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Airbus 330 > Limitations > Flashcards

Limitations Flashcards

1
Q

Kind of operations

A

‐ VFR and IFR ‐
Extended overwater flight ‐
Flight in icing conditions

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2
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

A

Clean configuration –1 g to +2.5 g

Other configurations 0 g to +2 g

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3
Q

WEIGHT LIMITATIONS

A4O-DA, A4O-DC, A4O-DF, A4O-DG

A 
Max taxi weight. 233900kg
Max takeoff weight. 233000kg
Max landing weight. 182000kg
Max zero fuel weight  170000kg
Min weight 116000kg
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4
Q

Weight limitations

A4O-DB, A4O-DD, A4O-DE

A 
Max taxi weight. 233900
Max takeoff weight. 233000kg
Max landing weight. 187000kg
Max zero fuel weight  175000kg
Min weight 121000kg
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5
Q

Weight limitations

A4O-DH, A4O-DI, A4O-DJ

A 
Max taxi weight. 235900
Max takeoff weight. 235000kg
Max landing weight. 187000kg
Max zero fuel weight  173000kg
Min weight 121000kg
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6
Q

Runway slope

A

+-2%

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7
Q

Runway altitude

A

12500ft

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8
Q

Max certified crosswind for takeoff

A

32kt (gust included)

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9
Q

Max tailwind takeoff

A4O-DA, A4O-DB, A4O-DC, A4O-DD, A4O-DE, A4O-DF, A4O-DG

A

10kts

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10
Q

Autopilot minimum engagement height

A

100 ft AGL or 5 s after liftoff.

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11
Q

In approach using F-LOC , F-G/S

A

200ft AGL

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12
Q

Autopilot cat 1

A

160fr AGL

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13
Q

Autopilot GLS

A

160ft AGL

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14
Q

Autopilot after a go around

A

100ft

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15
Q

Maximum wind for auto land cat II and III

A

Headwind: 35 kt Tailwind : 10 kt Crosswind: 20 kt

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16
Q

Auto land glide slope

A

-2.5 ° and -3.25 °

For airfield elevation below 9200ft

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17
Q

Weight limitations autoland

A
  • For weights below maximum landing weight

- For weights above 116 000 kg (255 737 lb)

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18
Q

Nominal Runway Width

A

45 m

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19
Q

Max tailwind takeoff

A4O-DH, A4O-DI, A4O-DJ

A

15kts

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20
Q

Max crosswind for landing

A4O-DA, A4O-DC, A4O-DF, A4O-DG

A

45kts

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21
Q

Max crosswind for landing

A4O-DB, A4O-DD, A4O-DE, A4O-DH, A4O-DI, A4O-DJ

A

40kts

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22
Q

Max tailwind landing

A

10kts

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23
Q

The maximum wind for passenger door operation

A

40 kt or 50 kt if the aircraft nose is into the wind

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24
Q

Takeoff is not recommended on the following runway conditions

A

‐ Wet ice,
‐ Water on top of Compacted Snow,
‐ Dry Snow or Wet Snow over Ice.

25
Q

COCKPIT WINDOW OPEN MAXIMUM SPEED

A

230 kt

26
Q

Max VMO/MMO

A

330kts/ m0.86

27
Q

Maximum speed with landing gear extended (VLE

A

250 kt/0.55

28
Q

Maximum speed with the landing gear operating - extension and retraction (VLO)

A

250 kt/0.55

29
Q

Maximum ground speed tire speed

A

204kts

30
Q

WIPERS MAXIMUM OPERATING SPEED

A

230 kt

31
Q

Maximum positive differential pressure

A

9.25 PSI

32
Q

Maximum negative differential pressure

A

.-0.73 PSI

33
Q

Safety relief valve setting

A

8.85 PSI

34
Q

APU start attempts

A

After three consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt.

35
Q

APU max rotor speed

A

107 %

36
Q

Maximum EGT for APU start

A

1 250 °C

37
Q

Maximum EGT for APU running

A

650 °C

38
Q

APU bleed air and elec power

A

25000ft

39
Q

APU elec power only

A

41450 ft

40
Q

When JET B or JP4 is used, APU operation is limited to

A

25 000 ft

41
Q

Maximum N1
Maximum N2
Maximum N3

A

99 %
103.3 %
100 %

42
Q

OIL TEMPERATURE Maximum continuous temperature

A

190 °C

43
Q

Minimum oil temperature before takeoff

A

20 °C

44
Q

Minimum oil pressure

A

25 PSI

45
Q

STARTER

A

‐ Starter maximum continuous operation is 5 min . ‐ Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to zero N3 between each cycle. ‐ After one continuous operation, or the three cycles wait 30 min to allow the starter to cool. ‐ No running engagement of the starter when the N3 is above 10 % on ground, or 30 % in flight.

46
Q

REVERSE THRUST

A

Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.

47
Q

Maximum operating altitude with slats and/or flaps extended

A

20 000 ft

48
Q

Minimum fuel quantity for takeof

A

5 200 kg

49
Q

Maximum brake temperature for takeoff (brake fans off)

A

300 °C

50
Q

If maximum one tire per gear is deflated (consider three gears) Maximum taxi speed during turn

A

7kts

51
Q

If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed

A

3 kt

52
Q

For the nosewheel steering (NWS) angle Maximum NWS angle

A

30 °

53
Q

APU bleed and elec

A

22500ft

54
Q

APU battery restart limit

A

25000ft

55
Q

APU ground operation

A

14600ft

56
Q

APU normal start

A

41450ft

57
Q

Max fuel temp

A

55 degrees for jet a1

58
Q

Starter

A

‐ Starter maximum continuous operation is 5 min .
‐ Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to zero N3 between each cycle.
‐ After one continuous operation, or the three cycles wait 30 min to allow the starter to cool. ‐ No running engagement of the starter when the N3 is above 10 % on ground, or 30 % in flight.

Airbus 330 (3 decks)

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