Flight Instruction And Check

Question 1

Diferenças de Altímetro

Answer 1

The maximum difference is: ±20 ft between both PFDs And depending on the aircraft configuration: ±60 ft between ISIS and PFDs, or ±300 ft between mechanical standby altimeter and PFDs.

FCOM PRO-NOR-SOP-06 P 20/26

Question 2

Contingências ETOPS

Answer 2

The procedures given in the EASA approved Airbus ETOPS CMP document are applicable. The SOP (refer to chapters PRO, NOR, SOP) and the ABNORMAL and EMERGENCY procedures (refer to chapters PRO, ABN) apply. For ETOPS flights, the following additional procedure apply: GEN 1 or 2 FAULT When in ETOPS segment : APU GEN (if available)……………………………………………………………………………………………….USE

PRO-SPO-40A-50 P 1/2

Question 3

Contingências ICAO

Answer 3

ICAO Doc 4444, In-flight Contingency Proce-dures. Chapter 15 of ICAO Doc 4444 (Proce-dures for Air Navigation Services — Air Traf-fic Management (PANS-ATM)) contains impor-tant guidance for pilot training programs. Chap-ter 15 includes Special Procedures for In-flight Contingencies in Oceanic Airspace, as well as Weather Deviation Procedures. Chapter 15 cov-ers in-flight diversion and turn-back scenarios, loss of navigation capability, and procedures to follow for weather avoidance. This critical guid-ance is reprinted in the Oceanic Operations sec-tion of the U.S. Aeronautical Information Pub-lication (AIP), the International section of the Notices to Airmen Publication, and FAA Advi-sory Circular 91-70, Oceanic and Remote Con-tinental Airspace Operations.

Question 4

Aerovia Y USA Y ROUTES: localizado na parte ENRT do manual Jeppesen: São rotas que requerem equipamento GNSS e capacidade de navegação RNAV 2. Para empresas aéreas de fora dos Estados Unidos é requerido uma autorização prévia para voar este tipo de rota. Não é permitido realizar SLOP neste tipo de rota. Devemos ter capacidade RAIM continua na rota, sendo autorizado somente 5 minutos de perda do PRAIM.

Answer 4

The Y-routes are designated RNAV 2 with GNSS required. Aircraft flying the Y-routes must be equipped with GNSS and able to meet RNAV 2 performance requirements. RNAV systems relying solely on DME/DME or inertial navigation are not suitable (and therefore not authorized) for use on any Y-route.
Jeppesen ENROUTE DATA - NORTH AMERICA p 432

Question 5

Engine Fail in cruise flight

Answer 5

When an engine failure occurs during cruise, three possible strategies apply: ‐ The standard strategy ‐ The obstacle strategy ‐ The fixed speed strategy.
FCTM PR-AEP-ENG P 12/24

Question 6

Decolagem para aeródromo com previsão de estar fechado na hora prevista de chegada, pode? Pode sim, desde que seja indicado dois aeródromos de alternativa e que sejam adicionadas algumas margens de teto e visibilidade para estes aeródromos. As condições devem se manter até 1 hora após a decolagem.

Answer 6

Previsão de destino fechado (Despacho ou Liberação de voo sobre grandes extensões de água)

MGOA-274

Na eventualidade do aeroporto de destino estar com previsão meteorológica abaixo dos mínimos requeridos para a operação pretendida, a Azul faz o despacho considerando dois aeródromos de alternativa. A previsão meteorológica deve indicar que a condição se mantém entre o momento estimado para o pouso e até uma hora após
MGOA 271

Question 7

Emergency Descent

Answer 7

CREW OXY MASKS - USE
SIGNS - ON
EMER DESCENT - INITIATE If A/THR not active: THR LEVERS - IDLE SPD BRK - FULL When descent established: SPEED - MAX/APPROPRIATE If structural damage suspected : MANEUVER WITH CARE
FCOM PRO-ABN-MISC P 1/50

Question 8

Funcionamento da porta da cabine (como fazer o check pré-voo)

Answer 8

COCKPIT DOOR If required by local Airworthiness Authorities: ANN LT selector…………………………………………………………………………………………………………TEST Check that the OPEN and FAULT light (on the pedestal), and the three LED light (on the overhead panel) come on. ANN LT selector…………………………………………………………………………………………………………..BRT Check that all lights go off. CKPT DOOR………………………………………………………………………CHECK CORRECT OPERATION Set the toggle switch to the UNLOCK position. Check that the door opens, and that the OPEN light comes on. Then, with the door fully opened, release the toggle switch (check that it returns to the NORM position). Close the door. Check that it is locked, and that the OPEN indicator goes off. CKPT DOOR MECHANICAL OVERRIDE…………………………………………………………………..CHECK Check that the door opens normally, and that it closes when the mechanical override is used.

FCOM PRO-NOR-SOP-06 P 8/26

Question 9

Falha de Comunicação

Answer 9

COMMUNICATIONS FAILURE 6.1 GENERAL RULES 6.1.1 An aircraft operated as a controlled flight shall maintain continuous air-ground voice commu-nication watch on the appropriate communication channel of, and establish two-way communication as necessary with, the appropriate air traffic control unit, except as may be prescribed by the appropriate ATS authority in respect of aircraft forming part of aerodrome traffic at a controlled aerodrome. (Annex 2, 3.6.5.1) NOTE 1: SELCAL or similar automatic signalling devices satisfy the requirement to maintain a listen-ing watch. NOTE 2: The requirement for an aircraft to maintain an air-ground voice communication watch remains in affect after CPDLC has been established.

Jeppesen Emergency chapter 6

Question 10

Quando usar Anti-Ice,: Quando o acumulo de gelo estiver acima de 5mm de espessura ou mais. vamos usar ENG ANTI ICE com temperatura menor ou igual 10. Em voo com temperatura menor ou igual 10C de TAT e com visibilidade menor 1SM ou 1600m, vamos ligar o ENG ANTI ICE. Se a temperatura estiver menor que -40C de SAT não precisamos ligar na Subida e em Cruzeiro, contudo na descida é preciso ligar pois o motor vai estar em IDLE por muito tempo.

Answer 10

Deicing/anti-icing fluids must be able to remove ice and to prevent its accumulation on aircraft surfaces until the beginning of the takeoff. In addition, the fluids must flow off the surfaces of the aircraft during takeoff, in order not to degrade takeoff performance. Several types of fluids can be used. These fluids have different characteristics:

PR-NP-SP-10-10-1 P 2/8

Question 11

Sequência de abastecimento automático
Inner Tank até 4500 de cada lado, total de 9.000kg, Outter Tank são enchidos, Inner Tank ate 15.385kg de cada lado, Trim tank ate 2400, Inner Tank é completado até encher e por fim o Trim Tank e o Center Tank são enchidos

Answer 11

The center tank pumps run continuously, whenever there is fuel in the center tank. Each inner tank inlet valve controls the transfer by cycling its inner tank contents between full and approximately 2 000 kg (4 415 lb) below full. When the center tank is empty, both center tank pumps temporarily stop, and both inner tank inlet valves close.

The outer tank fuel is transferred to the inner tanks by gravity. Each outer tank transfer valve controls the transfer by cycling the associated inner tanks contents between 3 500 kg (7 720 lb) and 4 000 kg (8 830 lb). When each outer tank has been empty for 5 min, its outer tank transfer valves close.

Question 12

Fluxo de Dump Fuel

1000kg ou 2200lb/min desconsiderando a queima de combustível

Answer 12

The Jettison system: ‐ Makes it possible to jettison fuel in flight. ‐ Output rate is approximate 1 000 kg (2 200 lb) per minute, excluding fuel burn. ‐ Is manually activated by two JETTISON pushbuttons, located on the overhead panel. Both pushbuttons must be pressed to select the jettison.
FCOM DSC-28-10-120 P 1/4

Question 13

Rotas, MDT, MTT etc

Answer 13

MTT = Minimum Time Track

MFT = Minimum Fuel Track MCT = Minimum Cost Track MDT = Minimum Distance Track
R= com restrição E = ETOPS

Question 14

O que informar nas mensagens de emergência?

Mayday Mayday Mayday Perigo
Pan Pan, Pan Pan, Pan Pan Urgencia
Pessoas a bordo, combustível em kg e se tem ou não cargas perigosas a bordo.

Answer 14

DOC 4444 ATC Jepp
The radiotelephony distress signal (MAYDAY) or urgency signal (PAN PAN) preferably spoken three times shall be used as appropriate. Subsequent ATC action with respect to that aircraft shall be based on the intentions of the pilot and the overall air traffic situation.

Question 15

Mensagem de Emergencia deve conter:

A: MAYDAY MAYDAY MAYDAY OU PAN PAN PAN B: Nome da estação
C: Call Sign
D: Tipo de Aeronave
E: Natureza da emergência
F: Intenções
G: Posição, Nivel Altitude e Proa.
Para cencelar? Cancel Mayday

RADIOTELEPHONY DISTRESS COMMUNICATIONS

Answer 15

5.2.1 Action by the Aircraft in Distress 5.2.1.1 In addition to being preceded by the radiotelephony distress signal MAYDAY, preferably spoken three times, the distress message to be sent by an aircraft in distress shall: a. be on the air-ground frequency in use at the time; b. consist of as many as possible of the following elements spoken distinctly and, if possible, in the following order: 1. name of the station addressed (time and circumstances permitting); 2. the identification of the aircraft; 3. the nature of the distress condition; 4. intention of the person in command; 5. present position, level (i.e., flight level, alti-tude, etc., as appropriate) and heading. (Annex 10, Vol II, 5.3.2.1.1)

Question 16

Manobras e Fraseologia TCAS.

Answer 16

Azul 4288 TCAS RA

MGO capítulo 18, fraseologia: Azul 4288 TCAS RA, AZUL 4288 clear of conflict returning to FL….

Question 17

Passageiro deportado (MGO capitulo 8 security): comandante deve ser avisado da presença de um deportado e sua localização na aeronave, também deve ser informado se o passageiro esta sendo acompanhado por escoltas. Comandante pode negar o transporte, contudo a empresa vai ter que fornecer por escrito ao estado deportador o motivo dessa negação. O passageiro deportado deve embarcar antes dos demais passageiros e desembarcar por ultimo. O deportado e as escoltas devem sentar nos últimos assentos ao fundo da cabine de clientes, sendo que o deportado deve sentar na janela e as escoltas no corredor. Não devem ser servidos bebidas alcoólicas nem talheres de metal.

Answer 17

MGOA 8.10. Clientes Sob Custódia

[Ref.: FLT 3.9.3(vii)]

O transporte aéreo de Clientes sob condições judiciais e sob escolta deve ser coordenado, com antecedência, entre o órgão policial responsável, a administração aeroportuária e a Empresa, de modo a: a. Estabelecer medidas especiais de segurança; b. Embarcar e desembarcar os Clientes discretamente e dentro das necessidades policiais; e c. Estabelecer a conduta a bordo da aeronave.

A periculosidade da pessoa sob custódia deve ser considerada pela autoridade policial para transportá-los em voos de Clientes, uma vez que a Empresa poderá negar seu embarque, pela potencial ameaça que representem à segurança do voo e a dos demais Clientes

Question 18

Cliente Sob Custódia:

Answer 18

As pessoas sob custódia, devem: a. Ser embarcadas antes dos demais Clientes e desembarcadas depois de todos os outros terem deixado a aeronave; b. Estar sempre acompanhadas e mantidas sob vigilância, inclusive no uso dos sanitários. c. Ocupar os assentos finais da cabine de passageiros, fora das saídas de emergência, em fileiras com dois ou mais assentos e, no mínimo, com um policial de escolta sentado entre ela e o corredor de passagem.

Question 19

ERA = Equipment Restrain Area, área restrita onde a aeronave vai parar no gate, o tamanho é definido pela maior aeronave que para naquela posição.
ASL = linhas que definem até onde os equipamentos de solo podem estar. Estas informações podem ser encontradas nos anexos da ICAO, mais especificamente no anexo 14, aeródromos.

Answer 19

Apron Safety Lines

5.2.1.6 Apron safety lines shall be of a conspicuous colour which shall contrast with that used for aircraft stand markings.
ERA =
Annex 14

Question 20

Abastecimento Manual: Podemos encontrar o procedimento no FCOM, Normal Procedures, Suplementos, Fuel e Abastecimento Manual.

Answer 20

MANUAL REFUELING DETERMINE FUEL QUANTITY IN EACH TANK Respect distribution in accordance with applicable REFUEL DISTRIBUTION graph . Note: To refuel the trim tank, one of these conditions must be fulfilled. ‐ the two inner tank inlet valves are open. ‐ both inner tank quantities are each greater than 14 000 kg. ‐ one inner tank quantity is greater than 14 000 kg and the other inner tank inlet valve is open. REFUEL VALVES sel…………………………………………………………………………………………………SHUT

REFUEL VALVES sel (tank(s) to be filled)……………………………………………………………………OPEN Note: Because the Fuel Control and Monitoring System (FCMS) does not have control of all the tanks, the END light will flash. MODE SELECT sw………………………………………………………………………………………………..REFUEL FUEL QTY…………………………………………………………………………………………………………..MONITOR  When the tank contents reach the required level : Corresponding REFUEL VALVES sel……………………………………………………………………..SHUT MODE SELECT sw………………………………………………………………………….OFF and GUARDED REFUEL VALVES sel…………………………………………………………………..NORM and GUARDED
FCOM PRO-NOR-SUP-FUEL P 5/10

Question 21

COCKPIT DOOR
If required by local Airworthiness Authorities:
ANN LT selector………………………………………………………………………………………………………… TEST Check that the OPEN and FAULT light (on the pedestal), and the three LED light (on the overhead panel) come on.
ANN LT selector………………………………………………………………………………………………………….. BRT Check that all lights go off.
CKPT DOOR………………………………………………………………………CHECK CORRECT OPERATION Set the toggle switch to the UNLOCK position. Check that the door opens, and that the OPEN light comes on.
Then, with the door fully opened, release the toggle switch (check that it returns to the NORM position).

Answer 21

Close the door. Check that it is locked, and that the OPEN indicator goes off.
CKPT DOOR MECHANICAL OVERRIDE………………………………………………………………….. CHECK
Check that the door opens normally, and that it closes when the mechanical override is used.

Question 22

PANS OPS holding speeds

Answer 22

Level / normal conditions / turbulence
Up to 4250 m (14000 ft) inclusive/425 km/h (230 kt)/520 km/h (280 kt)
Above 4250 m (14000 ft) to 6100 m (20000 ft) inclusive 445 km/h (240 kt)
Above 6100 m (20000 ft ) to 10350 m (34000 ft) inclusive 490 km/h (265 kt)
520 km/h (280 kt) or 0.8 Mach, whichever is less
Above 10350 m (34000 ft) 0.83 Mach 0.83 Mach
Table IV-1-1 (or I-6-1-1 in PANS-OPS). Holding speeds - Categories A through E

Question 23

Altitudes and hold speeds - at 6,000ft

Answer 23

up to 1850 m inclusive 6000 ft - 390 km/h (210 kt) / 520 km/h (280 kt) or 0.8 Mach whichever is less

Question 24

No Crew Desk explicar o Reclearance no plano de voo

Answer 24

O Planejamento de um voo com redespacho deverá ser efetuado mediante a seleção prévia dos seguintes fatores: a. Ponto de Reclearance - ponto de referência no rota para efeito do “redespacho” (ponto de “cheque de combustível”) b. Aeroporto Intermediário - para o qual a aeronave deverá prosseguir a partir do Ponto de Reclearance, caso o combustível não atenda o mínimo regulamentar para prosseguir para o destino; c. Alternativa - mais próxima do destino (não pode ser “Close-in”)
MGOA-283

Question 25

Qual a temperatura de WarmUp do motor CEO

Answer 25

After start, to avoid thermal shock, the engine should be operated at idle, or near idle for at least: ‐ 5 min when engines are cold, or ‐ 3 min when engines are warm after a stop of 1.5 h or less prior to advancing the thrust lever to high power. Taxi time at idle may be included in the warm-up period.

PRO-NOR-SOP-09 P 1/6

Question 26

Diferença máxima entre os altímetros.

Answer 26

Check the barometric reference and altitude indications on the PFDs and on the standby altimeter. The maximum difference is: ±20 ft between both PFDs And depending on the aircraft configuration: ±60 ft between ISIS and PFDs, or ±300 ft between mechanical standby altimeter and PFDs.
PRO-NOR-SOP-06 P 20/26

Question 27

Nosso plano saiu restrito inicialmente FL300, pq?

Answer 27

A explicação é o LIDO, considerou inicialmente esse nível mais económico, em função de vento, shear etc…

Question 28

Diferença entre o botão vermelho da RAT e do EMER GEN no OVHD, quando que entra um e quando que entra o outro.

Answer 28

Hydraulics FCOM DSC-29-20 P 3/1
RAT MAN ON pb The RAT may be extended at any time by pressing the RAT MAN ON pb. Note: The RAT automatically extends in flight, if: Both engines fail, or GREEN + BLUE LO LVL, or GREEN + YELLOW LO LVL.
Electric FCOM DSC-24-20 P 6/24
EMER GEN FAULT lt The light comes on red, if the emergency generator is not supplying and normal AC supply is lost in flight.

Question 29

Fraseologia TCAS

Answer 29

Azul 4288 TCAS RA

MGOA MGOA-1059

Question 30

O que falar quando estiver em uma situação de emergência?

Answer 30

The emergency message shall contain the following information (time and circumstance permitting) and, whenever possible, should be passed in the order given: a. ‘MAYDAY/MAYDAY/MAYDAY’ (or ‘PAN PAN/PAN PAN/PAN PAN’); b. Name of the station addressed (when appropriate and time and circumstances permitting); c. Call sign; d. Type of aircraft; e. Nature of the emergency; f. Intention of the person-in-command; g. Present or last known position, flight level/altitude and heading.
MGOA-1092

Question 31

Simulado de alternado, quanto que vamos precisar alijar? Qual seria o gerenciamento?

Answer 31

The jettison operation continues, until one of the following occurs: ‐ The crew stops the operation. ‐ Both inner fuel tank low level sensor on one side become dry. ‐ The Fuel Control and Monitoring System (FCMS) stops the operation at a fuel content level preset on the FMGES MCDU. ‐ The combined inner tank fuel quantity is less than 10 000 kg (22 000 lb).
FCOM DSC-28-10-120 P 1/4

Question 32

Pousando não tem handling, como que faz?

Answer 32

World Service

Question 33

Carga perigosa, se estiver transportando, o que o controlador vai querer saber em um situação de emergência? Ocorrendo uma emergência em voo, o Comandante deve informar ao ATC, para conhecimento das autoridades do aeroporto, a existência de quaisquer Artigos Perigosos a bordo.

Answer 33

Onde que estão as nossas ações quando tiver emergência com carga perigosa.
Se a situação permitir, a informação deve incluir: a. N° UN/ID ou nome do artigo perigoso (Proper Shipping Name); b. A quantidade do artigo sendo transportado a bordo; c. Localização do artigo;
ERG CODE – também conhecido como drill code.
Quando não for possível incluir toda a informação, considere, pelo menos, as partes mais relevantes.
MGOA MGOA-331

Question 34

O que devemos avaliar para mudança de nível? Peso, temperatura, Shear

Answer 34

OPT FL displayed on the MCDU is the cruise altitude for minimum cost when ECON MACH is flown and should be followed whenever possible. It is important to note that the OPT FL displayed on the PROG page is meaningful only if the wind and temperature profile has been accurately entered. The Flight crew should be aware that flying at a FL different from the OPT FL can have an adverse effect on the trip cost. For each Mach number, there will be a different OPT FL. Should an FMGES failure occur, the crew should refer to the FCOM or QRH to determine the OPT FL. FCOM and QRH charts are only provided for four different Mach numbers.
From a cost point of view, it is better to climb to a higher cruise altitude when aircraft weight permits, because the optimum altitude increases when fuel is consumed during the flight. This technique is referred to as a Step Climb.
FCTM PR-NP-SOP-150 P 7/10

Question 35

Como ativar A/THR.

Answer 35

The flight crew arms the A/THR: ‐ On ground: • By pushing the A/THR pb on the FCU when the engines are not running, or • By setting the thrust levers at the FLX or TOGA detent, when the engines are running. ‐ In flight: • By pushing the A/THR pb on the FCU while the thrust levers are out of the active range, or • While A/THR is active (“A/THR” white on the FMA), by setting all thrust levers beyond the CL detent, or at least one lever beyond the MCT detent, or • By engaging a go-around (MAN TOGA) or a Soft Go-Around (MAN GA SOFT): the flight crew sets the thrust levers to the TOGA detent. Then, in the case of soft go-around, the flight crew retards the thrust levers to the FLX/MCT detent.
FCOM DSC-22_30-90 P 4/18

Question 36

Alpha Floor Protection, quando que é ativado e em quais momentos é inibido?

Answer 36

The αfloor protection is triggered when the FMGECs receive a signal elaborated by the PRIMs. This signal is sent when the aircraft’s angle of attack is above a pre-determined threshold function of the aircraft’s configuration. A/THR is automatically activated and commands TOGA thrust, regardless of the thrust levers positions. The thrust remains at TOGA, as long as αfloor conditions are applicable and the speed is at or below VLS. This protection is available from liftoff to 100 ft RA in approach. A.FLOOR is then displayed in green, and outlined with a flashing amber box on the FMA, and on the EWD
αfloor is inhibited: ‐ In case of engine failure, with the flaps extended ‐ In case of engine failure, with derated TO selected ‐ Below 100 ft at landing ‐ Above M 0.53.
DSC-22_30-90 P 15/18

Question 37

Se estiver no meio do oceano e precisar usar ACARS via SATCOM como que faz?

Answer 37

It provides both voice and data channels: One or several channels are used for voice transmissions (cockpit or cabin voice). The cockpit voice function must be activated, in order for it to be available
The MANUAL DIAL PAGE enables the crew to initiate an air to ground call by manually entering a phone number.

So mudar a frequência do OVHD que ele deixa de transmitir em VHF 3 e passa para o SATCOM.

DSC-23-30-20-20 P 3/6

Question 38

Se pousarmos em um aeródromo e o abastecedor não souber abastecer, como que faz?

Answer 38

AUTOMATIC REFUELING From refueling control panel : [LOAD PRESELECTOR sw] REQUESTED BLOCK FUEL…………………………………………..SET REFUEL VALVES sel……………………………………………………….CHECK NORM and GUARDED MODE SELECT sw…………………………………………………………………………………………..REFUEL On completion of refueling : END light comes on. It flashes if after refueling an imbalance greater than 3 000 kg (6 614 lb) exists. ACTUAL QUANTITY…………………………………………………………………………………….CHECK MODE SELECT sw……………………………………………………………………OFF and GUARDED

From cockpit : BLOCK FUEL on FMGS MCDU INIT B page……………………………………………..CONFIRM/SET The CKPT light on the refueling control panel comes on. Note: Once BLOCK FUEL value has been entered on the MCDU, the aircraft will refuel to the MCDU value. Refuel to this value can be started from either panel.
FCOM PRO-NOR-SUP-FUEL P 3/10

Question 39

Explicar a sequencia de abastecimento e onde encontro esse procedimento?

Answer 39

FCOM Supplementary Fuel- refueling
Procedure for refueling
Preparation - automatic or manual refueling

DIM-1-30 - Capítulo 1: PESO E BALANCEAMENTO Seção: Ordem de abastecimento automático dos tanques

Question 40

Abastecimento manual, como que faz e onde está o procedimento?

Answer 40

MANUAL REFUELING DETERMINE FUEL QUANTITY IN EACH TANK Respect distribution in accordance with applicable REFUEL DISTRIBUTION graph . Note: To refuel the trim tank, one of these conditions must be fulfilled. ‐ the two inner tank inlet valves are open. ‐ both inner tank quantities are each greater than 14 000 kg. ‐ one inner tank quantity is greater than 14 000 kg and the other inner tank inlet valve is open. REFUEL VALVES sel…………………………………………………………………………………………………SHUT

REFUEL VALVES sel (tank(s) to be filled)……………………………………………………………………OPEN Note: Because the Fuel Control and Monitoring System (FCMS) does not have control of all the tanks, the END light will flash. MODE SELECT sw………………………………………………………………………………………………..REFUEL FUEL QTY…………………………………………………………………………………………………………..MONITOR  When the tank contents reach the required level : Corresponding REFUEL VALVES sel……………………………………………………………………..SHUT MODE SELECT sw………………………………………………………………………….OFF and GUARDED REFUEL VALVES sel…………………………………………………………………..NORM and GUARDED

PRO-NOR-SUP-FUEL P 5/10

Question 41

Como inserir no FMS um Mach constante.

Answer 41

ENTERING A CONSTANT MACH SEGMENT SELECT the F-PLN key on MCDU. SELECT a VERT REV at revised waypoint (except destination and alternate flight plan waypoint). WRITE the Mach/start waypoint pair. It is possible to enter only the Mach or the waypoint. But, for the first entry, a Mach entry is mandatory. The waypoint must be located in front of the aircraft and must be part of the cruise. ENTER it in 4L field The END WPT prompt appears in the 4R field.
DSC-22_20-30-20-25 P 14/16

Question 42

Combustivel minimo de espera, como saber quanto tempo tenho de espera?

Answer 42

HOLDING FUEL Calculation of holding fuel should take into account the altitude of the alternate and the landing weight at the alternate, using holding charts of Refer to PER-HLD-GEN GENERAL. A conservative quantity corresponding to 30 min holding at 1 500 ft above alternate airport elevation at green dot speed in the clean configuration is 2 800 kg or 6 200 lb.

PER-FPL-GEN-MFR P 1/4

Question 43

Mayday Fuel e Minimum Fuel?

Answer 43

O Piloto em Comando deverá declarar “Emergência por Combustível” (“MAYDAY FUEL”) ao constatar que, mesmo pousando no aeroporto adequado mais próximo, o Combustível remanescente a Bordo no pouso será menor do que o Combustível de Reserva Final planejado na navegação (planned final reserve fuel)

O Piloto em Comando deverá declarar “COMBUSTÍVEL MÍNIMO” (“MINIMUM FUEL”) sempre que todas as opções de aeroportos para pouso forem reduzidas a um único aeroporto e julgar que qualquer alteração na autorização ATC existente possa resultar em consumo do Combustível de Reserva Final planejado na navegação (planned final reserve fuel)
MGOA cap. 9

Question 44

Na aproximação final antes do pouso, ligou APU, pq? Explicação de qual bomba alimenta a APU e em que momento.

Answer 44

LH INR TK
Descent and landing, ground operation, climb to FL 255, and inflight above FL255 with trim tank empty.
Fwd APU pump running - aft APU pump not running

DSC-28-10-100 P 2/6

Question 45

ATC questiona quanto tempo para cruzar FL XXX? Como descobrir usando FMS?

Answer 45

The MCDU PROG page provides the crew with the MAX REC ALT and with the OPT ALT information (See cruise section). This information is to be used to rapidly answer to ATC: “CAN YOU CLIMB TO FL XXX?” The MCDU PERF CLB page provides predictions to a given FL in terms of time and distance assuming CLB mode. This FL is defaulted to the FCU target altitude or it may be manually inserted. The symbol level arrow on the ND assumes the current AP engaged mode. This information is to be used to rapidly answer to ATC: “CAN YOU MAKE FL XXX by ZZZ waypoint?”. The crew will use a PD (Place/Distance), i.e. ZZZ,-10 waypoint if the question is “CAN YOU MAKE FL XXX , 10 N.m before ZZZ point?”
FCTM PR-NP-SOP-140 P 3/4

Question 46

Conversa sobre proteção de pitch e bank em normal law.

Answer 46

The normal law provides complete flight envelope protection as follow : ‐ Load factor limitation ‐ Pitch attitude protection ‐ High angle of attack (AOA) protection ‐ High speed protection

DSC-27-20-10-20 P 4/18

Inside the normal flight envelope, the system maintains positive spiral static stability for bank angles above 33 °. If the pilot releases the sidestick at a bank angle greater than 33 °, the bank angle automatically reduces to 33 °. Up to 33 °, the system holds the roll attitude constant when the sidestick is at neutral. If the pilot holds full lateral sidestick deflection, the bank angle goes to 67 ° and no further.

DSC-27-20-10-30 P 3/4

Question 47

22B na localização de carga na NOTOC, a carga esta em qual compartimento?

Answer 47

Informação esta no manual de Weight and Balance.

Question 48

Posso desligar as baterias com a APU ligada?

Answer 48

Não, pois as baterias garantem a proteção da APU, Auto Shutdown.

OFF : The Battery Charge Limiter is not operating, the DC ESS BUS is not connected to the battery (except in flight in emergency configuration). OFF comes on white if the DC BAT BUS is powered. Hot buses remain supplied. DSC-24-20 P 2/24

APU FAULT WITH AUTOMATIC SHUTDOWN
9. DC power interrupt (BAT OFF, when aircraft on batteries only)
DSC-49-10-20 P 3/4

Question 49

Explicar sobre GRID MORA e MEA, onde achar essas informações.

Answer 49

GRID MINIMUM OFF-ROUTE ALTITUDE (Grid MORA) — An altitude derived by Jeppesen or pro-vided by State Authorities. The Grid MORA altitude provides terrain and man-made structure clearance within the section outlined by latitude and longitude lines. MORA does not provide for navaid signal cov-erage or communication coverage. a. Grid MORA values derived by Jeppesen clear all terrain and man-made structures by 1000ft in areas where the highest elevations are 5000ft MSL or lower. MORA values clear all terrain and man-made structures by 2000ft in areas where the highest elevations are 5001ft MSL or higher. When a Grid MORA is shown as “Unsurveyed” it is due to incomplete or insufficient tion. Grid MORA values followed by a +/- denote doubtful accuracy, but are believed to provide sufficient reference point clearance. b. Grid MORA (State) altitude supplied by the State Authority provides 2000ft clearance in moun-tainous areas and 1000ft in non-mountainous areas.

MINIMUM ENROUTE IFR ALTITUDE (MEA) — The lowest published altitude between radio fixes that meets obstacle clearance requirements between those fixes and in many countries assures accept-able navigational signal coverage. The MEA applies to the entire width of the airway, segment, or route between the radio fixes defining the airway, segment, or route.
Jepp Intro

Question 50

Pousou em Chicago, ai precisa decolar… tem SLUSH na pista, esta contaminada, não tem acesso a DOV, e não tem analise de pista, como que faz?

Answer 50

SLUSH : Slush is snow soaked with water, which spatters when stepped on firmly. Slush occurs at temperatures around 5 °C and has a density of approximately 0.85 kg/l (7.1 lb/US Gal).

Performance do FCOM, tem tabelas para decolagem com pista

Question 51

Com quanto de peso que vou conseguir subir para o FLXXX?

Answer 51

OPTIMUM AND MAXIMUM ALTITUDES

Utilizar o QRH para ver essa informação.
QRH

Question 52

PACK FLOW LOW, economiza combustível? Em qual parte do manual consigo ver isso?

Answer 52

Saves fuel.
- 0.9 %
FCOM PERFORMANCE PER-FPL-FLP-QFP-40 P 3/44

Question 53

Explicar como que eu faria uma analise de múltiplas panes no QRH?

Answer 53

METHOD TO DETERMINE AIRCRAFT PERFORMANCE AT LANDING WITH SEVERAL FAILURES
QRH

Question 54

Definição de Ice Acrettion e Severe Ice

Severe Icing Conditions: Quando o acumulo de gelo estiver acima de 5mm de espessura ou mais.

Answer 54

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.

Ice accretion - Evidence of ice accretion can be ice on the visual indicator (between the two cockpit windshields) or on the windshield wipers.
PRO-NOR-SUP-ADVWXR P 18/26
severe ice - Ice accretion is considered severe when the ice accumulation on the airframe reaches approximately 5 mm (0.2 in) thick or more.
LIM-ICE_RAIN P 1/2

Question 55

Qual a temperatura de WarmUp do motor NEO

Answer 55

After start, to avoid thermal shock, the engine should be operated at idle, or near idle for at least: ‐ 5 min when engines are cold, or ‐ 2 min when engines are warm after a stop of 2 h or less

PRO-NOR-SOP-09 P 1/6

Question 56

Como desativar A/THR

Answer 56

Standard disconnection: • The flight crew pushes the instinctive disconnect pb on the thrust levers (which immediately sets the thrust corresponding to the lever positions), or • The flight crew sets all thrust levers to IDLE detent.
FCOM DSC-22_30-90 P 6/18

Question 57

Sair do Thrust Lock

Answer 57

The thrust is locked or frozen at its level prior to disconnection. Moving the thrust levers out of the CL or MCT detent suppresses the thrust lock, and reverts to manual control.

DSC-22_30-90 P 7/18