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A330 Azul Limitations > Azul A330 Limitations > Flashcards

Azul A330 Limitations Flashcards

1
Q

Load Acceleration Limits

A

Clean -1g to 2.5g
Other 0g to 2g

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2
Q

Runway Slope

A

+-2%

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3
Q

Maximum Runway Altitude

A

NEO
8.000ft

CEO
12.500ft

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4
Q

Runway Width

A

45m

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5
Q

Wind Limitation: Crosswind Takeoff

A

30kt NEO
32kt CEO

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6
Q

Wind Limitation: Crosswind Landing (dry)

A

35kt NEO
40kt CEO

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7
Q

Wind Limitation: Wet or contaminated

A

-See RCAM on FCOM Limitations or Performance (EFB) chapter

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8
Q

Wind Limitation: Tailwind Takeoff

A

NEO 10kt

CEO 15kt

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9
Q

Wind Limitation: Tailwind Landing

A

10kt

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10
Q

Max wind for Passenger Door operation

A

40kt
50kt if nose into the wind,

60 max open

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11
Q

Max wind for Cargo Door operation

A

40kt
50kt if nose into the wind/downwind

60kt max open

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12
Q

Max speed for Cockpit Window Open

A

230kt

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

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13
Q

Max speed for Windshield Wiper operation

A

230kt

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14
Q

Maximum Flaps/Slats Speeds

A

NEO/CEO
Flaps 1…240kt
Flaps 1+F…215kt
Flaps 2…196kt
Flaps 3…186kt
Flaps Full…180kt

NEO
Flaps 2 (Corresponding to CONF 1*)…205kt, (225kt If SLATS Locked at 0)
Flaps 2…210kt If SLATS Locked at 0

CEO
Flaps 2 (Corresponding to CONF 1*)…205kt

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15
Q

VMO/MMO

A

330kt/.86M

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16
Q

Minimum Control Speed for Landing

A

NEO
126kt

CEO
118

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17
Q

A330 Weight Limitations

A

ANV ANW ANX ANY ANZ

  • Taxi…242.900kg
  • Takeoff…242.000kg
  • Landing…191.000kg
  • Zero Fuel…177.000kg to 181.000kg
  • Minimum…127.000kg

AIT AIV AIZ

  • Taxi…230.900kg
  • Takeoff…230.000kg
  • Landing…180.000kg
  • Zero Fuel…168.000kg
  • Minimum…116.000kg

AIU AIW AIX AIY

  • Taxi…233.900kg
  • Takeoff…233.000kg
  • Landing…182.000kg
  • Zero Fuel…170.000kg
  • Minimum…116.000kg
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18
Q

Air Conditioning limitation with PAX onboard

A

Do not exceed 20min without air conditioning

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19
Q

APU bleed + HP Ground Cart use

A

Not permitted

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20
Q

Packs Use With External Air Conditioning Unit

A

Not permitted

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21
Q

Max Differential Cabin Pressure

A

9.25Psi

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22
Q

Maximum Negative Differential Cabin Pressure

A

NEO
-0.73 PSI

CEO
-1.0 PSI

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23
Q

Cabin Pressure Safety Relief Valve Setting

A

8.85 PSI

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24
Q

Maximum Normal Cabin Altitude

A

8000ft cabin altitude
May be limited to 7.460ft for flights > 2.5 h depending on CPC std.

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25
Q

Cabin RATE display pulsing

A

Cabin rate > 1800fpm

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26
Q

Cabin ALTITUDE display pulsing

A

Cab Alt between 8800ft and 9550ft

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27
Q

Cabin ALTITUDE display Red

A

Cab Alt > 9550ft

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28
Q

Autopilot Engagement for Takeoff

A

100ft and 5sec

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29
Q

Autopilot Engagement for Circling

A

500ft

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30
Q

Autopilot Engagement for FINAL APP, V/S, FPA

A

250ft

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31
Q

Autopilot Engagement for ILS Cat 1 on FMA

A

160ft

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32
Q

Autopilot Engagement for ILS Cat 2 Manual Landing

A

80ft

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33
Q

Autopilot Engagement for ILS Cat2/CAT3 SINGLE or DUAL on FMA

A

0ft if AUTOLAND

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34
Q

Autopilot Engagement after Manual Go-Around

A

100ft

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35
Q

Autopilot Engagement: other situations

A

500ft

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36
Q

ILS Cat II Minimum Decision Height

A

100ft

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37
Q

ILS CAT III Single (FAIL PASSIVE) Limitations

A
  • A/THR must be used in selected or managed speed
  • At least one A/P must be engaged in APPR mode, and CAT 3 SINGLE or DUAL must be displayed on FMA
  • Minimum Decision Height…50ft
    -Minimum RVR…175m
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38
Q

ILS CAT III Dual (FAIL OPERATIONAL) Limitations

A
  • A/THR must be used in selected or managed speed
  • Both A/P engaged in APPR, CAT 3 DUAL must be displayed on FMA
  • With DH…min DH 20ft
  • Without DH…min RVR 75m
  • Alert Height…200ft
39
Q

ENGINE OUT CAT II and CAT III autoland Limitations

A

Approved if:
- Procedures completed before 1.000ft.
- Only in CONF 3
- Overweight up to 251T NEO and 229T CEO

40
Q

Wind Limitations for for CAT II and CAT III

A

NEO

  • Tailwind…10kt
  • Crosswind…20kt (10kt OEI)
  • Headwind…25kt (20kt OEI)

CEO

  • Tailwind…10kt
  • Crosswind…20kt
  • Headwind…35kt

FAA EO…15kt crosswind

Limitation based on wind reported by the tower
Automatic Rollout allowed on DRY and WET RWY. Not permitted on contaminated RWY.

41
Q

APU Cooldown after 3 consecutive starts

A

60min

42
Q

APU Maximum rotor speed (N)

A

107%

43
Q

Maximum EGT for APU start

A

1250°C

44
Q

Maximum EGT for APU running

A

650°C

45
Q

APU start and shutdown during refueling

A

Permitted.
- Do not try to start APU after aborted start or automatic shutdown
- In case of fuel spillage, shut down APU

46
Q

APU Maximum start altitude

A

41.450ft

47
Q

APU Max Battery start altitude

A

25.000ft

48
Q

APU use, electrical power only

A

41.450ft

49
Q

APU use, electrical + 1 Pack

A

22.500ft

50
Q

APU use, electrical + 2 Packs

A

17.500ft

51
Q

APU BLEED use for Engine Start (maximum altitude)

A

20.000ft

52
Q

Use of APU bleed for Wing Anti Ice

A

Not permitted

53
Q

ENGINE Maximum EGT and time for takeoff and go-around AEO

A

NEO
900°C, 5 min

CEO
920°C, 20 sec
900°C, 5 min

54
Q

Engine Maximum EGT for takeoff and go-around OEI

A

900°C, 10 min

55
Q

Engine Maximum Continuous EGT

A

850°C

56
Q

Engine Max Inflight Start EGT

A

NEO
900°C

CEO
850°C

57
Q

ENGINE Ground Start maximum EGT

A

700°C

58
Q

Max Engine Rotor Speeds (N1/N2/N3)

A

NEO
N1…101.5%
N2…103.5%
N3…101.5%

CEO
N1…99%
N2…103.3%
N3…100%

59
Q

Engine OIL maximum continuous temperature

A

NEO
191°C (Transient 15min - 196°C)

CEO
190°C

60
Q

Engine OIL minimum temperature for takeoff

A

NEO
Table

CEO
50°C

61
Q

Engine OIL minimum pressure

A

NEO
30 PSI

CEO
25 PSI

62
Q

Engine oil minimum quantity

A

NEO
Flight time < 10 hours…15qt
ETOPS or flight > 10 hours…16qt

CEO
15qt or 6qt + 0.7qt/h

63
Q

Engine starter limits

A

NEO

  • Normal cycle: Two consecutive start attempts of 3 min maximum, plus one additional start attempt of 1 min. Between each start attempt, allow a run down to zero N2 and wait 30 s
  • Extended (Start or Crank) cycle: One continuous operation cycle of 5 min.
  • After…30 min cooldown

CEO

  • Starter maximum continuous operation is 5 min
  • Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to zero N3 between each cycle.
  • After…30 min cooldown
64
Q

Engine starter pause required between cycles

A

30 min

65
Q

Engine starter running engagement limit

A

N3<10% on Ground
N3<30% in Flight

66
Q

Thrust reverser limitation for use in normal operations

A

Avoid Reverse Thrust above IDLE if speed < 70kt

67
Q

Flex takeoff limitation

A

Not permitted on contaminated runways

68
Q

Derated Takeoff Limitation

A
  • Selection of TOGA thrust not permitted when a derated takeoff is performed, except in emergency
  • FLEX takeoff not permitted
  • Permitted in dry, wet or contaminated runways.
69
Q

Go-around Soft limitation

A

Not permitted if OEI

70
Q

Flaps/Slats Maximum extension altitude

A

20.000ft

71
Q

Maximum fuel temperature

A

55°C

72
Q

Fuel imbalance limitation

A
  • 3000 Kg difference triggers ADVISORY
  • View table on limitations chapter
  • Imbalance may be exceeded without significant effect to aircraft handling
73
Q

Minimum Fuel for Takeoff

A

5200kg and no FUEL WING TK LO LVL message

74
Q

Definition of icing conditions

A

OAT (on ground) or TAT (in flight) is at or below 10 C and visible moisture is present (such as clouds, fog with visibility of 1 sm (1600 m) or less, rain, snow, sleet or ice crystals). Also when operating in ramps, taxiways and runways where water, snow, slush may be ingested.
Except in climb and cruise when SAT < -40 C

75
Q

Severe Icing

A

5mm or more

76
Q

Thin Hoarfrost

A

Crystalline deposit, usually uniform

In icing conditions, during walk around, thin hoarfrost is acceptable on the upper surface of the fuselage

77
Q

Rain Repellent use

A

Moderate to heavy rain only

78
Q

Maximum brake temperature for takeoff

A

300°C (150°C if Brake Fans were used)

79
Q

Landing gear EXTENDED limitation (VLE)

A

250kt/M.55

80
Q

Landing gear OPERATING - EXTENSION and RETRACTION limitation (VLO)

A

250kt/M.55

81
Q

Landing gear GRAVITY EXTENSION VLO/VLE

A

200kt

82
Q

Tires Maximum Ground Speed

A

204kt

83
Q

Taxi with deflated or damaged tires

A

If tire damage is suspected, crew must ask for inspection before vacating runway or taxi.

  • One tire per gear (consider 3 gears)…7kt
  • Two tires on same main gear (maximum 1 main gear)…3kt, NWS 30deg
84
Q

IR Alignment

A

On ground only. Between 82deg N and 82deg S

85
Q

Minimum crew oxygen pressure

A

View table on QRH

86
Q

Passenger Masks automatically drop at what Cabin Altitude?

A

14.000ft cabin altitude

87
Q

Power supply for PEDs

A

Must be off for takeoff and Landing

88
Q

Minimum TAT

A

-53°C

89
Q

Maximum flight path angle during the approach (NEO)

A

Maximum flight path angle is -4°

90
Q

Maximum Ceiling

A

41.450ft

91
Q

Autopilot Engagement for F-G/S mode

A

200ft

92
Q

Principal Dimensions

A

NEO
Length…63.66m
Wingspan…64m

CEO
Length…58.37m
Wingspan…60.3m

93
Q

Ground Clearance

A

NEO
PITCH UP ANGLE: 14.0° / 10.0° (ext. / comp.)

CEO
PITCH UP ANGLE: 16.0° / 11.5° (ext. / comp.)

A330 Azul Limitations (1 decks)

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