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

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
Cabin RATE display pulsing
Cabin rate > 1800fpm
26
Cabin ALTITUDE display pulsing
Cab Alt between 8800ft and 9550ft
27
Cabin ALTITUDE display Red
Cab Alt > 9550ft
28
Autopilot Engagement for Takeoff
100ft and 5sec
29
Autopilot Engagement for Circling
500ft
30
Autopilot Engagement for FINAL APP, V/S, FPA
250ft
31
Autopilot Engagement for ILS Cat 1 on FMA
160ft
32
Autopilot Engagement for ILS Cat 2 Manual Landing
80ft
33
Autopilot Engagement for ILS Cat2/CAT3 SINGLE or DUAL on FMA
0ft if AUTOLAND
34
Autopilot Engagement after Manual Go-Around
100ft
35
Autopilot Engagement: other situations
500ft
36
ILS Cat II Minimum Decision Height
100ft
37
ILS CAT III Single (FAIL PASSIVE) Limitations
- 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
38
ILS CAT III Dual (FAIL OPERATIONAL) Limitations
- 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
ENGINE OUT CAT II and CAT III autoland Limitations
Approved if: - Procedures completed before 1.000ft. - Only in CONF 3 - Overweight up to 251T NEO and 229T CEO
40
Wind Limitations for for CAT II and CAT III
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
APU Cooldown after 3 consecutive starts
60min
42
APU Maximum rotor speed (N)
107%
43
Maximum EGT for APU start
1250°C
44
Maximum EGT for APU running
650°C
45
APU start and shutdown during refueling
Permitted. - Do not try to start APU after aborted start or automatic shutdown - In case of fuel spillage, shut down APU
46
APU Maximum start altitude
41.450ft
47
APU Max Battery start altitude
25.000ft
48
APU use, electrical power only
41.450ft
49
APU use, electrical + 1 Pack
22.500ft
50
APU use, electrical + 2 Packs
17.500ft
51
APU BLEED use for Engine Start (maximum altitude)
20.000ft
52
Use of APU bleed for Wing Anti Ice
Not permitted
53
ENGINE Maximum EGT and time for takeoff and go-around AEO
NEO 900°C, 5 min CEO 920°C, 20 sec 900°C, 5 min
54
Engine Maximum EGT for takeoff and go-around OEI
900°C, 10 min
55
Engine Maximum Continuous EGT
850°C
56
Engine Max Inflight Start EGT
NEO 900°C CEO 850°C
57
ENGINE Ground Start maximum EGT
700°C
58
Max Engine Rotor Speeds (N1/N2/N3)
NEO N1…101.5% N2…103.5% N3…101.5% CEO N1…99% N2…103.3% N3…100%
59
Engine OIL maximum continuous temperature
NEO 191°C (Transient 15min - 196°C) CEO 190°C
60
Engine OIL minimum temperature for takeoff
NEO Table CEO 50°C
61
Engine OIL minimum pressure
NEO 30 PSI CEO 25 PSI
62
Engine oil minimum quantity
NEO Flight time < 10 hours…15qt ETOPS or flight > 10 hours…16qt CEO 15qt or 6qt + 0.7qt/h
63
Engine starter limits
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
Engine starter pause required between cycles
30 min
65
Engine starter running engagement limit
N3<10% on Ground N3<30% in Flight
66
Thrust reverser limitation for use in normal operations
Avoid Reverse Thrust above IDLE if speed < 70kt
67
Flex takeoff limitation
Not permitted on contaminated runways
68
Derated Takeoff Limitation
- 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
Go-around Soft limitation
Not permitted if OEI
70
Flaps/Slats Maximum extension altitude
20.000ft
71
Maximum fuel temperature
55°C
72
Fuel imbalance limitation
- 3000 Kg difference triggers ADVISORY - View table on limitations chapter - Imbalance may be exceeded without significant effect to aircraft handling
73
Minimum Fuel for Takeoff
5200kg and no FUEL WING TK LO LVL message
74
Definition of icing conditions
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
Severe Icing
5mm or more
76
Thin Hoarfrost
Crystalline deposit, usually uniform In icing conditions, during walk around, thin hoarfrost is acceptable on the upper surface of the fuselage
77
Rain Repellent use
Moderate to heavy rain only
78
Maximum brake temperature for takeoff
300°C (150°C if Brake Fans were used)
79
Landing gear EXTENDED limitation (VLE)
250kt/M.55
80
Landing gear OPERATING - EXTENSION and RETRACTION limitation (VLO)
250kt/M.55
81
Landing gear GRAVITY EXTENSION VLO/VLE
200kt
82
Tires Maximum Ground Speed
204kt
83
Taxi with deflated or damaged tires
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
IR Alignment
On ground only. Between 82deg N and 82deg S
85
Minimum crew oxygen pressure
View table on QRH
86
Passenger Masks automatically drop at what Cabin Altitude?
14.000ft cabin altitude
87
Power supply for PEDs
Must be off for takeoff and Landing
88
Minimum TAT
-53°C
89
Maximum flight path angle during the approach (NEO)
Maximum flight path angle is -4°
90
Maximum Ceiling
41.450ft
91
Autopilot Engagement for F-G/S mode
200ft
92
Principal Dimensions
NEO Length…63.66m Wingspan…64m CEO Length…58.37m Wingspan…60.3m
93
Ground Clearance
NEO PITCH UP ANGLE: 14.0° / 10.0° (ext. / comp.) CEO PITCH UP ANGLE: 16.0° / 11.5° (ext. / comp.)