A320 Limitations Flashcards

(64 cards)

1
Q

Max altitude

A

39,800’

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2
Q

Max taxi weight

A

77,400kg

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3
Q

Max take off weight

A

77,000kg

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4
Q

Max zero fuel weight

A

61,000 kg

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5
Q

Max landing weight

A

64,500 kg

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6
Q

Turning circle

A

22.8 m

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7
Q

Maximun runway altitude

A

9,200’

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8
Q

Normal runway width
Nominal
Minimal

A

45m

30m

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9
Q

Max demonstrated Xwind

A

38 kts

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10
Q

Max tailwind for takeoff

A

10 kts

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11
Q

Max tailwind for landing

A

10 kts

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12
Q

Max wind for Pax door operation

A

65 kts

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13
Q

Max wind for cargo door operation
if into wind or leeward
must be closed by

A

40 kts
50 kts
65 kts

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14
Q

Max Xwind for Damp GOOD
GOOD TO MEDIUM
MEDIUM
MEDIUM TO POOR
POOR

A
38 KTS
29 KTS
25 KTS
20 KTS
15 KTS
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15
Q

Max speed cockpit window open

A

200 kts

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16
Q
Max flap extension speeds
                             0
                             1
                             1 + F
                             2
                             3
                            Full
                            Max altitude
A
Vmo Mmo
230 kts
215 kts
200 kts
185 kts
177 kts
20,000'
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17
Q

Max operating speed Vmo

Mmo

A

350 kts

M 0.82

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18
Q

Max speed with the landing gear extended (VLE)

A

280 kt /M 0.67

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19
Q

Max speed at which the landing gear may be extended (VLO extension)

A

250 kt /M 0.60

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20
Q

Max speed at which the landing gear may be retracted (VLO retraction)

A

220 kt /M 0.54

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21
Q

Max tyre speed on ground

A

195 kts

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22
Q

Max Taxi speed

A

above 76t max 20 kts during turn

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23
Q

Max wiper speed

A

230 kts

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24
Q

Avionics ventilation on ground

49 °C < OAT ≤ 55 °C

A

2 hours

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25
Cabin pressure Max positive diff Max negative diff Safety relief valve setting
9. 0 psi - 1.0 psi 8. 6 psi
26
Auto pilot use height | Take-off
100 ft AGL and at least 5 s after liftoff
27
Auto pilot use height | In approach with F-G/S  mode
200 ft AGL
28
Auto pilot use height | In approach with FINAL APP, V/S or FPA mode
250 ft AGL
29
Auto pilot use height | In circling approach
500 ft AGL for aircraft category C
30
Auto pilot use height | ILS/MLS approach when CAT1 is on the FMA
160 ft AGL
31
Auto pilot use height | GLS  approach when AUTOLAND is not displayed on the FMA
160 ft AGL
32
Auto pilot use height | ILS/MLS  approach when CAT2 or CAT3 (single or dual) is displayed on the FMA
0 ft AGL if autoland
33
``` Auto pilot use height PAR approach (Precision Approach Radar) ```
250 ft AGL
34
Auto pilot use height | After a manual go-around
100 ft AGL
35
Auto pilot use height | In all other phases
500 ft AGL
36
Max wind for ILS/MLS CAT II OR CAT III and for GLS CAT I
Headwind : 30 kt Crosswind : 20 kt Tailwind : 10 kt
37
APU number of start attempts rest period after
3 start attempts 60 min wait period
38
APU | Max altitude to assist engine start
20 000 ft
39
APU | Max altitude for air conditioning and pressurization (single pack operation)
22,500’
40
APU | Max altitude for air conditioning and pressurization (dual pack operation)
15 000 ft
41
APU | Use of APU bleed air for wing anti-ice
not permitted
42
ENGINES Thrust setting Take-off and go-around all engines time ____ EGT____ one engine inop time ____ EGT____
5 min 635 °C | 10 min 635 °C
43
ENGINES Thrust setting | MCT time ____ EGT____
no time limit 610 °C
44
ENGINES Starting EGT limit | inflight/onground
635 °C
45
ENGINES | Minimum oil pressure
60 PSI
46
ENGINES starter limits Pause between starts (man & auto) Pause after __ attempts or __ min cycle time
15 seconds | 3 attempts or 5 min cycle, pause 30 minutes
47
ENGINES reduced thrust take-off | highest TMAXFLEX = ISA + ______
ISA + 55 | Lower than the actual OAT
48
ENGINES | Xwind limit for start
35 kt
49
``` FUEL Max imbalance at TAKE-OFF Inner tanks, (outer balanced) fuel quantity FULL fuel quantity 3000kg fuel quantity 1450 kg ```
500 kg 1 050 kg 1 450 kg
50
FUEL Max imbalance at TAKE-OFF Outer tanks, (inner balanced) Max assymetry
370 kg
51
``` FUEL Max imbalance IN FLIGHT AND AT LANDING inner tanks, (outer balanced) fuel quantity FULL fuel quantity 4300kg fuel quantity 2250 kg ```
1500 kg 1600 kg 2250 kg
52
FUEL Max imbalance at take-off outer tanks
690 kg
53
FUEL | Minimum fuel quantity for takeoff
1500 kg | or No ECAM alert for fuel low level
54
ICING | Definition of icing conditions
OAT (on ground or after takeoff) or the TAT (in flight) is at or below 10 °C and visible moisture, vis less than 1600m surface snow, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes.
55
Rain repellant should only be used _____
Moderate to heavy
56
BRAKE TEMPERATURES | Maximum brake temperature for takeoff (brake fans off)
300 °C
57
Maximum NWS angle
±75°
58
Minimum oil temp for take-off
50 °C
59
Minimum oil pressure
60 Psi
60
Minimum engine oil
11 qt plus 0.3 qt/hr
61
Cabin alt warning
9550’ +/- 350’
62
Manual start maximum cycle time
2 minutes
63
Maximum CRANK cycle time
5 minutes
64
In NAV mode, the IR will not provide valid magnetic heading and magnetic track angle
‐ North of 73 ° North, | and ‐ South of 60 ° South.