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HYD AUX PUMP Flashcards

Sist BLUE<1500PSI GEAR HANDLE DONW MOTOR GIRANDO PROP BRAKE REALESED

1
Q

HYD AUX PUMP

A

Sist BLUE <1500PSI
GEAR HANDLE DONW
MOTOR GIRANDO
PROP BRAKE RELEASED

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2
Q

ELEC FUEL PUMP

A

PB on
JET PUMP PRESS< 5PSI
XFEED ON
FUEL LO LV

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3
Q

TRU

Basic mode

A 
ALIMENTA 4 BARRAMENTOS
AC STBY BUS
EMERG BUS
ESS BUS
STBY BUS
TRU transforma corrente ACW-> DC
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4
Q

TO CONFIG

A 
PWR MGT TO
FLAP15
TLU LO SPEED
PITCH TRIN GREEN 
NO AILERON LOCK LIT
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5
Q

Punho de fogo

A 
ENERGIZA SQUIBS
CORTA COMBUSTIVEL
DESLIGA CORRENTE DC e ACW
DE ICE
Tira BLEED
EMBADEIRA
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6
Q

PROB BRAKE

A 
ACFT ON GROUND
GUST LOCK
CL FHT or  FUEL SO
PRESSAO BLUE 2100 PSI
FIRE HANDLE NÃO  puxado
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7
Q

ATPCS

A

ATPCS PB ON
PWR MGT TO
PL>49°
TQ>46%

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8
Q

Não reseta

A 
Leak 
LO LV
BUS
EEC
PEC
CABIN PRESS
Bateria  MAIN /EMERG
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9
Q

1°Ovrd

2° ovrd -> Botão sist elétrico
Ovrd und/v

A

1° OVRD
Tira todas as proteções das baterias

2°OVRD
O sistema DC STBY BUS passa de HOT MAIN para HOT EMER BAT BUS a alimentação da DC STBY BAT BUS e INV 1
Pq
UND/V = DC STBY BUS <19.5V fica apenas alimentando a DC ESS BUS

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10
Q 
Limite do motor
Mas ITT 
acionamento 
Operação motor
Hotel mode
ITT na decolagem
A

ACIONAMENTO
800°C- ilimitado
801° C até 840 °C -20s
841 Até 950°C - 5s

OPERAÇÃO MOTOR
Abaixo de 800°C ilimitado
840°C 20s

HOTEL MODE
715°C

Na dep
765°C

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11
Q

Torque max

A

Até 106.3% com NP<94 ILIMITADO
até 106.3 %com NP>94 10mim
106.4% até 120% com NP >94 20s

Ex 107% com NP 100% limitado em 20s

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12
Q

Temperatura que ocorre NAC OVHT

A

T>170°C

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13
Q

Qtos PSIs muda passando para Hight flow

A

O fluxo passa de 22PSI para 30PSI

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14
Q

Qual a pressão que tem que indicar no teste de máscara?

A

1500PSI

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15
Q

GND HDLG BUS

A

Só funciona no solo
DC SVCE BUS que supre qdo a EXT PWR está ON
Qdo a EXT PWR OFF vai ser suprida pela HOT MAIS BAT BUS qdo
* abrir a porta principal do avião
* abrir o painel de carga ou o de abastecimento

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16
Q

GND HDLG BUS

A

Só funciona no solo
DC SVCE BUS que supre qdo a EXT PWR está ON
Qdo a EXT PWR OFF vai ser suprida pela HOT MAIN BAT BUS qdo
* abrir a porta principal do avião
* abrir o painel de carga ou o de abastecimento

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17
Q

Pesos

A

Max de rampa 23170 / 22970
Max de dep 23000/ 22800
Max de pouso 22350/22350
Max zero comb 21000/20800

18
Q

Velocidades

A 
0.55 MMO
250 VMO
185 FLAP 15/ TREM DE POUSO ESTENDIDO
180 VRA (TURBULÊNCIA)
175 VA
170 ESTENDER O TREM
165 TIRE SPEED
160 RECOLHER O TREM e Wiper
150 FLAP 30
19
Q

Sistema pneumático

A

Max diferencial de pressão 6.35psi
Max diferencial de pressão negativo -0.5psi
Max diferencial de pressão pouso 0.35psi
Max diferencial de pressão OVBD FULL OPEN 1PSI
Max alt ONE BLEED OFF 20000FT

20
Q

Starter

A

3 tentativas dentro de 1mim 30s após 4mim OFF

21
Q

Combustível

A 
Temp mínima-34°C
Temp Max 57°C
Total de comb em cada asa 2500kg
Max umbalance 730kg
Max umbalance OEI 200kg
22
Q

Vento

A

25kt (dep/App RWY DRY e comp de proa CAT2, dep/app RWY SECA TRAVES

20KT ( dep RWY WET)

15 KT ( CAT II . APP RWY WET. DEP/APP RWY CURTA/ESTREITA/TWY DRY

10KT ( DEP/APP RWY CONTAMINADA GROOVED e MAX COMP DE CAUDA)

5KT ( DEP/APP RWY CURTA/ESTREITA/TWY WET e DEP /APP RWY CONTAMINADA NON-GROOVED

45KT door

23
Q

DC GEN 1+2 FAULT

A 
PF-- CAPT
DC GEN 1+2 -- RESET
■IF ONE GENERATOR recovered 
DC GEN 1(2) PROCEDURE A24.13
■ IF NO GENERATOR RECOVERED 
HYD GREEN PUMP ---OFF
TRU---ON
■ IF TRU ARROW LIGHT
MAX IMC FLIGHT TIME 30MIM
TRU --OFF
LAND ASAP
24
Q

Eng 1+2 FLAME OUT

A 
PF-- CAPT
PL1+2--- FI
■ IF NH DROPS BELOW 30%
CL 1+2 --- FTR THEN FUEL SO
OPTIMUN SPEED-- VMHB
25
Q

ENG 1(2) FIRE OR SEVER MECHANICAL DAMAGE ON GROUND

A 
ACFT --STOP
BRAKE HANDLE--- PARKING
CL1+2-- FTR THEN FUEL SO
FIRE HANDLE --- PULL
■ IF FIRE PERSIST
AGENT 1-- DISCH
■ IF FIRE PERSIST AFTER 30S
AGENT 2--- DISCH
26
Q

SEVERE ICING

A

IAS — INCREASE MAINTAIN ICING BUG +30kt
PWR MGT—-MCT
PL—ajust
CL—100%OVRD

27
Q

Stall

A 
CONTROL COLUMN---PUSH
ENG PWR--INCREASE
■ IF FLAP 0
FLAP 15 SET
BANK--- WINGS LEVEL
28
Q

INCREASE SPEED

A

IAS INCREASE ABOVE ICING BUG+30KT

29
Q

ENG FIRE AT TO

A

When airborne
LDG GEAR –UP

at acc altitude
PWR MGT–MCT

ATIVA CONTINGENCIA
SET NAV

AT VFTO
■IF NORMAL CONDITIONS 
FLAP 0
■IF ICING CONDITIONS 
FLAP 15 
PL--- FI
CL--- FTR THEN FUEL SO
FIRE HANDLE RED LIGHT ---PULL
■ IF 10S FIRE PERSIST
AGENT 1--DISCH
■IF 30 S FIRE PERSIST 
AGENT 2--DISCH
BLEED ENG ALIVE---OFF(se tiver abaixo de 90.9)
30
Q

ENG FLAME OUT AT TO

A 
Uptrim 
Autofeather 
■IF NO UPTRIM
PL 1+2-- RAMP
•WHEN AIRBORNE 
LGD GEAR--UP
BLEED1+2--OFF
•AT ACCELERATION ALTITUDE 
ALT --SET
SPEED AUTO VFTO
ATIVA CONTINGENCIA 
•AT VFTO
PL --NOTCH
PWR MGT ---MCT
■IF NORMAL CONDITIONS 
FLAP 0
■IF ICING CONDITIONS 
FLAP 15

IAS—-SET
PL—FI
CL– FTR THEN FUEL SO
BLEED-OFF(se river menor a 90.9% TQ)

31
Q

ABNORMAL parameters during start

A

■IF ITT TENDS TO EXCEED 900°C OR NO ITT OR NO NH
CL –FUEL SO
ENG START ROTARY SELECTOR -OFF START ABORT

32
Q

EMERGENCY DESCENT

A 
O2 -ON
GOGGLE AS REQ
CREW COMMUNICATIONS 
DESCENT 
PL -FI
CL --100%
33
Q

UNRELIABLE AIRSPEED INDICATION

A 
AP/YD-- OFF
FD--STBY
PITCH AND TQ --- MANTAIN
■IF AT TO OR GA BELOW 1500FT
PITCH --8
ICING AND VOLCANIC ASH-- ESCAPE
34
Q

Fire LOOP FAULT

A

Loop–OFF

35
Q

PEC FAULT

A

■ if below 400ft

GO AROUND —APPLY

36
Q

LO PITCH IN FLIGHT

A

Pl –FI

CL–FTR THEN FUEL SO

37
Q

FLAPS UNLK

A 
■if before V1
TO ---ABORT
■IF AFTER V1
VR, V2 -- SPEED BUG AUTOMATICALLY INCREASES 
■ IF DURING APP
GO AROUND 
VGA--- NOT LESS THE VmimOPS
38
Q

PITCH DISCONNECT

ELEVATOR JAM

A

COLUMN—IDENTIFY
PF– COLUMN FREE
IAS –180KT

39
Q

Voltagem da fonte GPU

A

28v mínimo abaixo tem q fazer weak GPU

40
Q

Janela de estabilização

A 
LDG DOWN
FLAP 30
SPEED VAPP+10/-5
LOC 1/2DOT
GS 1DOT
RNP 1DOT
DESCENT RATE -1500FT/MIM
CHECKLIST COMPLETO
41
Q

Velocidades taxi

A

Max 30kt
Recomendada 20kt
Patio 10kt dry
5kt wet

42
Q

Gradients

A 
1 seg- positivo
2 seg =2.4%
3 seg =1,2%
4 seg =1.2%
App climb =2,1%
Landing climb=3.2%
Decolagem normal =3,3%
Arremetida normal =2,5%

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