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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
APU start attempts
3 consecutive APU start attempts, crew must then wait 60min
26
APU operational Electric
Entire flight envelope
27
APU operational APU bleed Eng start
25,000 ft
28
APU operational APU bleed AC + press (single pack)
25,000ft
29
APU operational APU bleed AC + press (dual pack)
22,500ft
30
APU operational APU bleed for wing anti ice
Not permitted
31
Eng oil quantity 350-1000 ⬇️5hr flight = ⬆️5hr ⬇️7hr flight = ⬆️7hr flight =
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
Eng oil quantity 350-900 Min oil quantity =
Min oil quantity = 13 qts
33
Engine starter limitations - max continues operation - Two consecutive cycles of ….min + one additional cycle of ….. min with wait of ….s between each cycle
- Max continues = one 5min cycle - 3 min x 2 + 1min, 30s between each cycle
34
Engine starter cool down period
Wait 30 min after last cycle
35
ENG warm up period If engines shut down 90mins or less
= 2 min warm up
36
ENG warm up period If engines shut down more than 90mins
= 5 mins warm up
37
Max alt for Flaps/slats extended
= 20,000ft
38
Max allowed fuel imbalance between left and right tanks
= 3,000 kg
39
Max BRK TEMP for T.O.
= 300 deg/c
40
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
= 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
Back up steering function must not be used in what cases - - -
- On contaminated rays - For more than 90* turns - To perform more than 2 turns
42
350-9 A7 ALA SIM WV001 Maximum taxi weight =
= 275,900 kg
43
350-9 A7 ALA SIM WV001 MTOW =
= 275,000 kg
44
350-9 A7 ALA SIM WV001 MLW =
= 207,000 kg
45
350-9 A7 ALA SIM WV001 MZFW =
= 195,700 kg
46
350-9 A7 ALA SIM WV001 Min T.O. weight =
= 144,000 kg
47
350-9 A7 ALA SIM WV001 Min weight for LDG + FLT =
= 127,000 kg
48
Wing span
64.75M (65m)
49
Ac length 350-9 = 350-1000 =
350-9 = 66.61M (67M) 350-1000 = 73.59M (74M)
50
LDG gear width/span 350-9 350-1000
350-9 = 10.6M (11M) 350-1000 = 10.73m (11M) 5.5M from centre of AC
51
GRND Clearance Angle 350-9 Compressed gear = Extended gear =
Compressed = 10.1 deg Extended = 12.4 deg
52
GRND Clearance Angle 350-1000 Compressed gear = Extended gear =
Compressed = 8.6 deg Extended = 10.7 deg
53
180 deg turn on RWY 350-9
= 53M Additional width may be req when RWY wet or contaminated
54
180 deg turn on RWY 350-1000
= 59M Additional width may be req when RWY wet or contaminated
55
Automatic flap retraction (ARS) A350-900
210 KT
56
Automatic flap retraction (ARS) A350-1000
221 KT
57
Automatic extension system (AEA) A350-900
203 Kt
58
Automatic extension system (AEA) A350-1000
214 Kt
59
Flap load relief system (FLRS) Retracts at = Extends back at =
VFE + 2.5kt VFE - 2.5kt
60
Slat Alpha/Speed lock function Activation AOA above = Speed less than =
= 10.6 deg = less than 140 kt
61
Slat Alpha/Speed lock function Deactivation requires AOA below = Speed above =
AOA = 10.3 deg Speed above = 146 KT

A350 Limitations (2 decks)

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