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Airbus 320 AZUL > AIRBUS QUESTIONS > Flashcards

AIRBUS QUESTIONS Flashcards

1
Q

MAX FLAP SPEEDS A 320

A

Flap 1 = 230kts

Flap 1+F = 215 kts

Flap 2 = 200 kts

Flap 3 = 185 kts

Flap FULL = 177 kts

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2
Q

A COMPLETE IRS ALIGNMENT MUST BE PERFORMED:

A
  • Before first flight o the day
  • Crew Change
  • When GPS coverage is N/A and NAVAIDS coverage is poor
  • When GPS is N/A and ETEnroute > 3 hours.
  • LAT between 2 North and 2 South
  • For Full alignment: OFF > 5 seconds, then NAV
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3
Q

PACK FLOW LO, NORM and HIGH; When?

A

A 320 LO :
- PAX < 141

A 321 LO
- PAX < 168

A320 / 321 HIGH:
- For Abnormal hot and humid conditions
(If APU supply and Single ENG = Pack set to HI automatic.)

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4
Q

BAT CHECK cockpit preparation

A

OFF then ON

10 sec after cycle: check the BAT is below 60 A and descreasing.

(when charging cycle completed the batteries ar disconnected to DC BAT BUS

[BAT 1]_____[DC BAT]_____[BAT 2] (When charging)

[BAT 1] [DC BAT] [BAT 2] (Charging finish)

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5
Q

FUEL MODE SEL explain possible spillage

A

When MODE SEL in MAN and;

CTR TK PUMP 1 and 2 ON;

= Possible FUEL SPILLAGE

        WHY?

Because in this configuration the CENTER TANK FUEL TRANSFER will NOT stop when wing tanks become FULL.

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6
Q

THIRD OCCUPANT AUDIO CONTROL PANEL

A

PA knob - RECEPT

(This allows cabin attendant annoucementes recorded on the CVR)

Proper setting - VOL at or above MEDIUM range.

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7
Q

ALTITUDE REPORT on TCAS PANEL

A

for RVSM operations select SYS 1 if AP 1 is used, ans SYS 2 if AP 2 is used.

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8
Q

HF TEST on ground

A

DO NOT transmit during REFUELING

ONLY perform check when no personnel in the immediate vicinity.

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9
Q

PARKING BRAKE

A

ACCU PRESS —- CHECK

Must be in GREEN BAND. If not use the electric pump on YELLOW to recharge.

     {{{WARNING}}}

YELLOW + GREEN system are pressurized from YELLOW hyd pump. OBTAIN GROUND CREW CLEARANCE before using.

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10
Q

ALTIMETER difference

A

+/- 20 ft between PFDs

+/- 60 ft between ISIS and PFD or
+/- 300 ft between MECH STDby ALT and PFD

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11
Q

After OXY MASK TEST

A

Check REGUL LO PR indication NOT DISPLAYED.

    Where?

ON DOOR/OXY SD PAGE.

    WHY?

This ensure LP valve is OPEN.
(Due to residual pressure btw the LP valve and OXY MASKs, an LP valve failed in CLOSED POSITION may not be detected during the oxygen mask test)

REGUL 1(2)(1+2) LO PR indication
It is in amber, if oxygen pressure on the low-pressure circuit is low (50 PSI)

To complete TEST , CHECK DOOR/OXY sd page

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12
Q

START LIMITATIONS

A
  • MAX EGT for start: 635 C.
  • 3 consecutives start cycles
    Each cycle is 3 starts attempts
    1 min cool down each
  • AFTER 3 start attempts: 15 MIN cool down
  • No EGD of startes when N2 above 10% (on ground)
  • OIL TEMP
    –> START = -40 C
    –> EXCEED IDLE = - 10 C
    –> TAKEOFF = 50 C

-X WIND START: 35 KT

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13
Q

ENGINE START 2 minutes run before takeoff, WHY?

A

TO ENSURE CENTER TANK PUMP TEST IS FINISHED, AS TAKEOFF ON CENTER TANK IS PROHIBITED.

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14
Q

ANTI ICE after start

A

OAT < 10 C, visible moisture and visibility less than 1 SM

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15
Q

MAX BRAKE TEMP for TO

A

300 Celcius or

150 Celcius if brake fans have been used.

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16
Q

TO CONFIG

A

Rudder or Pitch trim out of range

Flaps or Slats no in TO CONFIG

speed brake not retracted

Left or Right sidestick fault

Fuel pumps 1+2 LO PRESS

G or Y HYD engine pump LO PRESS

Door not Closed

Brakes Hot

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17
Q

Abaixo de qual valor a PACK FLOW deve ser utilizada em LOW?

A

141 ocupantes

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18
Q

Qual a limitação de velocidade abaixo do FL100?

A

350 kts

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19
Q

Qual o peso máximo de rampa

A

77.400 kg

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20
Q

Qual a voltagem mínima para assegurar uma carga superior a 50% e possibilitar a partida do
APU?

A

25.5 V

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21
Q

Em NORMAL LAW, qual o bank máximo?

A

67 Graus

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22
Q

Com o BRAKE FAN ON, a máxima temperatura dos freios permitida para decolagem?

A

150 Graus

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23
Q

Qual a velocidade máxima de recolhimento do trem de pouso?

A

220Kt/0.54M

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24
Q

Qual o número de assentos de passageiros?

A

174

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25
Q

Qual a altitude máxima para partida do APU?

A

39.800Ft

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26
Q

Qual a velocidade máxima de penetração em atmosfera turbulenta abaixo do FL200?

A

260 kt

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27
Q

Qual a quantidade máxima de combustível?

A

18.623 Kg

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28
Q

Qual é o Mínimo Take off fuel?

A

1500 kg

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29
Q

Qual o vento máximo de cauda para decolagem?

A

15 kt

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30
Q

Qual a velocidade máxima de penetração em atmosfera turbulenta acima do FL200?

A

280Kt/0.76M

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31
Q

Qual tanque de combustível responsável por suprir o APU?

A

Esquerdo

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32
Q

Qual o range de seleção de temperaturas do sistema de ar condicionado?

A

De 18 a 30 Graus

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33
Q

PACK FLOW SELECTOR nas posições LOW, NORM e HI, suprem uma demanda de ar nas
proporções de:

A

80%, 100% e 120%

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34
Q

Quais são os níveis que o FMS considera para alternativa?

A

FL100, FL220, FL310

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35
Q

Em ALTERNATE LAW, qual das seguintes proteções será perdida?

A

Bank Protection

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36
Q

A função AUTO PITCH TRIM estará disponível

A

Em NORMAL e ALTERNATE LAW até 33º de inclinação

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37
Q

Durante a decolagem, caso o FLAP não seja recolhido, o ARS (Automatic Retraction System)
recolhe o FLAP automaticamente quando a velocidade atingir:

A

210 kts

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38
Q

Após decolagem com PACKS OFF, em qual momento a primeira PACK deve ser ligada?

A

Após redução de potência

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39
Q

Após três tentativas de partida do APU, quanto tempo deve-se esperar para uma nova
tentativa?

A

60 minutos

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40
Q

Qual a altitude mínima para ligar o AP durante a decolagem?

A

100 ft OR 5 SEC AFTER LIFT OFF

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41
Q

Qual a altitude máxima para extensão dos FLAPS?

A

FL 200

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42
Q

Qual a temperatura máxima dos freios para decolagem com Brake Fan OFF?

A

300 Graus

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43
Q

Quais são os sistemas hidráulicos do A320?

A

Amarelo, Azul e Verde

Trabalham com 3000 psi aprox cada um. Tem a PTU que transfere energia do sistema green pro yellow e vice versa. O sistema Azul, quando em pump failure sera pressurizado apenas com a RAT.

O sistema Green e Yellow possuem uma EDP e uma electrical pump. O sistema azul tem a electric pump e a RAT.

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44
Q

Quais são os respectivos pesos máximos de taxi, decolagem e pouso do A320?

A

77.400 kg, 77000kg e 67400kg

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45
Q

Quais válvulas o DITCHING pb-sw fecha?

A

Outflow Valve, Emergency Ram Air Inlet, Avionics Ventilation Inlet, Extract Valves and Pack Flow
Control Valve.

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46
Q

Como o ROPS pode ser desabilitado?

A

Overhead Panel / EGPWS

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47
Q

A função GROUND SPEED MINI não está disponível quando?

A

Selected Speed no FCU

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48
Q

O TCAS quando utilizado na função ALL, poderá observar tráfegos entre quais altitudes?

A

+2700ft e – 2700ft

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49
Q

Logica do TCAS

A

Range100 NM
ABV 9900ft BLW 2000ft
BLW 9900ft ABV 2000ft

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50
Q

Quando um ENGINE START VALVE MANUAL OPERATION será feito?

A

No início da partida automática, válvula não abrir.

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51
Q

Após a primeira partida dos motores, qual tempo mínimo de warm -up?

A

3 minutos

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52
Q

Quais são os MEMORY ITEMS do A320?

A

Unreliable Airspeed

Loss of Braking
Emergency Descent
Stall Recovery
Stall on Lift-off

Windshear
EGPWS,
TCAS

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53
Q

Caso haja perda do sistema hidráulico azul, qual sistema importante fica inoperante?

A

Emergency Generator

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54
Q

Qual a quantidade mínima de óleo requerida no motor?

A

8.9 qt + 0.45qt/h > 10.6 qt.

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55
Q

Em caso de uma rejeição de decolagem, o auto-brake atua se a mesma se iniciar acima de

A

72 kts

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56
Q

Qual a velocidade máxima pode-se voar com o trem de pouso estendido?

A

280kt

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57
Q

A partir de qual diferença de pressão a PTU entra automaticamente em funcionamento?

A

500 psi

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58
Q

Qual a velocidade máxima para uso do limpador?

A

230 kt

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59
Q

O sistema de ENG ANTI-ICE deve ser utilizado quando?

A

visible moisture
visibility less than 1 ST mile
temperature equal or less than 10 C

or antecipated ice conditions.

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60
Q

O sistema de ar condicionado fornece PACK HI FLOW independentemente da posição da PACK
FLOW SELECTOR sempre que?

A

APU ligado ou single PACK.

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61
Q

Qual o raio de curva do A320 em movimentações no solo e sua respectiva superfície limitante?

A

22.9 metros e ponta da asa oposta.

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62
Q

A luz verde do DECEL no auto-brake indica que

A

A aeronave atingiu 80% da capacidade de frenagem selecionada

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63
Q

A indicação do rádio altímetro no PFD se torna ativo abaixo de:

A

2.500ft.

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64
Q

A Speed Trend Tape no PFD indica a velocidade eu a aeronave atinge em um espaço de tempo
de:

A

10 segundos.

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65
Q

O Pitch inicial na decolagem para condição bimotor e mono motor são respectivamente:

A

15 graus e 12,5 graus

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66
Q

Na condição NAV ACCURANCE LOW, qual funcionalidade não deve ser usada:

A

TERR no ND

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67
Q

Com o modo lateral HDG sendo utilizado, ao sobrevoar o Pseudo Waypoint DECEL, a aeronave
irá:

A

Continua com a Present Speed até que o PF ative a função APPROACH PHASE no FMS

68
Q

Em uma aproximação, a página ECAM WHEEL SD aparece quando as seguintes condições forem
satisfeitas

A

Abaixo de 15500ft, Gear Down

69
Q

Com o AP desligado e TCAS Flight Guidence Mode inoperante, em caso de Resolution Advisory,
o piloto devera:

A

Seguir imediatamente o FD pitch bar

70
Q

Quais são as velocidades máximas de taxi?

A

30kt seca, 15 molhada
10kt pátio seco, 5kt molhado

71
Q

Qual a velocidade máxima em interseções rápidas?

A

60kt pista seca, 15kt pista molhada

72
Q

O Predictve Windshear Warning fica inibido na decolagem quando:

A

A aeronave estiver entre 100kt e 50ft de altitude.

73
Q

Quais são as funções do FAC?

A

Yaw Damping, Turn Coordination, Rudder Trim, Rudder Travel Limit, PFD Speeds Scale,
Minimum and Maximum Speeds, Alpha Floor, Windshear, Low Energy Warning

74
Q

Quantas fases de inibição o A320 possui

A

10

75
Q

Quais sistemas utilizam fonte pneumática?

A

Ar Condicionado, Partida dos Motores, Sistema Anti-Ice, Pressurização do Sistema Hidráulico e
Lavatórios

76
Q

Qual a desaceleração do Auto-Brake em LOW e MED respectivamente?

A

1,7m/s2 e 3m/s2

77
Q

É possível obter ar condicionado para os passageiros durante a partida do segundo motor?

A

Sim, posicionando a válvula XBLEED na posição SHUT e 60 segundos após a partida do primeiro
motor.

78
Q

Qual computador é responsável pela atuação do profundor esquerdo?

A

SEC 3

79
Q

Quando as formações estiverem abaixo de qual altitude em relação a aeronave o radar não
mostrará?

A

6.000ft.

80
Q

Qual é o range do Radar?

A

320NM

81
Q

O trem de pouso não estenderá caso comandado acima de

A

260kt

82
Q

A indicação de Side-Slip se tornará azul quando:

A

N1 for superior a 80%, diferença de potência superior a 35% e CONF em 1, 2 e 3.

83
Q

Quando os freios aerodinâmicos (spoilers) recolherão automaticamente?

A

Falha no SEC 1 e 3, falha no profundor esquerdo ou direito, ativação de proteção do ângulo de
ataque, dispositivo hiper sustentador completamente estendido, manete de potência acima da
posição MCT, ativação do APLHA FLOOR.

84
Q

Quando uma partida automática deve ser cortada imediatamente?

A

Perda das DU’s e ECAM

85
Q

Caso o pouso seja realizado com Ground Spoilers desarmados, é correto afirmar que:

A

Estenderão com uma manete na posição REV e outra abaixo de MCT e trens principais no solo.

86
Q

Após os INNER TKS totalmente abastecidos, com quantos quilos os CENTER TKS voltam a
reabastecê-los?

A

500kg.

87
Q

A aeronave foi reabastecida com 6500kg de combustível. O TRIP FUEL previsto para etapa era
3000kg. Logo após a decolagem, a tripulação percebe que a indicação de FOB está em 5200kg,
juntamente com uma indicação âmbar no EFOB no destino, cujo o valor está em 2300kg. A
tripulação diante deste cenário deverá:

A

Aguardar 6 minutos e verificar se a indicação de combustível e EFOB no destino voltaram aos
valores previstos.

88
Q

Em caso de falha na bomba do sistema yellow

A

Há uma bomba manual que pode ser usada para pressurizar o sistema

89
Q

Qual das falhas não ilumina o Autoland Light

A

Desvio de Glide Slope superior a ½ DOT acima de 100ft.

90
Q

Com relação a porta blindada do Cockpit, é incorreto afirmar que:

A

Durante a descompressão do cockpit a porta se abre automaticamente.

91
Q

Quando não fazer Rolling Takeoff?

A

Pista contaminada / Chuva forte / LVTO / Braking efficiency affected / Back Track / Quando
compromete o payload / Pista menor que 1800 m.

92
Q

Quando não usar FLEX?

A

Pista contaminada (SBSP pista molhada).
Obs. Em caso de esquecimento da inserção da Flex Temp. a decolagem dever ser efetuada em
TOGA.

93
Q

Qual o limite para uso do EXP CLB?

A

FL250

94
Q

Onde encontra-se o Configuration Summary?

A

QRH

95
Q

Quais documentos são necessários para operação doméstica e de Bandeira após o pouso?

A

Load/Trim Sheet, Navegação e Cópia do Plano de Voo

96
Q

Fórmula de cálculo da GREEN DOT

A

GW x 2 + 85 / Acima do FL250 usar 1000ft para cada 1kt

97
Q

Qual a Speed do SRS no FMA:

A

V2 + 10 dual engine, V2 single engine

98
Q

FMA Modes na fase de aproximação:

A

Land 400ft / Flare 50ft / Retard 20ft

99
Q

Alertas Row/Rop abaixo de 200ft:

A

AMBER – WET RWY GO AROUND / DRY RWY prossegue.
RED – GO AROUND.

100
Q

LMC limitado por 0.5% do MLW (335kg)

A

Diferença máxima entre Load e FLP 1300 (acima de 1300kg pede novo FPL)

101
Q

Prioridade Ar Condicionado

A

APU/ENG/LPU

102
Q

Prioridade Eletrica:

A

ELEC: GPU/APU/GEN

103
Q

O que limita a V1?

A

VR e VMCG

104
Q

Relação do CG com o gasto de combustível:

A

CG traseiro econômico

105
Q

Quais a ações a serem guardadas pelo PM

A

‐ ENG MASTER lever
‐ IR MODE selector
‐ All guarded controls
‐ Cockpit C/Bs.
-trust levers

106
Q

Quando se pode voar sem o A/THR?

A

Aproximação VMC

107
Q

Para que serve o Horn Cutout no painel de evacuação?

A

Sileciar a buzzer na cabine (quando ativado no painel de comissários)

108
Q

Qual a logica do sistema de combustível?

A

Só tem bomba Inner.
Sequência: Consome direto do Inner, Center (Inner baixou 500kg), Outer (Inner abaixo de 750kg
ou na descida)

109
Q

Qual a diferença entre CRZ e ALT CRZ?

A

CRZ a altitude do FCU é mantida e difere do FMGS. ALT CRZ FCU = FMGS + SOFT ALT (+/- 50’)

110
Q

Qual é a definição de VMCG?

A

Velocidade mínima de controle em solo, 113 kt

111
Q

Quais são as ECAM Caution Messages que requerem rejeição acima de 100kt?

A

F/CTL SIDESTICK FAULT
ENG FAIL
ENG REVERSER FAULT
ENGINE REVERSE UNLOCK
ENG 1(2) THR LEVER FAULT

112
Q

Quando se inicia uma arremetida, o que acontece se o PF não levar a Thrust Lever para
TOGA?

A

O modo SRS GA e o modo go-around no FMS não engajam. O AP/FD permanecem engajados no
APPROACH ou LANDING e o FMS permanece em APPR PHASE.

113
Q

WEIGHTS:

A

VW53 =
MTW 77400
MTW 77000
MLW 67400
MZFW 64300
MW 40600

114
Q

Airport Operation:

A

RWY Slop: + - 2%
Max RWY: Alt 9200ft
Nominal RWY Width: 45m
Narrow RWY Width: 30m

115
Q

Winds

A

Max tailwind for takeoff: 15kt
Max tailwind for landing: 10kt
Max tailwind Autoland: 5kt

116
Q

Doors limitation:

A

Pax door: 65kt para operação
Cargo door: haed wind 50 kt, cross wind 40kt

117
Q

Flaps/Slats Speeds:

A

1 230kt
1+F 210kt
2 200kt
3 180kt
Full 177kt

118
Q

Thrust/EGT

A

TOGA dual engine 5 min / 1016c
TOGA single engine 10 min / 1060
MCT EGT 1025C
Start on ground 750C
Start in Flight 875C

119
Q

Gear Down Speeds

A

VLE 280kt / M 0.67
VLO EXT 250kt
RET 220kt
Tire speed 195kt
Max Wipers Speed 230kt
Cockpit window open 200kt
VMO 350kt / MMO .82

120
Q

Cabin Pressure

A

Max Positive 9PSI
Max Negative 1PSI
Safety Valve 8.6 PSI

121
Q

Max Operating Altitude

A

Slats and Flaps Retracted 39800ft
Slats and Flaps Extended 20000ft (due to cabin press)

122
Q

Limitation AP:

A

Takeoff 100ft
App ILS 160ft
App Loc 200ft
App Non-Precision 250ft
App Circling 500ft
All others 500ft

123
Q

Wing ANTI ICE on ground ?

A

self test for 30 seconds.

124
Q

The following systems may be affected in very cold weather:

A

‐ The EFIS/ECAM (when the cockpit temperature is very low)
‐ The IRS alignment (may take longer than usual, up to 15 min).
The probe and window heating may be used on ground.

125
Q

BRAKES temp after landing: quando a manuntencao deve ser comunicada?

A

• The temperature difference between two brakes of a gear is more than 150 °C, and the
temperature of one of these brakes is above or equal to 600 °C, or
• The temperature difference between two brakes of a gear is more than 150 °C, and the
temperature of one of these brakes is below or equal to 60 °C, or
• The difference between the average temperature of the left gear brakes and right brakes is
above or equal to 200 °C, or
• The temperature of one brake exceeds 900 °C (800 C if A 321)

126
Q

CRUISE check o que checar no Hidraulico?

A

A slight decrease in quantity is normal.
Fluid contraction during cold soak can be expected.
Green system is lower than on ground, following landing gear retraction

127
Q

CRUISE check, a cada 30 min ou passando um waypoint?

A

Check FUEL:
‐ Check FOB (ECAM) and fuel prediction (FMGC), and compare with the computerized flight or
use the performance application of the EFB
‐ Check that there is no fuel leak
‐ Check that the sum of the fuel on board and the fuel used is consistent with the fuel on board
at departure:
• If the value is abnormally negative, suspect a fuel leak
• If the value is abnormally positive, suspect a fuel quantity overread.

APOS A DECOLAGEM, 6 MINUTOS, OS VALORES DE COMBUSTIVEL ESTAO CONFIAVEIS.

128
Q

Securing the aircraft , quando?

A

quando a aeronave vai ficar mais de 1:30 de solo.

129
Q

securing the aircraft conditions about ADIRS, and BATTERIES

A

After the shutdown off the ADIRS, wait at least 10 s before turning off the electrical supply, in order
to ensure that the ADIRS memorize the latest data.

Wait until the APU flap is fully closed (about 2 min after the APU AVAIL light goes out) before
switching off the batteries. Switching the batteries off before the APU flap is closed may cause
smoke in the cabin during the next flight.
If the batteries are off while the APU is running, APU fire extinguishing is not available.

130
Q

MASKS check

A

 On the mask stowage box:
‐ Press and hold the reset/test pb in the direction of the arrow.
• Check that the blinker turns yellow for a short time, and then goes black.
‐ Hold the reset/test pb down, and press the emergency pressure selector.
• Check that the blinker turns yellow and remains yellow, as long as the emergency
pressure selector is pressed.
• Listen for oxygen flow through the loudspeakers. Warn any engineer, whose headset
may be connected to the nose intercom, that a loud noise may be heard when performing
this check.
‐ Check that the reset/test pb returns to the up position and the N 100 % selector is in the
100 % position.
‐ Press the emergency pressure selector again, and check that the blinker does not turn
yellow. This ensures that the mask is not supplied.
 On the ECAM DOOR/OXY SD page:
REGUL LO PR message…………………………………………………………. CHECK OFF PF-PM
Note: The crew must perform this check after having checked all masks. It ensures that the
LP valve is open, (due to residual pressure between the LP valve and the oxygen
masks, an LP valve failed in the closed position may not be detected during the
oxygen mask test).

131
Q

qual a diferenca maxima aceita no UPLIFT?

A

FOB after refueling Abnormal difference above
Up to 6 t (13 200 lb) 400 kg (900 lb)
Between 6 t (13 200 lb) and 12 t (26 500 lb) 500 kg (1 100 lb)
More than 12 t (26 500 lb) 600 kg (1 300 lb)

132
Q

If, during the engine start, the ground crew reports a fuel leak from the engine drain mast, what to do?

A

run the engine at idle for 5 min. If the leak disappears during these 5 min, the aircraft can be dispatched without maintenance action. If the leak is still present after 5 min, shut down the engine and request the maintenance personnel to investigate the leakage source.

133
Q

‐ During ground operation, when in icing conditions and the OAT is +3 °C or less, or if significant
engine vibration occurs, the following procedure should be applied for ice shedding:

A
  1. The flight crew must consider the taxi-in time from the previous flight and the
    taxi-out time of the current flight to determine the total taxi time.
  2. If a maintenance task to de-ice the engines was performed before engine start, the
    taxi-in time of the previous flight must be disregarded.
  3. For taxi-in time, Refer to PRO-NOR-SOP-23 Parking - Logbook
134
Q

fire protection and fire extinguisher:

A

‐ Fire and overheat detection for the engines and APU
‐ Smoke detection for the cargo compartments, the lavatories, and the avionics bay
‐ Fire extinguishing for the cargo compartments, the engines, the APU, and the lavatories.

135
Q

Windshear detection

A

The windshear detection function is provided by the Flight Augmentation Computer (FAC) in takeoff
and approach phase in the following conditions:

‐ At takeoff, 3 s after liftoff, up to 1 300 ft RA
‐ At landing, from 1 300 ft RA to 50 ft RA
‐ With at least CONF 1 selected

During the takeoff roll, up to 100 kt, both warnings and cautions are available within a range of 3 NM.
At takeoff, alerts are inhibited above 100 kt and up to 50 ft.

During landing, alerts are inhibited below 50 ft

136
Q

COCKPIT WINDOW OPEN MAXIMUM SPEED

A

200 kts

137
Q

MAXIMUM TIRE SPEED

A

195 kts

138
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL)

A

116 kts

139
Q

WIPERS MAXIMUM OPERATING SPEED

A

230 kts

140
Q

MINIMUM CONTROL SPEEDS ON NARROW RUNWAYS

A

Runway Width 30 m 35 m 40 m
▵ VMCG(kt) + 2.5 + 1.5 + 0

141
Q

WEIGHT LIMITATIONS A321

A

Maximum taxi weight…………………………………………………………………………….. 93 900 kg (207 014 lb)
Maximum takeoff weight (brake release)………………………………………………….. 93 500 kg (206 132 lb)
Maximum landing weight……………………………………………………………………….. 79 200 kg (174 606 lb)
Maximum zero fuel weight………………………………………………………………………75 600 kg (166 669 lb)
Minimum weight……………………………………………………………………………………. 46 600 kg(102 736 lb

142
Q

APU BLEED USE WITH HP AIR START UNIT

A

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the
same time, to prevent any adverse effect on the Bleed Air System.

143
Q

AUTO PILOT LIMITATIONS

A

At takeoff 100 ft AGL and at least 5 s after liftoff

In approach with FINAL APP, V/S or FPA mode 250 ft AGL

ILS/MLS  approach when CAT1 is displayed on the FMA 160 ft AGL

After a manual go-around 100 ft AGL

In circling approach 500 ft AGL for aircraft category C (600 ft AGL for
aircraft category D).

In all other phases 500 ft AGL

144
Q

MAXIMUM WIND CONDITIONS FOR ILS/MLS  CAT II OR CAT III AND FOR GLS  CAT I

A

Headwind : 30 kt
Tailwind : 10 kt
Crosswind : 20 kt (15 kt for automatic rollout with OEI)

WIND LIMITATION: eh o vento oficial pago pela torre, nao no ND

If the tower reports a surface wind that exceeds the limitations, only CAT I automatic approach without autoland can be performed.

145
Q

MAXIMUM WIND CONDITIONS FOR ILS/MLS  CAT II OR CAT III AND FOR GLS  CAT I
(A 321)

A

Headwind : 15 kt
Tailwind : 10 kt
Crosswind : 10 kt

146
Q

AUTOMATIC LANDING O CONTAMINATED RWY?

A

4 Automatic rollout performance is approved on dry and wet runways, but performance on contaminated runways was not demonstrated.

During automatic rollout with one engine inoperative or one thrust reverser inoperative, the flight crew can use the remaining thrust reverser, provided that:

‐ No more than idle thrust is used
‐ Headwind component not above 30 kt
‐ Tailwind component not above 10 kt
‐ Crosswind component not above 15 kt.

147
Q

APU START LIMITATIONS

A

3 TIMES

60 MIN COOL DOWN.

148
Q

APU BLEED LIMITATIONS

A

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

149
Q

DEFINITION OF SEVERE ICE ACCRETION

A

ice accretion is considered severe when the ice accumulation on the airframe reaches approximately
5 mm (0.2 in) thick or more

150
Q

FLEX TAKEOFF ON CONTAMINATED RWY?

A

NOT ALLOWED

151
Q

If an engine failure occurs after liftoff, the SRS targets which speed ?

A

at which the failure occurred (limited between V2 and V2 +15 kt)

152
Q

GPWS MEMO ITEMS

A

GPWS
“PULL UP TOGA”
AP OFF
manetes em TOGA
Speed brake retracted
Nivela as asas

153
Q

WINDSHEAR MEMO ITEMS

A

“WINDSHEAR TOGA”
Manetes em TOGA
Follow SRS
Maintain configuração

154
Q

TCAS MEMO ITEMS

A

“TCAS blue” ou “TCAS, I have control”
AP off
FD off
Follow the green band

155
Q

EMERGENCY DESCENT MEMO ITEMS

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 brake FULL
PM – Check e declara emergência e 7700
PF – “ATENÇÃO descida rápida, permaneçam sentados, remain seated”

156
Q

LOSS OF BRAKINGS MEMO ITEMS

A

“LOSS OF BRAKING”
Máximo reverso
Brake PEDALS release
Anti skid off ORDER
Brake pedals apply MAX BRAKING 1000 PSI
Últimos casos Parking Break

157
Q

STALL RECOVERY MEMO ITEMS

A

“STALL, I have control”
Nose down pitch
Asas niveladas
Aplica potência aos poucos
Abaixo de 20.000ft – Flap 1!

158
Q

STALL LIFT OFF MEMO ITEMS

A

STALL AT LIFT-OFF
“STALL TOGA 15˚”
TOGA, pitch 15˚ e asas niveladas

159
Q

UNRELIABLE AIRSPEED MEMO ITEMS

A

“UNREALIBLE SPEED”
AP, A/THR e FP OFF
15˚ TOGA Below THR REDUCTION
10˚ CLB ABOVE THR REDUCTION BLW FL100
5˚ CLB ABOVE FL 100
Maintain CONF
Se CONF FULL – CONF 3
Speed break retracted
Gear UP

160
Q

PILOT INCAPACITATION

A

Pilot incapacitation

I have controls 
40s para desativar o outro sidestick
161
Q

LOC only COMO FAZER?

A

Vapp no FDP
Seleciona o LOC ao invés de APPR
Não seleciona segundo AP
1 NM antes do FDP seleciona -3.0 TRK/FPA
0.3NM pull

162
Q

Comprimento A320

A

37.57 M

163
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

164
Q

LOSS OF BRAKING MEMO ITEMS

A

“LOSS OF BRAKING”
Máximo reverso
Break release
Anti skid off
Break pedals
Últimos casos Parking Brake

165
Q

Envergadura do A320 e A321

A

35.80 metros

Airbus 320 AZUL (3 decks)

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