1
Q
Airspeed for climb in sev turbulence
A
280kias/.76M
2
Q
Max Fuel temperature
A
+49 °c
3
Q
Max speed tonuse alternate flaps
A
230kias
4
Q
During rapid depressurization, passenger Oxy switch activates when:
A
Cab altitude reach 14000ft
5
Q
Max wind for autoland
A
H25
X20
T10
6
Q
Max speed with window overheat
A
250kt below 10000ft
7
Q
Max Flap extended altitude
A
20000ft
8
Q
Do not deploy Spd brakes in flight at RA below:
A
1000ft
9
Q
Holding in icing conditions with flap extended:
A
Not permitted
10
Q
Max/min runway slope
A
+/- 2%
11
Q
Max takeoff/landing altitude
(With high altitude system)
A
8400ft
(13500ft)
12
Q
Max operating altitude
A
41000ft
13
Q
Scape slides must be armed for:
A
Taxi, takeoff and landing
14
Q
Stby altimeters for RVSM
A
Do not meet accurancy
15
Q
Max difference between capt and f/o altimeters in flight
A
200ft
16
Q
On the ground, max difference between capt and f/o altimeters
A
MSL/5000ft = 50ft
5001ft/10000ft = 60ft
17
Q
Max cabin differential pressure
A
9.1 psi
18
Q
Use aileron trim with A/P engaged
A
Prohibited
19
Q
During takeoff, do not engage A/P below:
A
400ft
20
Q
For landings above 8400ft, do not use A/P below
A
100ft RA
21
Q
Max/min glide slope angles for autolanding
A
Max 3.25
Min 2.5
22
Q
Autolanding may only be used on runways:
A
At or below 8400ft pressure altitude
23
Q
The use of LVL CHG during approach:
A
Gol: PROIBIDO após IAF (MSA se n houver iaf)
(Boeing: Not permitted below 1000ft AFE)
24
Q
Eng limit display markings are:
A
Min/Max red
Caution amber
See AFM limitations
25
Eng ignitions must be on for:
Takeoff
Landing
Anti-ice operation
In heavy rain
26
APU operating limits
Ground bleed + elec : 15000ft
Bleed + elec : 10000ft
Bleed: 17000ft
Elec: 41000ft
27
Apu bleed valve must be closed when:
- Gnd air connected/ isol open
- eng 1 bleed on
- eng 2 bleed on/ isol open
28
After three APU start attemps, cooling period:
15min
29
Fuel imbalance must be schedule:
To be zero (Max 453kg)
30
At what cabin altitude is the passenger oxygen system automatically activated?
14000ft
31
PASS OXY ON illuminated indicates:
Masks have dropped
32
737ng cargo compartments, are fire containment designed:
Class C
33
What the position of the isolation valve when the switch is in auto?
Open, if either Bleed or Pack switch in off
34
Bleed air duct pressure indicator is:
Ac operated
35
Pack illuminated indicates:
Pack trip off or failure of both primary and stby controls
36
Window heat pwr test verifies:
Operation of the window heat system
37
When are the Eng anti-ice turned on if icing conditions exist on the ground?
During after start procedure
38
Which pitot probe and sensors are not heated?
Static ports
39
After lift-off, A/T remains in throttle hold until:
800ft AFE
40
Cws Roll operation, the acft will roll wings level when:
Control wheel pressure is released and bank angle is 6° or less
41
The AFS (automatic flight system) consist of:
Autopilot flight director system(AFDS) and A/T
42
Cockpit voice recorder
Use four channels to record flight deck audio for 120min
43
Flight deck CALL light indicates:
Flight attendants or ground crew are calling
44
Altitude alert/ egpws/ WS with audio in the degraded mode
Are not heard
45
Bat discharge indicates:
Excessive battery discharge with battery switch on
46
In flight, TR UNIT light indicates:
Tr 1 or Tr 2 and Tr3 fails
47
Basic principle of 737 electrical system
There is no paralelling of the AC sources
48
If eng oil pressure is at amber band with takeoff power:
Do not takeoff
49
Pack switches position during secure checklist
Off
50
APU may be used as an electrical and bleed air source simultaneously in flight up to
10000ft
51
APU DET INOP indicates:
No fire protection, do not start the APU
52
Eng fire detection requires:
Both loops must sense a fire or overheat
53
Power source for engine fire extinguishing
Hot battery bus
54
Prior to perform Fire/ovht test with APU operating:
Advise ground personnel
55
How many flight spoilers are on each wing?
4
56
Correct position of spd brake lever to use spd brake in flight
FLT detent
57
ALTN FLAPS switch:
- Arm altn flaps position switch
- activates stby hyd pump
- closes TE flaps bypass valve
58
DH or minimums are set:
Independently by each pilot using efis control panel
59
Flight recorder operates:
On the ground: When electrical power is available and either engine is operating
In flight: operantes anytime electrical power is available
60
Position trend vector on ND represent
Prediction of acft position at the end of 30s, 60s and 90s intervals
61
Cds fault indication occours:
On the ground, before start the second engine
62
Whan an active database expires in flight what occours:
Remains in use until the active database is changed
63
Which fator is not considered in the Trip/crz computation
Reserves
64
Max angle can be selected on which page of fmc
CLB
65
Where fuel bypass valves are located?
Both main tanks
66
Where is the fuel temperature sensor located?
Main tank number 1
67
Can tank to tank tranfer of fuel be accomplished in flight?
No
68
Leak on system B affect stby hydraulic system?
No
69
Auto slats are powered by
System B (LE devices)
70
Hydraulic fluid is cooled by:
Heat exchangers, in the main tanks
71
Landing with autobrake in RTO:
No autobrake will occurs, autobrake disarm illuminates 2s after touchdown
72
What system provides hyd pressure for steering?
System A
73
What happens if a Rto occurs at 90kt with a-brake in RTO?
Max braking pressure is applied when thrust levers are selected to idle
74
PSEU monitors on the ground
- Tkoff/ldg config warnings
- ldg gear config warning
- air/ground sensing
75
When Mach/airspeed warning test is inhibited?
In flight
76
When egpws test switch is inhibited?
In flight
77
Com Flap 1 qual velocidade devemos manter? (Calculo pela Vref)
Vref 40 + 50
78
Describe a rejected landing
A go-around/missed approach initiated below Da/mda and before touchdown
79
Max crosswind dry/wet
32/25 (takeoff and landing)
80
Max crossind for autolanding
(Dry/ wet)
20 / 15
81
Gradiente mínimo do 737 monomotor no segundo segmento de decolagem
2.4%
82
Numa app RNP lnav/vnav, qual o mínimo a ser considerado pela carta de aproximação?
DA (se for só lnav: MDA)
83
Callout padrão para responder manutenção após "slats moving"
Ciente, remova o pino com sinal visual a esquerda/direita
84
Standard callout para comandar recolhimento trem de pouso
Positive rate / gear up
85
Callout do PM a 1000ft AFE durante aproximação:
- One thousand stabilized
- one thousand not stabilized, go-around
86
Condições para usar Eng e wing anti-ice na decolagem:
Oat no solo/ tat em voo igual ou menor que 10°c com:
- Umidade visível
- gelo, neve, lama, água parada no pátio, txy ou rwy
87
O que levar numa evacuação
Flash light and smooke hood (if needed)
88
Callout de speed
Vapp +10 / -5
89
Cite 4 situações de reporte obrigatório
Egpws
Aleta fogo/fumaça
Hard landing
Overspeed
Flap/ gear exceedance
Stickshaker
Upset
As
Tcas ra
Rto
Pouso abaixo combustível minimo(30min)
Tail strike
Airspeed unreliable
Despressurização
90
Como saber se a bateria está carregada
Set BAT or AUX BAT:
DC AMPS deve ser ZERO
91
Pane de TR Unit
- Não usar App Mode
Quando selecionar app e o GS for capturado a CROSS BUS TIE abrira e a pane será evidente, quando apertar To/ga a cross bus tie relay fechará.
92
Após perder um sistema hidráulico e seleciona stby rudder a low press light da stby pump acende
A bomba falhou ou o cb tripou (Cb fica no EE - electronic equipments bay)
93
GRD e não deu partida:
Muda o ignitor(Right Ignitor está na AC STBY BUS)
Pode ser o CB da ignição que esta saltado ENG 1 (P18-2 A1/3), ENG 2 (P6-2
D4/6).
*Somente a manutenção coloca o CB
94
Start valve não abre:
procedimento é abrir manualmente pela manutenção.
95
Ligar APU durante abastecimento:
Proibido
96
Pane conjulgada que resulte em R pack e L bleed INOP:
Start APU para usar APU bleed, descer para 17000ft para usar APU bleed
97
IRS FAULT – ATT mode failure can be recognized by
loss of PITCH and ROLL indication
98
IRS FAULT – NAV mode failure can be recognized by
loss of GROUNDSPEED and PRESENT
POSITION DATA
99
Quantas partidas anormais há?
1 LOW OIL PRESSURE
2 WET,
3 HOT,
4 HUNG,
5 NO N1 ROTATION,
6 HIGH OIL TEMPERATURE,
7 TAILPIPE FIRE,
8 START VALVE OPEN
9 HIGH VIBRATION.
100
falha da TRANSFER BUS 2
bom saber o que esta ligado nesse
barramento, STABILIZER TRIM INOP, pouso com Flap 15
101
Panes conjuntas de pack e bleed opostas:
alimentação cruzada com ISOLATION OPEN enquanto vai tentando TRIP RESET (não limita tentativas)
Não iniciar a descida pois pode diminuir a pressão no duto
agravando ainda mais a pressurização.( pois reduz motor)
102
BRAKE ACCUMULATOR em zero
o NNC fala para checar o
sistema hidráulico, se estiver tudo normal prossegue (NNC aplicável somente em
voo), no chão volta para o gate para cumprir procedimento MEL
103
Anti ice acima do FL350
Não se usa, pode causar bleed trip off, gelo só forma entre +10°c e -40°c
GOL
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Decks in class (4)
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