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A 330 > limitations > Flashcards

limitations Flashcards

1
Q

Max G load (clean)

A

-1G to + 2,5G

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2
Q

Max G load (other than clean)

A

0G to +2G

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3
Q

Minimum TAT

A

-53°C

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4
Q

Runway Slope

A

±2 %

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4
Q

Max runway altitude

A

12 500 ft

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5
Q

Max crosswind for Take-Off

A

32 kts (gust included)

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6
Q

Max demonstrated crosswind for landing standard vs enhanced

A

40 kts/45kts (gust included)

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7
Q

Max wind for doors

A

40kts, 50 kts if aircraft nose into the wind, 60kts doors must be closed

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8
Q

Max speed to open cockpit windows

A

230 kts

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9
Q

Max speed Flaps/Slats

A

-0 : VMO/MMO
-1 : 240kts
-1+F: 215kts
-2: 205kts/196kts Take-Off
-3: 186kts
-Full: 180kts

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10
Q

Max speed landing gear operation (VLO/VLE) normal operation and gravity extension

A

VLE/VLO: 250kts/0.55
Gravity extension: 200kts

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11
Q

Max tire speed

A

195.5kts

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12
Q

Max wipers operating speed

A

230kts

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13
Q

Max cabin pressure (+,- and safety relief valve setting)

A

+9.25psi
-1.0psi
+8.85psi

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14
Q

Autopilot: Take-off

A

100ft AGL and 5 s after liftoff

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15
Q

Autopilot: Approach FINAL APP, V/S OR FPA

A

250ft AGL

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16
Q

Autopilot: Circling approach or any other phases

A

500ft AGL

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17
Q

Autopilot: Approach ILS CAT 1 displayed

A

160ft AGL

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18
Q

Autopilot: Approach ILS CAT 2/3

A

0ft AGL if autoland

19
Q

Autopilot: Go-Around

20
Q

Max Tailwind

21
Q

Max crosswind ILS CAT 2/3

22
Q

Max headwind ILS CAT 2/3

23
Q

Max APU start attemps

A

3 starts then 60 min cool down

24
Q

Max altitude for APU start in flight

25
Q

Max altitude for APU batteries(BAT) start in flight

26
Q

APU bleed in flight

A

Engine start: 20 000ft
Single pack: 22 500ft
Dual pack: 17 500ft
Use of APU bleed air for wing anti-ice is not permitted.

27
Q

Max time at TOGA if ENG fail

28
Q

Minimum Oil Qty

A

15qt or 6qt + 0.7 qt/h
(13h flt)

29
Q

Min Oil temp before Take-Off
Max Oil temp

A

50°C
190°C

30
Q

Starter limitation for ENG

A

Continuous operation: 5 min
3 cycles or 1 continuous cycle = 30 min cool down
No starter engagement if N3 above:
10% on ground
30% in flight

31
Q

Use of reverse thrust

A

Max reverse thrust should not be used below 70kts

32
Q

Max altitude to extend slats

33
Q

Max brake temperature for Take-Off (brake fans off/on)

A

300°C/150°C

34
Q

Highest latitudes for IRS alignments

A

82° N and 82° S

35
Q

Vmcl

A

-300: 126kts
-200: 118kts

36
Q

max EGT APU start

37
Q

EGT take-off/Go-Around

A

20s/920°C
5min(2eng)/10min(1eng)=900°C

38
Q

EGT MCT

A

850°C unlimited

39
Q

EGT Starting

A

on ground: 700°C
in flight: 850°C

40
Q

Max shaft speed

A

N1:99%
N2:103.3%
N3100%

41
Q

Min Oil Pressure

42
Q

Minimum fuel for take-off

A

5200kg
Man-ops: 11 400kg

44
Q

Max N speed APU

A 330 (2 decks)

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