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Airbus > Limitations > Flashcards

Limitations Flashcards

1
Q

Max landing weights A319

N502-N536

A

137,788 lb

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2
Q

Wingspan standard

A

111 ft 10 in

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3
Q

Wingspan sharklet

A

117 ft 5 in

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4
Q

Max certified altitude

A

39,800 ft

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5
Q

Max APU start battery only

A

FL250

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6
Q

Max APU start normal ac power

A

FL410

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7
Q

Max Landing gear extended altitude

A

FL250

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8
Q

Max flaps and or slats extended altitude

A

FL200

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9
Q

Max runway slope

A

+/- 2%

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10
Q

Max runway altitude

A

9200 ft

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11
Q

Nominal runway width

A

148 ft

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12
Q

Max certified crosswind takeoff neo

A

35 kts

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13
Q

Max crosswind demonstrated crosswind Landing

A

38 Kts

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14
Q

Max tailwind takeoff

A

15 kts

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15
Q

Max tailwind Landing

A

10 kts

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16
Q

Max wind for pax door open

A

65 kts

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17
Q

Max landing gear extended

A

280/ .67

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18
Q

Max landing gear extension

A

250/ .60

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19
Q

Max landing gear retraction

A

220/ .54

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20
Q

Max wiper speed

A

230 kts

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21
Q

A320/321

Max speed durning a turn if over 167,550 lb

A

20kt

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22
Q

Do not use conditioned air simultaneously from packs and LP ground

A

True

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23
Q

Do not use HP ground unit when the APU supplies bleed air to avoid bleed system damage

A

True

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24
Q

A320 618-

Max imbalance takeoff

Mac imbalance flt/ Landing

A

Inner tank full 1102 lbs

Inner tank full. 3306 lbs

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25
Q

A321

Max fuel imbalance flt/ Landing

A

Wing tanks one side full

2910 lbs

26
Q

A321 656-

Max fuel imbalance takeoff

A

Wing one side full

882lbs

27
Q

For jet a only if TAT reaches -34c monitor fuel SD page that fuel temperature remains warmer than -36c

A

True

28
Q

APU

After 3 starter motor cycles

A

Wait 60 min before 3 more cycles

29
Q

Air bleed extraction from the APU for wing A/I is not permitted

A

True

30
Q

APU max bleed extraction with one pack

A

FL 200

31
Q

APU max altitude for bleed extraction with two packs

A

15,000 ft

32
Q

Max brake temp for takeoff

A

300c

33
Q

Autopilot min height for use

Takeoff with SRS mode

A

100 ft agl

34
Q

Min autopilot use for

Straight in NP approach

A

Approach mins

35
Q

Autopilot min use for

Circling approach

A

Approach mins - 100

36
Q

Autopilot min use for

ILS when cat 2/3 not displayed

A

160 ft agl

37
Q

Autopilot min use height for

Go around

A

100 ft agl

38
Q

Autopilot min use height for

All other phases 319-320

A

500 ft agl

39
Q

Min autopilot height for

All other phases 321

A

900 ft agl

40
Q

Use of the AP or FD in OP DES or DES mode is not permitted durning approach mode unless fcu alt

A

500 feet 319/321

900 feet 321

41
Q

Nav mode may be used in the terminal area provided

A

GPS primary is available or

The appropriate RNP is checked or entered on the MCDU and high accuracy is displayed

Or fms navigation is cross checked with raw data

42
Q

Max temps A319/320

TOGA 5 min/ min eng fail

Max continuous

Starting

A

635c 5 min 2 Eng. 10 single

610c

635c

43
Q

Max temps A321

TOGA 5 min/ min eng fail

Max continuous

Starting

A

650c

610c

635c

44
Q

Max temps NEO

TOGA 5 min/ min eng fail

Max continuous

Starting

A

1083c

1043c

1018c

45
Q

Min oil temp for starting

A

-40c

46
Q

Min oil temp prior to exceeding idle

A

-10c

47
Q

Min oil psi NEO

A

65psi

48
Q

Min oil quantity

A

11.0 qts + est. cons. (.30 qt/hr)

49
Q

Min oil quantity NEO

A

14 qts

50
Q

Starter limits

319/320/321

A

Standard cycle equals one attempt

Ground starts need a 15 second pause between cycles

30 minute cooling or 5 min of continuous cranking

Manual start two minute max cycle

Crank max 5 min cycle

No starter 10% on the ground 18% in flight

51
Q

Starter limits NEO

A

3 attempts equals 1 cycle

35 seconds between cycles

A 15 minute cooling period is required or 15 minutes of continuous cranking

No running of the starter when N2 is above 20%

52
Q

Max crosswind durning engine start

A

35 kts

53
Q

Max reverse not to be used below

A

70 kts

54
Q

Reduced thrust takeoffs are not permitted when

A

Contaminated runways or

Known windshear conditions

55
Q

Cabin pressure differential

Max/ min

A

+9 psi

-1 psi

56
Q

If one engine out you cannot use the autopilot to perform npas in the following modes

A

Final App, nav vs, nav/fpa

57
Q

Max Landing weight A320

N601-N653

A

145,505 lb

58
Q

Max Landing weight NEO

N901-N905

A

148,591

59
Q

Max Landing weight A321

N657-687

A

171,519 lb

60
Q

Tail strike 319

A

13.9

61
Q

Tail strike 320 and NEO

A

11.7

62
Q

Tailstrike 321

A

9.7

Airbus (5 decks)

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