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A330 > Limitations > Flashcards

Limitations Flashcards

0
Q

Flight Maneuvering Load Acceleration Limits

Other configurations

A

0 g to +2 g

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1
Q

Flight Maneuvering Load Acceleration Limits

Clean configuration

A

-1 g to +2.5 g

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2
Q

Weight Limitations

Maximum taxi weight (-200/-300)

A

233 900 kg

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3
Q

Weight Limitations

Maximum takeoff weight (-200)
30-03-2014 t/m 25-10-2014

A

PH-AOA t/m PH-AOC: 222.000 kg

PH-AOD t/m PH-AON: 230.000 kg

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4
Q

Weight Limitations

Maximum landing weight (-200)

A

182 000 kg

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5
Q

Weight Limitations

Maximum zero fuel weight (-200)

A

170 000 kg

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6
Q

Weight Limitations

Minimum weight (-200)

A

116 000 kg

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7
Q

Weight Limitations

Maximum takeoff weight (-300)

A

233 000 kg

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8
Q

Weight Limitations

Maximum landing weight (-300)

A

187 000 kg

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9
Q

Weight Limitations

Maximum zero fuel weight (-300)

A

175 000 kg

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10
Q

Weight Limitations

Minimum weight (-300)

A

121 000 kg

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11
Q

Environmental Envelope

Minimum TAT (-200/-300)

A

-53 ‘C

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12
Q

Airport Operations and Wind Limitations

Runway slope (mean)

A

+/-2 %

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13
Q

Airport Operations and Wind Limitations

Runway altitude

A

12 500 ft

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14
Q

Airport Operations and Wind Limitations

Maximum demonstrated crosswind

A

40 kt

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15
Q

Airport Operations and Wind Limitations

Maximum tailwind for takeoff

A

15 kt

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16
Q

Airport Operations and Wind Limitations

Maximum tailwind for landing at or below 11 000 ft

A

15 kt

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17
Q

Airport Operations and Wind Limitations

Maximum tailwind for landing above 11 000 ft

A

10 kt

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18
Q

Airport Operations and Wind Limitations

Maximum wind for passenger door operation

A

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

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19
Q

Airport Operations and Wind Limitations

Maximum wind for cargo door operation

A

40 kt (or 50, if the aircraft nose is oriented into the wind, or the cargo door is on the leeward side)

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20
Q

Airport Operations and Wind Limitations

The passenger/cargo door must be closed before the wind speed exceeds:

A

60 kt.

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21
Q

Airport Operations and Wind Limitations

Maximum Crosswind for Takeoff/Landing (Gust included) - Damp
Wet (3mm or less water)

A

40 kt

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22
Q

Airport Operations and Wind Limitations

Maximum Crosswind for Takeoff/Landing (Gust included) -
3mm or less of slush, dry snow, wet snow;
Frost
Compacted Snow (OAT at or below -15’C)

A

27 kt

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23
Q

Airport Operations and Wind Limitations

Maximum Crosswind for Takeoff/Landing (Gust included) - 
Dry Snow - between 3 mm and 100 mm
Wet Snow - between 3 mm and 30 mm
Compacted Snow (OAT above -15'C)
Slippery when wet
A

20 kt

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24
Q

Airport Operations and Wind Limitations

Maximum Crosswind for Takeoff/Landing (Gust included) -
Water - between 3 mm and 12.7 mm
Slush - between 3 mm and 12.7 mm

A

20 kt

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25
Q

Airport Operations and Wind Limitations

Maximum Crosswind for Takeoff/Landing (Gust included) -
Ice (cold & dry)

A

15 kt

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26
Q

Maximum Operating Speed VMO/MMO

VMO/MMO

A

330 kt / M.86

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27
Q

Minimum Control Speeds

VMCL (-200)

A

118 kt

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28
Q

Minimum Control Speeds

VMCL (-300)

A

123 kt

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29
Q

Gear Down Speeds

Maximum speed with landing gear extended (VLE)

A

250 kt/0.55

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30
Q

Gear Down Speeds

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

A

250 kt/0.55

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31
Q

Gear Down Speeds

Maximum speed for gravity extension (VLE/VLO)

A

200 kt

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32
Q

Gear Down Speeds

Maximum altitude at which the landing gear may be extended

A

21 000 ft

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33
Q

Maximum Tire Speed

Ground speed

A

204 kt

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34
Q

Windshield Wipers In Use

Maximum speed

A

230 kt

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35
Q

Cockpit Window Open

Maximum speed

A

230 kt

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36
Q

Speedbrakes

A

No limitation.

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37
Q

Ram Air Inlet

Opens only if differential pressure is lower than:

A

1 PSI

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38
Q

Cabin Pressure

Maximum positive differential pressure

A

9.25 PSI

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39
Q

Cabin Pressure

Maximum negative differential pressure

A

-0.73 PSI

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40
Q

Cabin Pressure

Safety relief valve setting

A

8.85 PSI / -0.26 PSI

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41
Q

Cabin Pressure

Maximum normal cabin altitude

42
Q

Cabin Pressure

Minimum/Maximum cabin altitude selection

A

-2000 ft / +14000 ft

43
Q

Auto Pilot Function

Minimum weight for use of autoland

A

123 000 kg

44
Q

Cabin Pressure

Outflow valve closure (altitude)

45
Q

Auto Pilot Function

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

A

100 ft AGL

46
Q

Auto Pilot Function

Minimum height for use of the autopilot in:
Straight-in non precision approach

A

Applicable minimum

47
Q

Auto Pilot Function

Minimum height for use of the autopilot in:
Straight-in LNAV/VNAV approach

A

Applicable minimum

48
Q

Auto Pilot Function

Minimum height for use of the autopilot in:
Circling approach

A

Applicable circling minimum -100 ft

49
Q

Auto Pilot Function

Minimum height for use of the autopilot in:
ILS approach when CAT2 or CAT3 is not displayed on the FMA

A

160 ft AGL

50
Q

Auto Pilot Function

Minimum height for use of the autopilot in:
Go-around (AP or FD engagement)

A

100 ft AGL

51
Q

Auto Pilot Function

Minimum height for use of the autopilot in:
All other phases

A

500 ft AGL

52
Q

Use Of Nav And Final App Modes For Non-Precision Approach

NAV, or NAV and FINAL APP mode may be used for:

A

VOR, VOR/DME, NDB, NDB/DME or RNAV (including GPS) approach, but not for ILS, LOC, LOC-BC, LDA or SDF.

53
Q

Use Of Nav And Final App Modes For Non-Precision Approach

FINAL APP mode guidance capability with GPS PRIMARY has been demonstrated down to:

A

MDH/DH (barometric) 250 ft.

54
Q

Category II

Minimum decision height

A

100 ft AGL

55
Q

Category III Fail Passive

Minimum decision height

56
Q

Category III Fail Operational

Alert height
Minimum RVR

A

200 ft

75 m

57
Q

Maximum Wind Conditions For CAT II/CAT III Automatic Approach, or Automatic Landing and Automatic Rollout

Headwind
Tailwind
Crosswind

A

35 kt
10 kt
20 kt

58
Q

Engine Out

CAT II and CAT III fail passive autoland are only approved:

A

In Configuration 3;

If engine out procedures are completed before reaching 1000 ft in approach.

59
Q

Threshold Crossing Height

Minimum threshold crossing height (TCH)

A

38 ft

If the TCH is below the minimum TCH, the ILS glideslope is too low to give sufficient main gear clearance at the runway threshold. It is allowed to fly the ILS, however at 200 ft HAT a gentle transition must be made from the ILS glideslope to a visual glideslope.

60
Q

Automatic Landing

Depending on the situation (e.g. emergency or other) and provided that the runway is approved for automatic landing, the flight crew can decide to perform an autoland up to:

A

229 000 kg

61
Q

Electronic Outlets

It is forbidden to use the electronic outlets during

A

Takeoff and landing

62
Q

In Seat Power Supply System (ISPSS)

Maximum outlet load (except for momentary exceedance)

63
Q

In Seat Power Supply System (ISPSS)

Maximum momentary outlet current

64
Q

Flaps And Slats

Maximum operating altitude with flaps and/or slats extended

66
Q

Maximum Allowed Wing Fuel Imbalance

Maximum allowed wing fuel imbalance in inner tanks at takeoff, landing and in flight (outer balanced)?

A

Tank content (heavier tank) - Authorized asymmetry

FULL - 2900 kg
17000 kg - 4800 kg
7500 kg - 7500 kg

66
Q

Fuel Temperature

Maximum fuel temperature JET A, JET A1, JP 5, JP 8, N3 JET, RT, and TS-1

67
Q

Maximum Allowed Wing Fuel Imbalance

Maximum allowed wing fuel imbalance in outer tanks at takeoff, landing and in flight (inner balanced)?

A

Tank content (heavier tank) - Authorized asymmetry

FULL - 1480 kg
2400 kg - 1580 kg
1730 kg - 1730 kg

68
Q

Fuel Temperature

Maximum fuel temperature JP 4, JET B

69
Q

Fuel Temperature

Fuel freezing point JET A

70
Q

Fuel Temperature

Fuel freezing point JET A1

71
Q

Fuel Management

In case of a trim tank forward transfer pump failure, do not select the trim tank forward when the pitch attitude is above … to avoid inadvertent fuel aft transfer.

72
Q

Minimum Fuel Quantity For Takeoff

A

5200 kg;

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

73
Q

Fuel Mixability

If a freeze point measurement is not possible, how do we determine the fuel freezing point of a mixture of fuels?

A

Assuming that fuel type A has a higher freezing point than fuel type B:

  • If the mixture of fuel type A and type B contains less than 10% of fuel type A, the freezing point of the mixture can be considered as that of fuel type B.
  • If the mixture of fuel type A and type B contains more than 10% of fuel type A, the freezing point of the mixture can be considered as that of fuel type A.
74
Q

Hydraulic

Normal operating pressure

A

3000 PSI +/-200

75
Q

Brakes

Maximum brake temperature for takeoff

76
Q

Nosewheel Steering (NWS)

Nosewheel steering angle limit

A

72 degrees

77
Q

Nosewheel Steering (NWS)

Nosewheel steering angle limit for towing and pushback

A

65 degrees (markings on the nose landing gear door)

78
Q

Inertial Reference System

The ground alignment of the IRS has been demonstrated to be acceptable between …

A

82’N and 82’S.

79
Q

Inertial Reference System

If all ADIRUs have the same magnetic variation table; in MAGNETIC reference, flight using the NAV mode are prohibited:

A
  • North of 73’N between 90’W and 120’W;
  • North of 82’N;
  • South of 60’S.

(When flying at latitudes beyond these limits, TRUE reference must be selected)

80
Q

Enhanced Ground Proximity Warning System (EGPWS)

The EGPWS enhanced functions should be inhibited when (TERR push button OFF, on the GPWS panel) when the aircraft is less than 15 nm from the airfield:

A
  • For operations to/from runways not incorporated in the EGPWS database;
  • For specific approach procedures, which have been previously been identified as potentially producing false terrain alerts.
81
Q

Cockpit Fixed Oxygen System

Minimum flight crew oxygen must be checked when below …

82
Q

APU - General

Maximum EGT
Maximum EGT for start

A

650’C

1250’C

83
Q

APU - General

Maximum N (rotor speed)

84
Q

APU - general

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

85
Q

APU - General

The APU may be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed. Maintenance action is required within next … Of APU operation.

86
Q

APU - Envelope

APU operation and start limit (FL)

A

41 450 ft (entire envelope)

87
Q

APU - Envelope

APU battery start limit (ELEC EMER CONFIG) (FL)

88
Q

APU - Envelope

Ground starting and operation limit (FL)

89
Q

APU - Envelope

Bleed air & elec power

A

-1 000 ft to 22 500 ft

90
Q

APU - Envelope

Elec power only

A

22 500 ft to 41 450 ft

91
Q

Power Plant - Thrust Setting / EGT Limits

Takeoff and go-around
Time limit / EGT limit

A

5 or 10 min / 975’C

92
Q

Power Plant - Thrust Setting / EGT Limits

MCT
Time limit / EGT limit

A

Unlimited / 940’C

93
Q

Power Plant - Thrust Setting / EGT Limits

Starting
EGT limit on ground / in flight

A

750’C / 975’C

94
Q

Power Plant - Oil

Maximum continuous temperature

95
Q

Power Plant - Oil

Maximum transient temperature (15 min)

96
Q

Power Plant - Oil

Minimum starting temperature

97
Q

Power Plant - Oil

Minimum oil quantity

A

12 qt + estimated consumption (average estimated consumption = 0,56 qt/h)

98
Q

Power Plant - Oil

Minimum oil pressure

99
Q

Power Plant - RPM

N1 max

A

115.5 %

Note: the N1 limit depends upon ambient conditions and engine air bleed configuration. These may limit the N1 to a value lower than that given above.

100
Q

Power Plant - RPM

N2 max

101
Q

Power Plant - Starter

Starter limitations

A
  • Starter maximum continuous operation is 5 min;
  • Between each cycle, wait 30 s per minute of operation for stater cooling;
  • After two consecutive 5 min duty cycles, wait 10 min to allow starter to cool before each subsequent 5 min duty cycle;
  • No running engagement of the starter when the N2 is above 30%.
102
Q

Power Plant - Reduced Thrust Takeoff

T MAX FLEX (-200)
T MAX FLEX (-300)

A

ISA+43’C

ISA+72’C

A330 (3 decks)

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