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A330 DC > Limitations > Flashcards

Limitations Flashcards

1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

A

Clean……………..–1g to +2.5g

Other config………..0g to +2g

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2
Q

MTOW

A

233000kg

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3
Q

Max landing Weight

A

180000kg

182000kg

187000kg

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4
Q

Maximum taxi weight

A

233900kg

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5
Q

Max Altitude

A

41450’

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6
Q

Maximum demonstrated crosswind: dry (gusts included)

A

40 knots

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7
Q

Maximum crosswind: damp/wet (gusts included)

A

32 knots

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8
Q

Maximum tailwind for takeoff

A

15 knots

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9
Q

Maximum tailwind for landing at or below 11000ft

A

15 knots

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10
Q

The maximum wind for passenger door operation

A

40kt (or 50kt , if the aircraft nose is into the wind)

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11
Q

The maximum wind for FWD and AFT cargo doors operation

A

40kt (or 50kt , if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the downwind side of the aircraft).

The passenger, FWD and AFT cargo doors must be closed before the wind speed exceeds 60kt.

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12
Q

MAXIMUM OPERATING SPEED VMO/MMO

A

M.86/330

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13
Q

Maximum speed with landing gear extended

And

Maximum speed at which the landing gear may be operated (extension and retraction)

A

250kt/0.55

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14
Q

Maximum speed for gravity extension

A

200kt

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15
Q

WINDSHIELD WIPERS

Maximum speed

COCKPIT WINDOW OPEN

Maximum speed

A

230kt

It is not possible to open the cockpit windows, with the packs ON.

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16
Q

RAM AIR INLET

Opens only if differential pressure is lower than

A

1psi

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17
Q

Limitation of APU with HP GROUND UNIT

A

Do not use HP ground unit when APU supplies bleed air to avoid bleed system damage.

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18
Q

Maximum positive differential pressure

A

9.25PSI

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19
Q

Maximum negative differential pressure

A

-1.0 or -0.73PSI

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20
Q

MAX. NORM. CABIN ALT.

A

8000’

Depending of CPC standard, for flights longer than 2.5h, the MAXIMUM NORMAL CABIN ALTITUDE can be limited to 7460ft.

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21
Q

Safety relief valve setting

+/-psi?

A

8.85PSI /-0.26PSI

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22
Q

Minimum height for use of the autopilot on takeoff with SRS mode

A 
100ft AGL 
(An internal FMGES logic prevents the autopilot from engaging during the 5s after liftoff)
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23
Q

AP minimum.

Straight-in non precision approach

A

applicable minimum

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24
Q

AP minimum, ILS approach when CAT2 or CAT3 is not displayed on the FMA

A

160ft AGL

25
Q

Minimum height for use of the autopilot

for all other phases

A

500ft AGL

26
Q

If the Flight Crew performs an automatic approach without autoland, the autopilot must be disengaged no later than

A

80ft RA.

27
Q

MAXIMUM WIND CONDITIONS FOR ILS CAT II OR CAT III
Head
Xwind
Tailwind

A

35
20
10

28
Q

Maximum operating altitude with flaps and/or slats extended

A

20000

29
Q

HYDRAULIC

Normal operating pressure is

A

3000PSI ± 200.

30
Q

The nosewheel steering angle is limited to

A

72° or 65°

31
Q

TAXI WITH DEFLATED TIRES

If one tire is deflated on one or more gears (ie. a maximum of three tires), the speed should be limited to

If two tires are deflated on the same main gear (the other main gear tires not being deflated), speed should be limited to

A

7kts

3kts

32
Q

APU OPERATION AND START LIMIT

A

41450’

33
Q

APU BATTERY START LIMIT (ELEC EMER CONFIG)

A

25000’

34
Q

APU use of BLEED AIR plus ELEC POWER
Altitude limitations

1 pack

Engine in flight start with APU bleed assist

2 packs on APU

A

22500’ one pack

ENG START 20000’

17500’ TWO PACKS

35
Q

THRUST SETTING EGT LIMITS & time limit

A

975°C
5 mins
10 mins eng fail

36
Q

THRUST SETTING / EGT LIMITS

MCT

A

940 unlimited

37
Q

THRUST SETTING / EGT LIMITS

Starting

A

750 on ground

950 inflight

38
Q

FUEL-INNER TANKS (OUTER BALANCED)
Authorized asymmetry

Full (32970kg)

Half (15385kg)

7500kg

A

2900kg

4800kg

7500kg

No limitation below 7500kg

39
Q

FUEL-OUTER TANKS (INNER BALANCED)
Authorized asymmetry

FULL (2865kg)

2400kg

1730kg

A

1480kg

1580kg

1730kg

No limitation below 1730kg for outer tanks

40
Q

FUEL TEMPERATURE

JET A1 minimum

A

-47c

41
Q

MINIMUM FUEL QUANTITY FOR TAKEOFF

A

5200kg

WING TK LO LVL warning must not be displayed on ECAM for takeoff

42
Q

Tanks must be emptied in the following order

A

Center tank, then wing tanks

43
Q

LOAD SHEET FUEL DISTRUBUTION

When must load control be notified?

A

Flight Crew are to continue to notify Load Control of Total Fuel
discrepancies exceeding +- 1000kg and/or Trim Tank discrepancies exceeding +-200kg.

Provided Total Fuel and Trim Tank LMC limits as per FAM 17.1.7.3 A330 LMC are respected

44
Q

A330-200 CENTRE WING TANK (CWT) RESIDUAL FUEL acceptable amount

A

A330-200 CWT residual fuel amounts less than or equal to 750kg are acceptable, provided:
• Performance and structural weight limitations are not exceeded.
• Fuel in the CWT is considered unusable and remaining fuel is assessed sufficient. If useable fuel is insufficient, ensure the fuel quantity is increased to a sufficient amount

45
Q

Severe turbulence speeds

200

300

A
  • 200 series M.8/260 then 240 below FL200

- 300 series M.78/260 then 240 below FL200

46
Q

Max flap speeds for extension

1

2

3

Full

A

240kts

196

186

180

47
Q

Max tyre ground speed

A

204

48
Q

AIR CONDITIONING WITH LP GROUND UNIT limitation?

A

Do not use conditioned air simultaneously from packs and low pressure ground units (to avoid chattering of the non return valves)

49
Q

APU STARTER
Limitation

After 3 consecutive start attempts.

A

After three consecutive start attempts without cooling down, a 60 min cooling interval must be observed before the next start.

50
Q

APU max EGT limitations

A

MaximumEGT……………………….650 °C

Maximum for start……………….1 250 °C

51
Q

Engine oil limits

Max cont temp

Max transient temp

Min start temp

A

Max continuous temperature…………160 °C

Max transient temperature (15min)……175 °C

Minimum starting temperature ……… -40 °C

52
Q

Engine start crank time limitations and cooling requirements?

A
  • Starter max cont operation is 5 min .
  • Between each cycle, wait 30 s per minute of operation for starter cooling.
  • After two consecutive 5 min duty cycles, wait 10 min to allow starter to cool before each subsequent 5 min duty cycle.
53
Q

Engine starter engagement N2 limit?

A

No running engagement of the starter when the N2 is above 30 %.

54
Q

Minimum oil quantity for start

A

Oil quantity is at or above 12 qt + estimated consumption
(average est consumption = 0.56 qt/h).
Engine operation with engine oil consumption above 0.56 and up to 0.87 qt/h

55
Q

A330 Oxygen Dispatch Pressure minimum

A

An aircraft technical log entry is to be made if preflight oxygen pressure is less than 1330 psi

56
Q

Wake turbulence time separation

Heavy following Super

Arrival
Departure full length
Departure from intersection

A

Arrival…………………………………….3 mins
Departure full length………………..2
Departure from intersection……..4

57
Q

Wake turbulence Distance separation

Heavy following Super

Heavy following Heavy

A

6nm

4nm

58
Q

Maximum useable Fuel load

200

300

A

109186kg

76369 or 76561kg

A330 DC (2 decks)

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