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A350 Limitations > Limitations > Flashcards

Limitations Flashcards

1
Q

Flight manoeuvring load acceleration limits

Clean =

Other config =

A

Clean = -1g to +2.5g

Other config = 0g to +2.0g

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2
Q

Min TAT

A

-52 degrees

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3
Q

RUNGWAY slope mean

A

+/- 2%

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4
Q

Max tailwind for T.O.

A

15kt

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5
Q

Max tailwind for LDG

A

15kt

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6
Q

Max wind for cabin and cargo door operation

A

40kt

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7
Q

Flap/ slat speeds 350-9

A

0 = VMO/MMO
1 = 255kt
1+F = 220kt
2 = 212kt
3 = 195kt
Full = 186kt

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8
Q

Flap/slat speeds 350-1000

A

0 = VMO/MMO
1 = 260kt
1+F = 231kt
2 = 219kt
3 = 206kt
Full = 192kt

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9
Q

VMO/MMO

A

VMO = 340kt
MMO = 0.89M

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10
Q

LDG gear speeds 350-1000 for

(VLE/MLE) gear extended
(VLO/MLO) gear operating
(VLO/MLO = VLE/MLE) gravity extension

A

250kt/ M0.55 for all

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11
Q

LDG gear speeds 350-900 for

(VLE/MLE) gear extended
(VLO/MLO) gear operating
(VLO/MLO = VLE/MLE) gravity extension

A

(VLE/MLE) + (VLO+MLO) = 250kt / M 0.55

(VLO/MLO) gravity extension = 220kt / M0.48

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12
Q

Max tire speed 350-9

A

204kt

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13
Q

Max tire speed 350-1000

A

213kt

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14
Q

Max wiper speed

A

230kt

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15
Q

Differential cabin pressures + and -

A

+ pressure max = 10.29 psi
- pressure max = -0.71 psi

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16
Q

Ram air inlet differential pressure req

A

Pressure bellow 2 psi

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17
Q

Aoto pilot engagement after T.O.

A

At least 5 seconds after lift off

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18
Q

Autopilot engagement after a Go -Around

A

100ft AGL

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19
Q

Autopilot disconnect height for F-G/S mode, V/S or FPA mode and APP-DES mode

A

200ft AGL

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20
Q

Autopilot disconnect height in G/S mode and APPR1 on FMA

A

160ft AGL

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21
Q

Autopilot disconnect height for G/S mode and one of the following in FMA

-LAND 1
-LAND2
-LAND3 SINGLE
-LAND3 DUAL

A

0ft AGL if an auto land

80ft AGL if manual landing

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22
Q

Max Auto land winds 350-9

Tail. =
Head. =
X wind =

A

Tail = max tailwind for landing
Head = 40kt
X wind = 30kt

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23
Q

Max Auto land winds 350-1000

Tail. =
Head. =
X wind. =

A

Tail = max tail wind for landing
Head = 30kt
X wind = 30kt

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24
Q

Alert height 350

A

200ft

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25
Q

APU start attempts

A

3 consecutive APU start attempts, crew must then wait 60min

26
Q

APU operational

Electric

A

Entire flight envelope

27
Q

APU operational

APU bleed Eng start

A

25,000 ft

28
Q

APU operational

APU bleed AC + press (single pack)

A

25,000ft

29
Q

APU operational

APU bleed AC + press (dual pack)

A

22,500ft

30
Q

APU operational

APU bleed for wing anti ice

A

Not permitted

31
Q

Eng oil quantity 350-1000

⬇️5hr flight =
⬆️5hr ⬇️7hr flight =
⬆️7hr flight =

A

Eng oil quantity 350-1000

⬇️5hr flight. = 13 qts
⬆️5hr ⬇️7hr flight = 15 qts
⬆️7hr flight = Full tank

Oil tank considered full when ENG SD page says22 qts or tech log says fully filled

32
Q

Eng oil quantity 350-900

Min oil quantity =

A

Min oil quantity = 13 qts

33
Q

Engine starter limitations

  • max continues operation
  • Two consecutive cycles of ….min + one additional cycle of ….. min with wait of ….s between each cycle
A
  • Max continues = one 5min cycle
  • 3 min x 2 + 1min, 30s between each cycle
34
Q

Engine starter cool down period

A

Wait 30 min after last cycle

35
Q

ENG warm up period

If engines shut down 90mins or less

A

= 2 min warm up

36
Q

ENG warm up period

If engines shut down more than 90mins

A

= 5 mins warm up

37
Q

Max alt for Flaps/slats extended

A

= 20,000ft

38
Q

Max allowed fuel imbalance between left and right tanks

A

= 3,000 kg

39
Q

Max BRK TEMP for T.O.

A

= 300 deg/c

40
Q

Taxi with deflated or damaged tires

Max taxi speed =
Max nosewheel steering andle =
N.o. Affected for nose LDG gear =
N.o. Affected for each main landing gear

A

= 3 kt
= 30 deg
= no more than one affected
= mo more than two affected tires on each LDG gear, provided tires not on the same axle.

41
Q

Back up steering function must not be used in what cases

  • ## -
A
  • On contaminated rays
  • For more than 90* turns
  • To perform more than 2 turns
42
Q

350-9 A7 ALA SIM WV001

Maximum taxi weight =

A

= 275,900 kg

43
Q

350-9 A7 ALA SIM WV001

MTOW =

A

= 275,000 kg

44
Q

350-9 A7 ALA SIM WV001

MLW =

A

= 207,000 kg

45
Q

350-9 A7 ALA SIM WV001

MZFW =

A

= 195,700 kg

46
Q

350-9 A7 ALA SIM WV001

Min T.O. weight =

A

= 144,000 kg

47
Q

350-9 A7 ALA SIM WV001

Min weight for LDG + FLT =

A

= 127,000 kg

48
Q

Wing span

A

64.75M (65m)

49
Q

Ac length

350-9 =

350-1000 =

A

350-9 = 66.61M (67M)

350-1000 = 73.59M (74M)

50
Q

LDG gear width/span

350-9
350-1000

A

350-9 = 10.6M (11M)

350-1000 = 10.73m (11M)

5.5M from centre of AC

51
Q

GRND Clearance Angle 350-9

Compressed gear =

Extended gear =

A

Compressed = 10.1 deg

Extended = 12.4 deg

52
Q

GRND Clearance Angle 350-1000

Compressed gear =

Extended gear =

A

Compressed = 8.6 deg

Extended = 10.7 deg

53
Q

180 deg turn on RWY 350-9

A

= 53M

Additional width may be req when RWY wet or contaminated

54
Q

180 deg turn on RWY 350-1000

A

= 59M

Additional width may be req when RWY wet or contaminated

55
Q

Automatic flap retraction (ARS) A350-900

A

210 KT

56
Q

Automatic flap retraction (ARS) A350-1000

A

221 KT

57
Q

Automatic extension system (AEA) A350-900

A

203 Kt

58
Q

Automatic extension system (AEA) A350-1000

A

214 Kt

59
Q

Flap load relief system (FLRS)

Retracts at =

Extends back at =

A

VFE + 2.5kt

VFE - 2.5kt

60
Q

Slat Alpha/Speed lock function
Activation

AOA above =
Speed less than =

A

= 10.6 deg

= less than 140 kt

61
Q

Slat Alpha/Speed lock function

Deactivation requires
AOA below =
Speed above =

A

AOA = 10.3 deg

Speed above = 146 KT

A350 Limitations (2 decks)

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