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A330-200 Systems > Normal procedures > Flashcards

Normal procedures Flashcards

1
Q

Preliminary Cockpit Preparation

FCAP - APU start

A

APU……………………………………………………………………………..START
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;
c)FTIS (Fuel Tank Inerting System): Aircraft with placard NO FTIS should remain with both packs off when the temperature is above 15°C until 30 minutes prior to the estimated time of departure regardless of cabin temperature. It is not necessary to shutdown the APU;
d)In order to reduce cabin temperature, after APU start, select both packs to ON until the temperature drops below 26°C then select PACK 1(2) OFF according the day of the flight. Change between the packs on each flight, in order to prevent excessive wear of one pack.

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2
Q

Preliminary Cockpit Preparation
FCAP
EXT PWR pb-sw

A

*EXT PWR pb-sw ……………………………………AS RQRD
GPU should be left ON even after APU AVAIL, this action reduces generator load and, as a consequence, decrease fuel consumption.

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3
Q

Preliminary Cockpit Preparation
FCAP
*AIR COND panel…………………………………….SET

A

*AIR COND panel…………………………………….SET
FWD Cargo Cooling may be selected to OFF if there is no livestock on fwd cargo hold

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4
Q

Preliminary Cockpit Preparation
FCAP
*PACKS 1 or 2……………………………………AS RQRD

A

*PACKS 1 or 2……………………………AS RQRD

Use odd days for PACK 1 OFF and even days for PACK 2 OFF

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5
Q

Preliminary Cockpit Preparation
FCAP
*ECAM ENG OIL QTY………………………….CHECK

A

*ECAM ENG OIL QTY………………………………………………………………………….CHECK
Check that the oil quantity is at or above 6 qt + estimated consumption (average estimated consumption = 0.7 qt/h) but not lower than 15 qt.

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6
Q

FCAP Cockpit preparation

NAV & LOGO Lights

A

During daytime operation, NAV&LOGO lights must be turned ON prior to external inspection and turned OFF after the external inspection is accomplished. At night NAV&LOGO lights must be turned ON once the airplane is energized.
Vai ser ligada mesmo somente para o pushback junto com a beacon.

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7
Q

FCAP LMC

A

900KG

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8
Q

FCAP ENGINE START

PACKS …………………. ON

A

After the ENG START selector is commanded to IGN/START position by CM1, the PACKS must be turned ON.

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9
Q

FCAP No after landing, quanto tempo deve-se esperar para dar start na apu após ter selecionado o APU MASTER sw ON/R?

A

The APU MASTER pb-sw must be turned ON at least 2 minutes before pushing the APU START pb-sw to avoid fuel starvation during start.

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10
Q

FCAP No after landing, qual a TAT para deixar flaps em CONF 1?

A

Select slats in CONF 1 when OAT is above 30ºC.

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11
Q

FCAP No after landing, quando podemos cortar o ENG 2 após o pouso?

A

Após 1 min em Idle (sem reverso começa no flare e com reverso, após voltar para idle).
APU…………………………………………………..START/2MIN
When the APU indicates AVAIL and during taxi in a straight line:
ENG 2……………………………………………….SHUT DOWN

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12
Q

FCAP Quando é feito o After Landing?

A

After landing flow can be initiated on taxi speed, however, After Landing Checklist must be read after vacating the runway.

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13
Q

FCAP Quando desliga a beacon e nav no parking?

A

Only when all slides are disarmed on ECAM DOORS/OXY page, CM1 should set BEACON light OFF.
This procedure ensures that the slides are disarmed prior to the approach of any equipment/person near the aircraft.
NAV&LOGO sw……………………………………….AS RQRD
During day time operation NAV&LOGO lights must be OFF. During night time operation NAV&LOGO lights must be ON.

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14
Q

Quando se pede o Before Start to the line?

A

Load conferida
FMS page - Select
Tira a externa —> Before Start CL to the line

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15
Q

BEFORE START CHECKLIST
XXX
BARO REF……………………….______ SET
“Bellow the line”

A

Speeche

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16
Q

Feito o speeche….

A

Azultec: Cheque de segurança efetuado e trator engatado?
Solicita o push
CM2: ATC AUTO
CM1:
EXTERIOR LIGHTS………………………..BEACON E NAV
THRUST LEVERS………………………….IDLE
ACCU PRESS…………………………… CHECK
NW STRG DISC ……………………… CHECK AS RQRD
PARK BRK ………………………………. AS RQRD
BEFORE START C/L below the line………… COMPLETE

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17
Q

Sequência de parâmetros do acionamento dos motores.

A

N2 increases
Corresponding start valve is in line.
Bleed pressure indication is green.
Oil pressure increases.

At 25 % N3:
- Indication of the active igniter (A or B) .
‐ FF increases

30 s (maximum) after fuel is on:
‐ EGT increases (Limitation 700 graus no solo e 850 em voo)
‐ N1 increases

At 50 % N3
Start valve starts closing. (It is fully closed after about 10 s.) Igniter is turned OFF.

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18
Q

Engine idle parameters after Start?

A 
At ISA sea level : 
EPR about 1.015
N1 about 22.6 %
N2 about 47 %
N3 about 63 %
EGT about 380 °C,
FF about 820 kg/h (1 800 lb/h)
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19
Q

After landing

A

CM1:
GRND SPLRS……………………. DISARM

CM2
EXTERIOR LIGHTS…………… SET (AD)*
ldg lights off, ao livrar: Nose Taxi e Strobe Auto
APU MASTER pb-sw …………ON (AD) + Time
RADAR………………………………..OFF
PREDICTIVE WINDSHEAR…OFF
ENG START selector…………. NORM
FLAPS………………………………….RETRACT / CONF 1 (AD)
TCAS …………………………………. STBY
ATC ……………………………………AUTO (AD)
CLOCK……………………………….CHR START (APU START) (AD)
CLOCK……………………………….ELAPSED TIME RESET (AD)
APU …………………………………..START / 2 MIN (AD)
ANTI ICE…………………………….AS RQRD
BRAKE TEMP ………………….. CHECK
BRAKE FAN (If Required)…. ON / 5 MIN

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20
Q

After landing brake temperature check

A

BRAKE TEMPERATURE………………………………….. CHECK
‐ Check brake temperature on the WHEEL SD page for discrepancies and high temperature
‐ If brake fans  are installed:
When the turnaround time is short or if the temperature of any brake is likely to exceed 500 °C, use the brake fans without delay. In other cases, the flight crew would delay brake fans selection to 5 min after landing, or approaching the gate, whichever occurs first.

21
Q

Parking CM1

A

ACCU PRESS………………………………… CHECK
PARKING BRAKE handle ………………. ON
ALL ENG MASTERS…………………………. OFF
SEAT BELTS sw ………………………..OFF (AD)
SLIDES ………………………CHECK DISARMED
EXTERIOR LIGHTS…………………………. SET (AD)
GROUND CONTACT………………. ESTABLISH
PARK BRK ………………. AS RQRD
DU’s……………………………………….. DIM
PARKING C/L

22
Q

Parking CM2

A

ANTI-ICE…………………………. OFF
APU BLEED pb-sw ………….ON
FUEL PUMPS…………………….OFF
ATC …………………………………STBY (AD)
IRS PERFORMANCE……….CHECK
FUEL QTY ……………………….CHECK
STATUS…………………………….CHECK
BRAKE FAN  ………………..OFF
DU’s…………………………………DIM
PARKING C/L

23
Q

• CM2 - AT THR RED ALT:

A

PACK 1+2 (if applicable)……………… ON
• Select PACK 1 on, after CLB thrust reduction.
• Select PACK 2 on, at least 10 s after PACK 1 is selected on, for passenger comfort.

24
Q

•AT S SPEED:

FLAPS 0…………………………………..ORDER

A

FLAPS 0……………………………………..SELECT
GND SPLRS…………………………….. DISARM
EXTERIOR LIGHTS………………… SET

25
Q

AFTER TAKE OFF

PM

A

APU BLEED pb-sw…………………………..AS RQRD
APU MASTER SW……………………………AS RQRD
ENG START selector……………………….AS RQRD
TCAS Mode selector………………………TA/RA
ANTI ICE pb-sw……………………………….AS RQRD
AFTER TAKEOFF / CLIMB C/L down to the line

26
Q

FL 100

PM

A

LAND LIGHTS sw …………………….OFF
SEAT BELTS sw ………………………. AS RQRD
NO SMOKING sw ……………………Cycle ON / AUTO 2x (AD)
EFIS option……………………………….AS RQRD
Select CSTR on one side, for grid MORA (if available), and ARPT on the other side.
ECAM MEMO……………………………REVIEW
TERR ON ND…………………………….OFF (AD)
NAVAIDS…………………………………..CLEAR
SEC F-PLN ……………………………….AS RQRD
OPT / MAX ALT ………………………. CHECK
Enroute Chart……………..Avaliable for both Pilots
IN RANGE REPORT ………………. PERFORM (AD)

27
Q

Is it possible to climb above REC MAX FL?

A

The displayed MAX REC FL gives the aircraft at least a 0.3 g buffet margin. The pilot may enter a
cruise flight level above this level into the MCDU and the FMGS will accept it, provided that it does
not exceed the level at which the margin is reduced to 0.2 g.

28
Q

During Climb, when operating within 5 NM and 2.000ft of other aircraft, what is the recomended V/S?

A

reduce the rate of climb to 1000 fpm (feet per minute) to avoid the generation of TAs and RAs.

29
Q

How constraints should be managed with the FCU during climb/descent?

A

All constrains must be set on the FCU altitude window. When ALT is displayed on FMA, select next constrain or assigned flight level.

30
Q

When landing performance permits: the best combination to reduce fuel costs and brake wear is:

A

CONF 3 + REV IDLE + Autobrake LO.

31
Q

If the flight Crew needs to reduce the landing distance, they should change the configuration in the following order:

A

a) Consider Flaps Full;
b) Consider REV MAX;
c) Consider Autobrake MED.

32
Q

Why Autobrake MED in combination with CONF 3 and REV IDLE shouldn’t be use for landing?

A

The use of Autobrake MED in combination with CONF 3 and REV IDLE increases the brake oxidation, which may be severe. When the Flight Crew rides the brakes (and overrides the Autobrake) at landing, the same oxidation phenomenon may occur.

33
Q

Descent preparation PF flow

A

A-CHA-PER-F-ELEV-AUTO
ATIS………………OBTAIN
JEPPESEN CHARTS…………….PREPARE (AD)
LANDING PERFORMANCE…CONFIRM (AD)
FMS …………………………………….. PREPARE (AD)
LDG ELEV…………………………………CHECK
AUTO BRK ………………………………AS RQRD
APPR BRIEFING…………………….. PERFORM

34
Q

FL100 na descida

PF

A

EFIS option pb ………………… CSTR

LS pb …………………………….. AS RQRD

35
Q

FL100 na descida

PM

A

LAND LIGHTS sw …………………. SET
SEAT BELTS sw ……………………. ON (AD)
NO SMOKING sw ………………….Cycle ON / AUTO 2x (AD)
EFIS option pb …………………….. CSTR
LS pb …………………………………….. AS RQRD
TERR ON ND…………………………. ON (AD)
RADIO NAV ……………………………SELECT / IDENT
ENG START selector …………….AS RQRD

36
Q

APPROACH USING LOC G/S GUIDANCE

A

INITIAL / INTERMEDIATE APPROACH:
APPR pb on FCU………………….. PRESS
BOTH AP…………………………….. ENGAGE
G/S CAPTURE…………………….. MONITOR
GO-AROUND ALT………………..SET

37
Q

AIRCRAFT CONFIGURATION FOR APPROACH

•At green dot:

A

FLAPS 1…………………………………..ORDER
FLAPS 1……………………………………SELECT
TCAS ………………………………. TA or TA/RA
CABIN CREW………………………….ADVISE (AD)

38
Q

When to order FLAPS 1?

A

At green dot

39
Q

What means the “F” speed at take off or go around?

A

At takeoff or go-around: F is the minimum recommended speed at which the flaps may be retracted from CONF 3 to CONF 1+F or from CONF 2 to CONF 1+F.

40
Q

What means the “F” speed during approach?

A

Minimum Flap Retraction Speed. F is the target speed, when the aircraft configuration is
CONF 2 or CONF 3.

41
Q

Define S speed during take off.

A

Minimum recommended speed at which the

slats may be retracted from CONF 1+F to CONF 0 or from CONF 1 to CONF 0.

42
Q

Define S speed during approach.

A

Minimum Slat Retraction Speed
S is the target speed, when the aircraft configuration is
CONF 1.

43
Q

What to order when Flaps 2? PM actions?

A

•When FLAPS 2
L/G DOWN………………………….ORDER
AUTO BRAKE……………………..CONFIRM
GRND SPLRS……………………..ARM
EXTERIOR LIGHTS…………….SET

44
Q

When L/G down during approach…

A

FLAPS 3……………………………………………ORDER
ECAM WHEEL PAGE…………………………CHECK

45
Q

•When FLAPS 3 during approach…

PM

A

FLAPS FULL………………… SET
SPEED TARGET……………CHECK OR SET
A/THR ………………………….CHECK SPD or OFF
WING A. ICE (if not Required)……..OFF
SLIDING TABLE  ……………………… STOW
LDG MEMO………………………………….CHECK NO BLUE
CABIN REPORT……………………………RECEIVE
LDG C/L ………………………………………COMPLETE

46
Q

Parameters to announce as PM during final app

A 
Announce any deviation in excess of:
• V/S : sink rate 1 200 ft/min
• IAS : speed target + 10 kt; speed target - 5 kt
• PITCH : 0 ° nose down; 10 ° nose up
• BANK : 7 °
47
Q

APPROACH USING LOC G/S GUIDANCE

•At 350 ft

A

PF:

LAND mode…….CHECK ENGAGED / ANNOUNCE

48
Q

For CATI, CATII and CATIII with DH approach:

Callouts during final approach

A 
•At minimum + 100 ft:
PM: ONE HUNDRED ABOVE...MONITOR OR ANNOUNCE
•At minimum:
PF: CONTINUE or GO-AROUND... ANNOUNCE 
PM: MINIMUM.........MONITOR OR ANNOUNCE
For CATIII with no DH approach:
•At 200 ft RA
If no failures is detected:
PF: CONTINUE.................................. ANNOUNCE

A330-200 Systems (8 decks)

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