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Airbus > Limitations > Flashcards

Limitations Flashcards

1
Q

Flight maneuvering load acceleration limits
Clean configuration
Slats & flaps extended
Slats extended & flaps retracted

A

-1g to +2.5g

0g to 2g

0g to 2g

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2
Q

Center of gravity limits
A319 reference chord line
A320 reference chord line

A

13.76 ft / 48.26 ft aft of nose
13.76 ft / 53.51 ft aft of nose

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3
Q

Weight limits A319
Max taxi wt
Max t/o wt
Max ldg wt
Max zfw
Min wt

A

70,400 kg
70,000 kg
61,000 kg
57,000 kg
35,400 kg

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4
Q

Weight limits A320
Max taxi wt
Max t/o wt
Max ldg wt
Max zfw
Min wt

A

77,400 kg / 73,900 kg
77,000 kg / 73,500 kg
66,000 kg
62,500 kg
37,230 kg

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5
Q

Max flt level

A

39,800 ft

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6
Q

Airpot operations limits
Rwy altitude
Nominal rwy width
Max x-wind
Max tailwind

A

9,200 ft
45 m
38 kt
15 kt

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7
Q

Pax cargo door limits

Max wind for pax door operation
Max wind for cargo door operation

A

65 kt

40 kt (50 kt if a/c nose into the wind or cargo door is on leeward side)

note: cargo door must be closed before wind speed exceeds 65 kt

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8
Q

T/o is NOT permitted on what rwy conditions?

A

Wet ice
Water on top of compacted snow
Dry snow or wet snow over ice

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9
Q

Max operating speeds

VMO / MMO

A

350 kt / 0.82 M

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10
Q

Max flaps / slats speeds

Max speed config 1
Slats position
Flaps position

A

230 kt
18 deg
0 deg

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11
Q

Max flaps / slats speeds

Max speed config 1+f
Slats position
Flaps position

A

215 kt
18 deg
10 deg

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12
Q

Max flaps / slats speed

Max speed config 2
Slats position
Flaps position

A

200 kt
22 deg
15 deg

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13
Q

Max flaps / slats speed

Max speed config 3
Slats position
Flaps position

A

185 kt
22 deg
20 deg

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14
Q

Max flaps / slats speed

Max speed config full
Slats position
Flaps position

A

177 kt
27 deg
35 deg A320 / 40 deg A319

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15
Q

Max speed with ldg gear extended (VLE)

A

280 kt / M 0.67

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16
Q

Max speed which ldg gear may be extended (VLO extension)

A

250 kt / M 0.60

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17
Q

Max speed which ldg gear may be retracted (VLO retracted)

A

220 kt / M 0.54

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18
Q

Max tire ground speed

A

195 kt

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19
Q

Max speed for use of windshield wipers

A

230 kt

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20
Q

Max speed for cockpit window open

A

200 kt

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21
Q

When taxi wt is higher than 76,000 kg what is the max speed during a turn?

A

Do not exceed 20 kt

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22
Q

Only open if differential pressure is lower than how many psi?

A

1psi

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23
Q

Airflow supplied by ground cart shall not exceed how many psi?

A

1.2 kg/s

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24
Q

Max positive differential pressure

A

9 psi

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25
Q

Max negative differential pressure

A

-1 psi

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26
Q

What is the max safety relief valve setting?

A

8.6 psi

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27
Q

Max cabin alt selecion?

A

14,000 ft

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28
Q

Min cabin alt selecion

A

-2000 ft

29
Q

Max delta pressure & safety valve tolerance

A

+/- 7 hpa or 0.1 psi

30
Q

Max Avionics ventilation
OAT = 49 deg C

A

No limit

31
Q

Max avionics ventilation
OAT = 55 deg C

A

2 hrs

32
Q

Max avionics ventilation
OAT = 60 deg C

A

1 hrs

33
Q

Max avionics ventilation
OAT = 64 deg C

A

1/2 hr

34
Q

Min height for use of AP on t/o with SRS

A

100 ft AGL / more than 5 sec after lift off

35
Q

Min height for use of AP in straight in NPA

A

Acceptable minimum

36
Q

Min height for use of AP in circling approach

A

Circling minimum -100ft

37
Q

Min height for use of AP in LLS app when CAT 2 or CAT 3 not displayed

A

160 ft agl

38
Q

Min height for use of AP in PAR (precision app radar)

A

250 ft

39
Q

Min height for use of AP in GO AROUND

A

100 ft agl

40
Q

Min height for use of AP in all other phases

A

500 ft agl

41
Q

CAT II / CAT III

Max headwind
Max tailwind
Max crosswind

A

30 kt
10 kt
15 kt

42
Q

Max continuous load per generator

A

100% (90 kva)

43
Q

Max continuous load per TR

A

200A

44
Q

Max operating altitude with flaps and slats extended

A

20,000 ft

45
Q

Fuel imbalance at t/o

Outer tanks (with inner tanks balanced)

A

370 kg

46
Q

Min temp for fuel jet A

A

-36 deg C

47
Q

Max temp for fuel jet A

A

54 deg C

48
Q

Min fuel qty for t/o

A

1500 kg

49
Q

Hydraulics normal operating pressure

A

3000 psi +/-200

50
Q

Max brake temp for t/o (brake fans off)

A

300 deg C

51
Q

Max nose wheel angle

A

75 deg

52
Q

Max NW angle for towing & pushback

A

95 deg

53
Q

Max NW angle for towbarless towing

A

85 deg

54
Q

Oxygen ref temp formula on ground
Oxygen ref temp formula in flt

A

Ref temp = OAT + cockpit temp / 2
Ref temp = CAB temp - 10 deg C

55
Q

Oxygen supply (normal - diluted)

A

13 minutes

56
Q

Oxygen 100% at cabin 8000 ft

A

15 minutes

57
Q

Oxygen during CRZ at fl 100 (normal - diluted)

A

107 minutes

58
Q

Max APU Starter

A

3 cycles then wait 60 minutes before attempting 3 more cycles

59
Q

APU max N rotor speed

A

107%

60
Q

Max use for TOGA thrust and EGT
AEO
OEI

A

5 minutes AEO
10 minutes OEI

EGT limit 950 deg C

61
Q

MCT thrust EGT limit

A

915 deg C

62
Q

Power plant oil min temp for starting

A

-40 deg C

63
Q

Power plant oil min temp for t/o

A

-10 deg C

64
Q

Power plant min oil qty

A

9.5 qtz

65
Q

Power plant max N1

A

104%

66
Q

Power plant max N2

A

105 %

67
Q

Power plant max start cycle?
Start duration?
Pause?
Cooling period?

A

4 cycles 2 minutes each cycle
20 sec pause
15 minutes cooling period

68
Q

Max Inner tanks imbalance at T/O (outer tanks banlanced)

A

Heavier tank qty Max allowed imbalance
Full 500 kg
3000 kg 1050 kg
1450 kg 1450 kg

69
Q

Max Inner tanks imbalance in FLT & at LDG (outer tanks balanced)

A

Heavier tank Max allowed imbalance
Full 1500 kg
4300 kg 1600 kg
2250 kg 2250 kg

Airbus (1 decks)

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