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A320-AD > Limitations > Flashcards

Limitations Flashcards

1
Q

MTOW A320 and A321

A

A320: 77000 kg or 79000 kg
A321: 89000kg (antigo 93500 kg)

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2
Q

Max. Taxi weight A320 and A321

A

A320: 77400 kg or 79400 kg
A321: 89400kg (antigo 93900 kg)

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3
Q

MLW A320

A

A320: 67400 kg

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4
Q

MZFW

A

64300 kg
A321: 75600 kg

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5
Q

Min. Weight

A

40600 kg
A321: 46.600 kg

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6
Q

Rwy Slope

A

+/- 2 %

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7
Q

Max. Rwy Altitude

A

9200 ft / 14100 ft (YY..)

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8
Q

Narrow Rwy (Minimum Rwy)

A

Bellow 45m / min. = 30m - Check add procedures

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9
Q

Max. Tailwind for takeoff

A

15 kt

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10
Q

Max. Tailwind for landing

A

10 kt (15 kt for YY… reg)

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11
Q

Max. Tailwind for Autoland

A

10 kt

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12
Q

Max. X-wind for Takeoff

A

25 kt

As AZUL policy

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13
Q

Max. X-wind for landing

A

38 kt. (Check Matrix)

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14
Q

Max. Wind for pax door operation

A

65 kt

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15
Q

Max. Wind for cargo door operation

A

40 kt or 50 kt if headwind. Must be closed before 65 kt

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16
Q

Max flaps/slats speeds A320

A

A320:
1 = 230 kt
1+F = 215 kt
2 = 200 kt
3 = 185
Full = 177

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17
Q

Eng. in TO/GA limit

A

All eng.= 5 min. EGT 1060 C
OEI = 10 min / 1060 C

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18
Q

Eng in MCT max temperature

A

1025 C

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19
Q

Eng. Starting max temperature

A

On ground = 750 C
In flight = 875 C

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20
Q

VLE

A

280 kt / M0.67

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21
Q

VLO extension

A

250 kt / M0.60

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22
Q

VLO retraction

A

220 kt / M0.54

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23
Q

Max tire speed

A

195 kt

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24
Q

Max. Windshield wipers in use

A

230 kt

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25
Q

Cockpit Window open

A

200 kt

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26
Q

VMO / MMO

A

350 KIAS / M 0.82

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27
Q

Cabin Pressure

A

Max. Positive = 9.0 PSI
Max. Negative = -1 PSI
Safety relief valve = 8.6 PSI

28
Q

Max Operating Altitude

A

39800 ft ( Cab alt < 8000 ft)
W/ Slats/Flaps = 20000 ft

29
Q

Brakes max temp for takeoff

A

300 C w/ brakes fan off

30
Q

Auto Pilot

A

T/O with SRS mode = 100 ft and 5 sec
ILS = 160 ft
Non Precision F-G/S = 200 ft Agl
Non Precison Final App, V/S, FPA = 250 ft AGL
CIRCLING approach =500 ft agl
Go-Around = 100 ft
All Others = 500 ft

31
Q

Eng. Oil Quantity

A

8.9 + 0.45 qt/h (min. 10.6 qt)

32
Q

MLW A321

A

79200 kg

33
Q

MAX Slat and Flap Speeds - A321

A

1 = 243 kt
1+F = 225 kt
2 = 215 kt
3 = 195 kt
FULL = 186 kt

34
Q

Load Acceleration

A

Clean: -1g / +2.5 g
Other: 0g / +2.0 g

35
Q

Enviromental Temperature

A

-40 oC / + 55 oC (sea level)

36
Q

PFC Wet max. altitude for ldg dist. reduction

A

4000ft

37
Q

VMCL

A

116 kt

38
Q

VMCA

A

111 kt (320)
110 kt (321) sea level

39
Q

VMCG

A

109 kt (320 26k)
117 kt (320 29k)
118 kt (321) sea level

40
Q

RNP accuracy

A

En route = 1 NM
Terminal = 0.5 NM
Approach = 0.3 NM
RNP-AR = < 0.3 NM

41
Q

CAT-II or CAT-III Max. Wind A321

A

Headwind = 15 kt
Tailwind = 10 kt
Crosswind = 10 kt

42
Q

CAT-II or CAT-III Max. Wind A320

A

Headwind = 30 kt
Tailwind = 10 kt
Crosswind = 20 kt (15 w/ OEI)

43
Q

Auto-landing Winds

A

Headwind = 30 kt
Tailwind = 10 kt
Crosswind = 15 kt

44
Q

APU Max. N speed

A

107 %

45
Q

APU max. EGT

A

Start = 1090 C
Start above FL350 = 1120 C
Running = 675 C

46
Q

APU Battery Start Limit

A

FL250

47
Q

APU ass. start max. alt.

A

FL200

48
Q

APU DUAL PACK opr.

A

FL150

49
Q

APU Single PACK opr.

A

FL200

50
Q

Eng. Max. Shaft Speeds

A

N1 = 101%
N2 = 116.5 %

51
Q

Oil Temperature

A

Max. cont. = 140 C
Max. transd. (15 kin) = 155 C
Min. for Start = -40 C
Min. for Takeoff = 19 C

52
Q

Oil pressure

A

Min = 17.4 PSI
Max = 145 psi (w/ temp < 50 C)
Max = 130.5 psi (w/ temp > 50 C)

53
Q

Eng. Starter limit

A

1 cycle - 60 sec - 1 cycle - 60 sec - 1 cycle - 15 min.
N 2 max = 63%

54
Q

Flex Temp. limit

A

Max. ISA +55 C
Max. TREF
Min >= OAT

Depending on the acft reg. +50 and +52 also exists

55
Q

Eng. Start max. X-WIND

A

45 kt

56
Q

FLAPs/SLATs max. Alt

A

20,000 ft

57
Q

FUEL imbalance A320

A

Takeoff : inner = 500 kg / outer = 370 kg (Tanks FULL)
IN FLIGHT: inner = 1500 kg / outer = 690 kg

58
Q

FUEL imbalance A321

A

Takeoff = 400 kg (Tanks FULL)
Inflight = 1320 kg

59
Q

Minimum FUEL for Takeoff

A

1500 kg

60
Q

Nose Wheel Steering max. angle

A

+/- 85 degrees

61
Q

Taxi w/ tires deflated

A

One tire deflated = 7 kt
Two tires on the same gear = 3 kt
NWS angle = 30 degrees

62
Q

(LIM) What is the maximum indication difference allowed between the altimeters to proceed with the RNP
AR approach?

A

100 ft at IAF

63
Q

In accordance with Flight Safety Foundation, what are the definitions for abnormal attitudes?

A

Pitch: Above 25 and Below 10 °. Bank: Above 45

64
Q

(LIM) What is the tailwind limit for the SBRJ operation?

A

5 kt

65
Q

During descent for ILS CAT I operation, ATC reports the runway threshold lights are inoperative. Will the A320 be
able to proceed with the approach and landing?

A

During day: no effect.
During night: ILS CAT I is not allowed

ICA 100-16 anexo A

66
Q

What is the vertical limit of tolerable deviation in an RNP AR procedure that, if exceeded, should a go around be
considered?

A

75 ft

A320-AD (3 decks)

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