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Limits > 330 > Flashcards

330 Flashcards

1
Q

Flight maneuvering load acceleration limit - clean configuration.

A

-1g to +2.5g

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2
Q

Flight maneuvering load acceleration limit - other configurations

A

0g to +2g

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3
Q

Environmental Envelope - Maximum Pressure Altitude

A

41,450 ft

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4
Q

Environmental Envelope - Maximum Elevation for takeoff and Landing

A

12,500 ft

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5
Q

Environmental Envelope - Minimum elevation for TO and LDG

A

-2,000 ft

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6
Q

Runway slope

A

-+2%

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7
Q

Nominal runway width

A

45m

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8
Q

Maximum certified Cross wind for
TO

A

32 kts gust included. An engine limitation

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9
Q

Max demonstrated crosswind for landing

A

40 kts gust included

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10
Q

Max tailwind TO

A

15 kts

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11
Q

Max tailwind LDG

A

15 kts at or Below 11,000 ft
10 kts above 11,000ft

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12
Q

Max wind conditions for ILS CAT II and CAT III

A

Headwind 35 kts
Tailwind 10 kts
Crosswind 20 kts

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13
Q

Cockpit window open Max speed

A

230 kts

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14
Q

Max Flaps/Slats Speed Config 1

A

240 kts

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15
Q

Max Flaps/Slats Speed Config 1+F

A

215 kts

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16
Q

Max Flaps/Slats Speed Config 2 (CONF 1*)

A

205 kts

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17
Q

Max Flaps/Slats Speed Config 2

A

196 kts

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18
Q

Max Flaps/Slats Speed Config 3

A

186 kts

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19
Q

Max Flaps/Slats Speed Config FULL

A

180 kts

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20
Q

Max operating speed VMO/MMO

A

330 kts/Mach 0.86

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21
Q

Max speed with landing gear extended VLE

A

250 kts/0.55 mach

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22
Q

Max speed with landing gear operating - extending

A

250 kts/0.55 mach

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23
Q

Max speed with landing gear gravity extension

A

200 kts

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24
Q

Max tire speed

A

204 kts

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25
Q

Min control speed for LDG (VMCL)

A

126 kts

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26
Q

Wipers Max operating speed

A

230 kts

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27
Q

With pax on board, it is not recommended to exceed this time without air conditioning supply.

A

20 minutes

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28
Q

Cabin pressure - Max positive differential pressure

A

9.25 psi

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29
Q

Cabin pressure - Max negative differential pressure

A

-0.73 psi

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30
Q

Auto pilot can be used with the following minimum values:

A

At takeoff 100 ft AGL and at least 5s after lift off
In approach with FINAL APP, V/S or FPA mode 250 ft AGL
In circling approach 500 ft AGL
ILS approach when CAT I on FMA 160 ft AGL
ILS approach when CAT 2 or CAT 3 (single or dual) on FMA 0 ft AGL if autoland

31
Q

Autoland landing glideslope limitation

A

-2.5 deg to -3.25 deg
Airfied below 9.5

32
Q

Minimum weight for autoland

A

116,000 kgs

33
Q

APU start: after 3 consecutive start attempts, flight crew must wait for how many minutes before a new start attempt.

A

60 minutes

34
Q

Max EGT for APU start

A

1250 deg C

35
Q

Max EGT for APU running

A

650 deg C

36
Q

APU Max N speed

A

107 %

37
Q

APU Operation and Normal Start Envelope - maximum Pressure Altitude

A

41,450 ft

38
Q

APU Operation - electrical power only

A

22,500 ft and above

39
Q

APU Operation - bleed air and electrical power only

A

22,500 ft and below

40
Q

APU Battery restart limit

A

25,000 ft

41
Q

APU ground operation max and min altitude

A

14,600 ft and -1,000 ft

42
Q

Engine Max EGT for TO and GA - all engines operative

A

900 deg C for 5 min includes TOGA, FLEX, DERATE thrust modes

43
Q

Engine Max EGT for TO and GA - one engine inoperative

A

900 deg C for 10 min
includes TOGA, FLEX, DERATE thrust modes

44
Q

Engine Max EGT for TO and GA max MCT

A

850 deg C no time limit

45
Q

Engine Max EGT for starting on ground

A

700 deg C

46
Q

Engine Max EGT for starting in flight

A

850 deg C

47
Q

Shaft Speed Max N1 Low Pressure Rotor Speed (in %)

A

99%
depends on ambient conditions and on the configuration of the engine air bleed.

48
Q

Shaft Speed Max N2

A

103.3%

49
Q

Engine Shaft Speed Max N3

A

100%

50
Q

Max Oil Temperature continuous

A

190 deg C

51
Q

Min Oil Temperature before TO

A

20 deg C

52
Q

Min Oil quantity

A

Above 6 qt + estimated consumption average 0.7 qt/hr but no lower than 15 qt

53
Q

Min Oil pressure

A

25 psi

54
Q

Eng Starter MAX continuous operation

A

5 min

55
Q

Max engine starter operation

A

Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to Zero N3 between each cycle.

No running engagement of the starter when N3 is above 10% on ground or 30% in flight.

56
Q

After one continuous operation, or the three cycles, how long to wait to allow the starter to cool.

A

30 minutes

57
Q

Limitation of Reverse Thrust

A

Selection of Reverse Thrust is prohibited in flight.

Backing the aircraft with Reverse Thrust is not permitted.

Max reverse should not be used below 70 kts.

Idle reverse is permitted down to aircraft stop.

58
Q

FLEX TO limitations

A

not permitted in contaminated runway

TFLEX cannot be:

  • higher than TMAXFLEX, equal to ISA+60 deg C
  • lower than the flat rating temp (TREF)
  • lower than the actual OAT
59
Q

Max operating Altitude with Flaps/Slats extended

A

20,000 ft

60
Q

Max fuel temp

A

Jet A1 +49 deg C

61
Q

Min fuel temperature

A

Jet A1 -47 deg C

62
Q

Max allowed Fuel Imbalance

A

Inner Tanks (Outer Balanced)
Heavier Tk. Max Asymmetry
Full. 2,900 kg
17,000. 4,800 kg
7,500 kg. 7,500 kg

63
Q

Min fuel quantity for TO

A

5,200 kg

ECAM alerts related to fuel low in the wing tanks must not appear for TO

64
Q

Severe Ice accretion

A

Ice accumulation on the airframe reaches 5mm or 0.2in thick or more

65
Q

Rain repellent

A

Use in case of heavy and moderate rain

66
Q

Wipers Max operating speed

A

230 knots

67
Q

Max break temp for TO

A

300 deg C

68
Q

Nosewheel Syeering angle limit

A

72%

69
Q

Taxi speed during a turn with deflated or damaged tire, maximum one tire per gear

A

7 kts

70
Q

Taxi speed during turn with two deflated or damaged tire on the same gear.

A

3 kts

71
Q

Max NWS angle with deflated or damaged tire

A

30 deg

72
Q

APU Max Alt for aircon and pressurization - dual pack operation.

A

17,500 ft

73
Q

APU Max Alt for aircon and pressurization - single pack operation.

A

22,500 ft

74
Q

Use of APU bleed for wing anti-ice.

A

Not permitted

Limits (1 decks)

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