectors to OFF then, back to the NAV mode within 5s

66
Q

IRS ALIGN CHECK

A

On the POSITION MONITOR page, check that the IRS are in NAV mode, and check that the distance between each IRS and the FMS position is lower than 5 NM.

Select ND in ROSE NAV or ARC mode, and confirm that the aircraft position is consistent with the position of the airport, the SID and the surrounding NAVAIDs.

67
Q

TCAS TA/RA INHIBITION MODE?

A

DESCEND BLW 900 FT
CLIMB UP TO 1100 FT.

ALL- +2700 and - 2700
ABV- +9900 AND -2700
BLW +2700 AND - 9900
more info: FCOM - AIRCRAFT SYSTEMS - SURV - TCAS

68
Q

Quais as falhas que não são inibidas no ECAM durante a decolagem?

A

REJECT TAKEOFF

  • F/CTL sidestick fault;
  • Eng Fail;
  • Eng Reverse Fault;
  • Eng Reverse Unlocked;
  • Eng 1(2) THR Lever Fault.
69
Q

Quando não podemos utilizar Flexible Takeoff Thrust?

A

PISTA CONTAMINADA

SBSP WET

70
Q

START LIMITATION

A

‐ A standard automatic start that includes up to three start attempts, is considered one cycle
‐ For ground starts (automatic or manual), a 60 s pause is required between successive cycles
‐ A 15 min cooling period is required, subsequent to three failed cycles
‐ The starter must not be run when N2 is above 63 %.

71
Q

APU bleed limitations?

A

APU BLEED
Max altitude to assist engine start…… 20 000 ft

Max altitude for air conditioning and pressurization (single pack operation)……… 20 000 ft

Max altitude for air conditioning and pressurization (dual pack operation)…………..15 000 ft

TURNING ON 25 000 FT

Use of APU bleed air for wing anti-ice is not permitted.

72
Q

FUEL IMBALANCE AT TAKEOFF?

A

INNER TANKS (OUTER TANKS BALANCED)

Full ————————– 500 kg

3 000 kg —————– 1 050 kg

1 450 kg —————- 1 450 kg (3 196 lb)

73
Q

FUEL IMBALANCE IN FLIGHT AND AT LANDING?

A 
INNER TANKS (OUTER TANKS BALANCED)
Tank Fuel Quantity
(Heavier Tank) Maximum Asymmetry

Full —————————–1 500 kg
4 300 kg ——————– 1 600 kg
2 250 kg ——————– 2 250 kg

74
Q

ASSYMETRY OUTER TANKS?

A

690 KG

75
Q

DEFINITION OF ICE CONDITIONS

A

‐ Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is at or below 10 °C and visible moisture in any form is present (such as clouds, fog with visibility of 1 sm (1 600 m) or less, rain, snow, sleet or ice crystals).

‐ Icing conditions also exist when the OAT on the ground and for takeoff is at or below 10 °C and
operating on ramps, taxiways or runways where surface snow, standing water or slush may be
ingested by the engines, or freeze on engines, nacelles or engine sensor probes.

76
Q

Quando fazer rolling takeoff?

A

‐ Runway longer than 1.800m;
‐ Taxiway with direct access to the threshold (no backtrack);
‐ Select Modify Runway then choose ENTRY ANGLE of 76° (this configuration will reduce runway length in 76 meters);
‐ Line up following the yellow line

77
Q

Quando NAO fazer um rolling takeoff?

A
  1. When penalize the payload;
  2. Contaminated runway;
  3. Heavy rain;
  4. Low Visibility
  5. Technical conditions that may affect braking efficiency;
  6. SBSP and SBRJ Operations;
  7. Narrow Runways (less than 45m width).
78
Q

BAROMETRIC DIFFERENCE ON GROUND?

A

The maximum difference is:
±20 ft between both PFDs
And depending on the aircraft configuration:
±100 ft between ISIS  and PFDs, or
±300 ft between mechanical standby altimeter and PFDs.

79
Q

Maximum difference between Operational Flight Plan and Loadsheet (AZFW greater than EZFW)?

A

1300 KG

80
Q

LAST MINUTE CHANGE? 320/321

A

335 KG/ 390KG

81
Q

Fuel burn for each 500 kg per hour?

A

16 KG

Airbus 320 Prova (1 decks)

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