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QT A320 > Performance > Flashcards

Performance Flashcards

1
Q 
514. According to airworthiness, what is the maximum number of passager seats on a A
320-200 :
145
180
220
A

180

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2
Q
  1. After TAKE OFF, pilot can engage AP :
    At 30 ft.
    5 seconds after LIFT-OFF.
    At 100 ft and at least 5 seconds after LIFT-OFF.
A

At 100 ft and at least 5 seconds after LIFT-OFF.

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3
Q
  1. What is the maximum speed for the landing gear retraction ?
    250 kt
    220 kt
    280 kt
A

220 kt

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4
Q
  1. In normal operation, what is the maximum speed with landing gear extended ?
    280 kt / M 0.67
    250 kt / M 0.67
    220 kt / M 0.60
A

280 kt / M 0.67

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5
Q
  1. The maximum altitude to extend the speed brakes is :
    FL 250
    No limitation
    FL 200
A

No limitation

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6
Q 
519. Minimum usable altitude for AP during an ILS approach with CAT 1 displayed on FMA
is :
160 ft AGL
MDA
When flare is displayed on FMA
A

160 ft AGL

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7
Q
  1. On A320 the use of AP or FD in OPEN DES or DES MODES is not permitted in
    approach unless the FCU altitude is set at or above :
    No restriction
    1500 ft.
    MDA or 500 ft AGL.
A

MDA or 500 ft AGL.

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8
Q
  1. LFPG 27L - WIND = 180/31 kt.
    TAKE OFF and LANDING are allowed
    TAKE OFF is prohibited
    TAKE OFF is allowed but LANDING is prohibited
A

TAKE OFF and LANDING are allowed

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9
Q
  1. The maximun brake temperature for TAKE-OFF is :
    300°C BRAKE FAN OFF
    250°C BRAKE FAN ON
    150°C BRAKE FAN OFF
A

300°C BRAKE FAN OFF

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10
Q
  1. The pilot can disengage AUTO BRAKES system :
    Only by pressing firmly the brake pedals.
    Only by pushing the armed mode P/B.
    Either by pushing the armed mode P/B or by pressing firmly the brake pedals.
A

Either by pushing the armed mode P/B or by pressing firmly the brake pedals.

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11
Q
  1. During preflight check on a A320-200, external temperature 17°C, cabine temperature
    23°C, 1 observer is expected in cockpit, the minimum crew oxygen bottle pressure has
    to be :
    1425 PSI
    731 PSI
    959 PSI
A

959 PSI

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12
Q
  1. During PREFLIGHT on a A320-200, external temperature 17°C, cabine temperature
    23°C, the flight crew oxygen pressure is 1000 PSI :
    You can accept one jump seat
    You can accept two jump seats
    This is the minimum pressure for PEQ 2
A

You can accept one jump seat

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13
Q 
526. After 3 APU STARTER CYCLES separated by 1 minute COOL DOWN, you have to
wait :
At least 60 minutes
At least 15 minutes
Mechanical check has to be performed
A

At least 60 minutes

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14
Q
  1. APU can be started :
    Up to FL 390
    Up to FL 250
    Only on ground
A

Up to FL 390

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15
Q
  1. The APU START LIMITATION with only batteries is :
    Up to FL 390
    Up to FL 250
    Only on ground
A

Up to FL 250

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16
Q
  1. In case of engine failure during TAKE-OFF, TOGA THRUST can be set for :
    5 minutes
    10 minutes
    Unlimited time
A

10 minutes

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17
Q
  1. If after 4 consecutive engine start cycles of 2 mn, start up is not completed, pilot has to
    wait :
    15 minutes to allow starter cooling before attempting a new start
    20 seconds to allow starter relubrification
    No delay is required
A

15 minutes to allow starter cooling before attempting a new start

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18
Q
  1. REVERSE THRUST can be used :
    To back track the aircraft
    IDLE REVERSE is allowed to stop the aircraft in normal operation
    Maximum REVERSE should not be used below 70 kt except in emergency
A

Maximum REVERSE should not be used below 70 kt except in emergency

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19
Q
  1. FL 190, APU GEN ON, APU AIR BLEED can support :
    1 PACK
    2 PACKS
    APU cannot support AIR CONDITIONNING
A

1 PACK

20
Q
  1. WING ANTI-ICING supplied by APU AIR BLEED is :
    Allowed.
    Not allowed.
    Technically impossible
A

Not allowed.

21
Q
  1. After one unsuccessful APU START UP, a new start can be performed :
    Immediately
    After a 1 minute cooling period
    After a 2 minute cooling period
A

Immediately

22
Q
  1. On contamined runways :
    Reduced TAKE OFF THRUST is allowed
    Reduced TAKE OFF is allowed but FLEX TEMP must be reduced by 4°C
    Reduced TAKE OFF THRUST is not allowed
A

Reduced TAKE OFF THRUST is not allowed

23
Q
  1. When items are affecting performance at take-off (like THRUST REVERSERS
    inoperative), TAKE-OFF with reduced THRUST :
    Is permitted without any restriction
    Is not permitted
    Is permitted on dry runways only
A

Is not permitted

24
Q
  1. During preflight check in winter at MOSCOW, the ECAM ENG OIL T° is - 45°C :
    Start-up is not allowed
    There is no oil temperature limitation for start-up
    Start-up may be performed
A

Start-up is not allowed

25
Q
  1. During DESCENT, flying under IMC conditions, TAT = +5°C :
    Pilot has not to use ENG ANTI ICE
    Pilot has to use ENG ANTI ICE
    Before using ANTI ICE, pilot can wait ice emergence
A

Pilot has to use ENG ANTI ICE

26
Q
  1. Flying FL 390, SAT = - 50°C, entering cirrus clouds :
    ENG ANTI ICE is required
    ENG ANTI ICE is not required
    ENG ANTI ICE is not allowed at FL 390
A

ENG ANTI ICE is not required

27
Q
  1. On ground, A/C is under icing conditions when :
    OAT < 10°C
    OAT < 10°C and visibility less than 1600 m
    Visibility less than 1600 m
A

OAT < 10°C and visibility less than 1600 m

28
Q
  1. On ground, A/C is under icing conditions when :
    OAT < 10°C
    OAT < 10°C and water patches on runway
    OAT < 10°C and ceiling below 200 ft
A

OAT < 10°C and water patches on runway

29
Q
  1. IGN START must be used for TAKE-OFF when :
    Runway is wet
    Heavy rain or severe turbulences are expected
    Icing conditions are encountered
A

Heavy rain or severe turbulences are expected

30
Q
  1. During CLIMB, IMC CONDITIONS, TAT - 30°C :
    ENG ANTI ICE is required
    ENG ANTI ICE is required if SAT < - 40°C
    ENG ANTI ICE is not required if SAT < - 40°C
A

ENG ANTI ICE is not required if SAT < - 40°C

31
Q
  1. Extended flight in icing conditions with the SLATS extended :
    Is permitted because SLATS are deiced
    Is not permitted
    Extended flight in icing conditions should be avoided
A

Extended flight in icing conditions should be avoided

32
Q
  1. In flight, the maximum fuel unbalance is :
    530 kg between inner tanks
    530 kg between both wings
    530 kg between outer tanks
A

530 kg between outer tanks

33
Q
  1. On A320-200, tanks must be emptied as follows :
    Central tanks then wing tanks
    Wing tank then central tanks
    Simultaneously if the fuel load exceeds the wing tanks capacity
A

Simultaneously if the fuel load exceeds the wing tanks capacity

34
Q
  1. The cabin altitude reaches 9550 ft :
    There is no alarm
    There is an EXCESS CABIN ALT alarm and “FASTEN SEAT BELTS” illuminates
    There is only an EXCESS CABIN ALT alarm
A

There is only an EXCESS CABIN ALT alarm

35
Q
  1. Crew want to TAKE-OFF without FD :
    It is permitted with this aircraft
    It is permitted without any restriction
    It is permitted, according to MEL conditions
A

It is permitted, according to MEL conditions

36
Q
  1. When pressing T.O. CONFIG P/B for TAKE-OFF, T.O. CONFIG TEST remains BLUE
    on ECAM TAKE-OFF CHECK LIST.
    Pilot cannot check if TAKE OFF conditions are correct
    There is a technical procedure to check T.O. CONFIG (MEMO ECAM INOP)
    QRH CHECK LIST has to be performed
A

There is a technical procedure to check T.O. CONFIG (MEMO ECAM INOP)

37
Q
  1. An AUTOLAND procedure can be conducted with one engine failure :
    Without any restriction
    If the engine failure procedure is completed before reaching 1000 ft AGL and DH is
    limited to 50 ft
    There is no AUTOLAND procedure allowed with 1 engine out
A

If the engine failure procedure is completed before reaching 1000 ft AGL and DH is
limited to 50 ft

38
Q
  1. When starting the engine in flight :
    EGT MAX is 725° and FADEC controls the overlimit
    EGT MAX is 950° and FADEC does not control the overlimit
    EGT MAX is 725° and FADEC does not control overlimit
A

EGT MAX is 725° and FADEC does not control overlimit

39
Q
  1. A localizer (ILS without G/S) approach can be performed in full MANAGED mode :
    Yes, provided the approach exists in DATA BASE, and is performed with AP
    No, in any case
    Yes, provided the approach exists in DATA BASE and the navigation accuracy is
    HIGH
A

No, in any case

40
Q
  1. When a VOR approach is performed in SELECTED MODE, with AP ON, the AP
    disconnects automatically when reaching MDA minus 50 ft :
    Yes, in any case
    No, and the aircraft automatically levels OFF
    No, and the aircraft continues to descent according to the selected rate of descent
A

No, and the aircraft continues to descent according to the selected rate of descent

41
Q 
554. In descent, with the FMA reading SPD / DES / NAV, if the HDG KNOB on FCU is
pulled, the FMA will turn to :
SPD / DES / HDG
THR IDLE / OPEN DES / HDG
SPD / VS / HDG
A

SPD / VS / HDG

42
Q
  1. Normal electrical power being available, APU may be started up :
    25000 ft or lower
    10000 ft or lower
    Throughout the normal flight envelope
A

Throughout the normal flight envelope

43
Q
  1. The MAX SPEED at which the L/G may be extended is :
    260 kts
    250 kts
    240 kts
A

250 kts

44
Q
  1. The maximum speed to use the windshield wipers is :
    200 kts
    250 kts
    230 kts
A

230 kts

45
Q
  1. What is the MAX TIRE speed ?
    205 kts
    195 kts
    185 kts
A

195 kts

QT A320 (21 decks)

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