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AIRBUS A330 > Limitations > Flashcards

Limitations Flashcards

1
Q

Flight maneuvering load acceleration limits

Clean config

A

-1g to +2.5g

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2
Q

Flight maneuvering load acceleration limits

Other config

A

0g to +2g

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3
Q

Environmental envelope

Max alt

A

41450ft

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4
Q

Environmental envelope

Takeoff and landing altitude

A

-2000 to 8500ft

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5
Q

Environmental envelope

Minimum TAT

A

-53 degC

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6
Q

Airport operations and wind limitations

Runway slope

A

+-2%

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7
Q

Airport operations and wind limitations

Runway altitude

A

8000ft

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8
Q

Airport operations and wind limitations

Nominal runway width

A

45m

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9
Q

Airpprt operations and wind limitations

Maximum certified crosswind for takeoff

A

30kt (gust included)

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10
Q

Airport operations and wind limitations

Maximum certified crosswind for landing

A

35kt (gust included)

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11
Q

Airport operations and wind limitations

Maximum tailwind for takeoff

A

15kt

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12
Q

Airport operations and wind limitations

Maximum tailwind for landing

A

15kt

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13
Q

Airport operations and wind limitations

For landing with tailwind greater than __, FLAPS FULL is recommended

A

10kt

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14
Q

Airport operations and wind limitations

Maximum wind for passenger door operation

A

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

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15
Q

Airport operations and wind limitations

Maximum wind for FWD and AFT cargo doors operation

A

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

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16
Q

Airport operations and wind limitations

Passenger and cargo doors must be closed before the wind speed exceeds __

A

60kt

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17
Q

Runway surface condition: Good

Max crosswind for takeoff

A

30kt

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18
Q

Runway surface condition: Good

Max crosswind for landing

A

35kt

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19
Q

Runway surface condition: Good to Medium

Max crosswind for takeoff and landing

A

27kt

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20
Q

Runway surface condition: Medium

Max crosswind for takeoff and landing

A

20kt

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21
Q

Runway surface condition: Medium to Poor

Max crosswind for takeoff and landing

A

20kt

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22
Q

Runway surface condition: Poor

Max crosswind for takeoff and landing

A

15kt

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23
Q

Airport operations and wind limitations

Max flight path angle during approach

A

-4deg

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24
Q

Cockpit window open maximum speed

A

230kt

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25
Maximum flaps/slats speeds Config 1
240kt
26
Maximum flaps/slats speeds Config 1 + f
215kt
27
Maximum flaps/slats speeds Config 1*
205kt
28
Maximum flaps/slats speeds Config 2
196kt
29
Maximum flaps/slats speeds Config 3
186kt
30
Maximum flaps/slats speeds Config FULL
180kt
31
Vmo
330kt
32
Mmo
0.86 mach
33
Maximum speed with landing gear extended (Vle)
250kt / 0.55
34
Maximum speed with the landing gear operating - extension and retraction (Vlo)
250kt / 0.55
35
Maximum speed for landing gear gravity extension
200kt
36
Maximum tire speed
204kt
37
Minimum control speed for landing (Vmcl)
126kt
38
Vmcg at 0 ft
131kt
39
Vmca at 0 ft, config 1 + f
128kt
40
Vmca at 0 ft, config 2
127kt
41
Vmca at 0 ft, config 3
124kt
42
Wipers maximum operating speed
230kt
43
Maximum taxi weight
242 900 kg
44
Maximum takeoff weight (brake release)
242 000 kg
45
Maximum landing weight
191 000 kg
46
Maximum zero fuel weight
From 177 000 kg to 181 000 kg
47
Maximum zero fuel weight at MTOW 238 000 kg
181 000 kg
48
Maximum zero fuel weight at MTOW 242 000 kg
177 000 kg
49
With passengers on board, it is not recommended to exceed __ without air conditioning supply.
20min
50
Maximum positive differential pressure
9.25psi
51
Maximum negative differential pressure
-0.73psi
52
Safety relief valve setting
8.85psi
53
Max norm cabin alt
8000ft
54
Outflow valve closure (cabin alt)
15000ft
55
AP must not be used in approach and autoland with an aft CG at or above __
35% MAC
56
Autopilot at takeoff
100ft AGL and at least 5 s after liftoff
57
58
Autopilot in approach with F-G/S mode
200ft AGL
59
Autopilot in approach with FINAL APP, V/S, or FPA mode
250ft AGL
60
Autopilot in circling approach
500ft AGL
61
Autopilot in ILS approach when CAT1 is diaplayed on the FMA
160ft AGL
62
Autopilot in ILS approach when CAT2 or CAT3 (single or dual) is displayed on the FMA
0ft AGL if autoland
63
Autopilot after a manual go-around
100ft AGL
64
Autopilot in all other phases
500ft AGL
65
RNP accuracy with GPS PRIMARY With AP ON Enroute, terminal, approach
1nm, 0.5nm, 0.3nm
66
RNP accuracy with GPS PRIMARY With AP OFF and FD ON Enroute, terminal, approach
1nm, 0.51nm, 0.3nm
67
RNP accuracy with GPS PRIMARY With AP OFF and FD OFF Enroute, terminal, approach
1.1nm, 0.51nm, 0.3nm
68
ILS CATEGORY II Minimum decision height
100ft
69
ILS CATEGORY III FAIL PASSIVE (SINGLE) Minimum decision height
50ft
70
ILS CATEGORY III FAIL OPERATIONAL (DUAL) Alert height
200ft
71
CAT III without DH Minimum runway visual range
75m
72
Maximum wind conditions for ILS CAT II or CAT III AEO Headwind, Tailwind, Crosswind
25kt, 10kt, 20kt
73
Maximum wind conditions for ILS CAT II or CAT III OEI Headwind, tailwind, crosswind
20kt, 10kt, 10kt
74
Automatic landing is demonstrated: Glide slope angle between __ and __
-2.5deg and -3.5deg
75
Automatic landing is demonstrated: For airfield elevation below __
5750ft
76
Automatic landing is demonstrated: For weights above __
140 000 kg
77
Automatic landing is demonstrated: With aircraft weight below __
The maximum landing weight
78
Automatic landing is demonstrated: Depending on the aircraft situation and provided that the runway is approved for automatic landing, the flight crew can decide to perform an autoland up to __
251T
79
Autoland must not be used with an aircraft CG forward of __
15% MAC
80
APU START After three consecutive APU start attempts, the flight crew must wait __ before a new start attempt
60min
81
APU max N speed
107%
82
APU max EGT for APU start
1250degC
83
APU max EGT for APU running
650degC
84
APU Battery Restart Limit (elec emer config)
25000ft
85
APU BLEED Max altitude to assist engine start
20000ft
86
APU BLEED Max altitude for airconditioning and pressurization (single pack operation)
22500ft
87
APU BLEED Max altitude for air conditioning and pressurization (dual pack operation)
17500ft
88
ENG EGT LIMIT Takeoff and go-around
900degC
89
ENG EGT LIMIT MCT
850degC
90
ENG EGT LIMIT Starting on ground
700degC
91
ENG EGT LIMIT Starting in flight
900degC
92
ENG max N1
101.5%
93
ENG max N2
103.5%
94
ENG max N3
101.5%
95
ENG max oil temp continuous operation
191degC
96
ENG max oil temp transient operation (limited to 15 min during takeoff)
196degC
97
ENG min oil temp for starting
-40degC
98
ENG min oil temp before takeoff
40degC
99
ENG oil min quantity Flight time below 10h
15qt
100
ENG oil min quantity ETOPS, or flight time at or above 10h
16qt
101
ENG oil minimum pressure
30psi
102
ENG starter Extended cycle: one continuous operation cycle of __
5mins
103
ENG starter Normal cycle: Two consecutive start attempts of __ maximum, plus __ continuous operation
3min, 1min
104
ENG starter High tailwinds (higher than __) may have an adverse effect on start. It may be necessary to reposition the airplane into the wind
15kt
105
ENG starter No running engagement of the starter when the N3 is above __ on ground, or __ in flight
10%, 30%
106
FLEX TAKEOFF TFLEX cannot be higher than TMAXFLEX, equal to ISA + __
60degC
107
ENG crosswind limit for landing
35kt (gust included)
108
Maximum altitude flaps/slats extended
20000ft
109
Maximum fuel temperature
55degC
110
Minimum fuel temperature The highest of freezing point or __ below 30000ft or __ above 30000ft, in inner tank
-44degC, -54degC
111
Maximum allowed fuel imbalance Inner tanks (outer balanced) Heavier tank full
2900kg
112
Maximum allowed fuel imbalance Inner tanks (outer balanced) Heavier tank 17000kg
4800kg
113
Maximum allowed fuel imbalance Inner tanks (outer balanced) Heavier tank 7500kg
7500kg
114
Maximum allowed fuel imbalance Outer tanks (inner balanced) Heavier tank full
1480kg
115
Maximum allowed fuel imbalance Outer tanks (inner balanced) Heavier tank 2400kg
1580kg
116
Maximum allowed fuel imbalance Outer tanks (inner balanced) Heavier tank 1730kg
1730kg
117
Minimum fuel quantity for takeoff
5200kg
118
Severe ice accretion on airframe, thickness
5mm (0.2in) or more
119
Maximum brake temperature for takeoff (brake fans off)
300degC
120
NWS limit angle
72deg
121
Taxi with deflated or damaged tires Maximum one tire per gear is deflated (consider three gears) Max taxi speed
7kt
122
Taxi with deflated or damaged tires Two tires are deflated on the same main gear (maximum one main gear) Max taxi speed, max nws angle
3kt, 30deg
123
Ground alignment of the IRS is possible in lattitudes between __ North and __ South
82deg, 82deg
124
Minimum flight crew oxygen pressure 30deg, CAPT or FO
540psi
125
Minimum flight crew oxygen pressure 30deg, 3rd or 4th occupant
750psi
126
The predictive GPWS functions should be inhibited when the aircraft position is less than __ from the airfield
15nm
127

AIRBUS A330 (2 decks)

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