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A320 > Limitation > Flashcards

Limitation Flashcards

1
Q

Maneuver load (clean)

A

-1g to +2.5g

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2
Q

Maneuver load (other conf)

A

0g to +2g

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3
Q

Runway slope

A

±2%

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4
Q

Runway altitude

A

9.200ft
(YYB~YYL - 14.100ft)

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5
Q

Runway width

A

45m
minimal 30m

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6
Q

Maximum crosswind for takeoff

A

25kt (Gust Included)

Azul limitation

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7
Q

Maximum crosswind for landing

A

25kt (Gust Included)

Azul limitation

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8
Q

Maximum Tailwind for Takeoff

A

15kt

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9
Q

Maximum tailwind for landing

A

10kt

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10
Q

Maximum wind for passenger door operation

A

65kt

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11
Q

Maximum wind for FWD and AFT cargo door operation

A

40kt (50kt if the aircraft nose is into the wind, or if the FWD or AFT door are on the leeward side)

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12
Q

The FWD and AFT cargo doors must be closed before the wind speed exceeds

A

65kt

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13
Q

Maximum recomended crosswind on wet and contaminated runways

A

15kt

*Note:​ The maximum crosswind values given in the above table are recommended values​based on Azul Safety Department assessement for regular operations.

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14
Q

Altitude limitation for landing on PFC/Grooved wet runways

A

Runway pressure altitude below 4 000ft

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15
Q

Cockpit window open maximum speed

A

200kt

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16
Q

Maximum flap/slat speeds A321

A

Flap 1 - 243kt (Holding)

Flap 1 + F - 225kt (Takeoff)

Flap 2 - 215kt (Takeoff/Approach)

Flap 3 - 195kt (Takeoff/Approach/Landing)

FULL - 186kt (Landing)

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17
Q

Maximum flap/slat speeds A320

A

Flap 1 - 230kt (Holding)

Flap 1 + F - 215kt (Takeoff)

Flap 2 - 200kt (Takeoff/Approach)

Flap 3 - 185kt (Takeoff/Approach/Landing)

FULL - 177kt (Landing)

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18
Q

Maximum operating speed VMO/MMO

A

350kt / M 0.82

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19
Q

Maximum speed with landing gear extended (VLE)

A

280kt/M.067

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20
Q

Maximum speed in wich the landing gear may be extended (VLO extension)

A

250kt/M.060

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21
Q

Maximum speed at which the landing gear may be retracted (VLO retraction)

A

220kt/M.054

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22
Q

Maximum tire speed

A

195kt

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23
Q

Minimum control speed for landing (VMCL)

A

116kt

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24
Q

Wipers maximum operating speed

A

230kt

*Note:​ This limitation is applicable when the wipers are sweeping. It is not applicable if the wipers​are not sweeping for any reasons

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25
Maximum taxi weigth A320
77 400 kg (170 637 lb) 79 400 kg (175 047 lb) (PR-YRD, PR-YRE, PR-YRH, PR-YRI, PR-YRJ, PR-YRK, PR-YRT, PR-YRU)
26
Maximum takeoff weight A320
77 000 kg (169 755 lb) 79 000 kg (174 165 lb) (PR-YRD, PR-YRE, PR-YRH, PR-YRI, PR-YRJ, PR-YRK, PR-YRT, PR-YRU)
27
Maximum landing weight A320
67 400 kg (148 591 lb)
28
Maximum zero fuel weight A320
64 300 kg (141 757 lb)
29
Minimum weight A320
40 600 kg (89 508 lb)
30
Maximum taxi weght A321
88 400 kg (197 093 lb)
31
Maximum takeoff weight A321
88 000 kg (196 211 lb)
32
Maximum landing weight A321
79 200 kg (174 606 lb)
33
Maximum zero fuel weight A321
75 600 kg (166 669 lb)
34
Minimum weight A321
46 600 kg (102 736 lb)
35
With passengers on board, it is not recommended to exceed ___ min without air conditioning supply
20 min
36
The flight crew must not use bleed air from the ___________ and from the ___________ at the​same time, to prevent any adverse effect on the Bleed Air System
APU BLEED HP Air start unit
37
During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must​limit the time that the aircraft electric power supply is used, in normal avionics ventilation system​configuration, as follows:
OAT ≤ 49 °C​ - No limitation 49 °C < OAT ≤ 55 °C​ - 2 h 55 °C < OAT ≤ 60 °C​ - 1 h 60 °C < OAT ≤ 64 °C​ - 0.5 h
38
Cabin pressure - maximum positive differential pressure
9.0 PSI
39
Cabin pressure - maximum negative differential pressure
-1.0 PSI
40
Cabin pressure - safety relief valve setting
8.6 PSI
41
Packs use with LP air conditioning unit
The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at​the same time, to prevent any adverse effect on the Air Conditioning system
42
Use of autopilot at takeoff
100 ft AGL and at least 5s after takeoff
43
Use of autopilot in approach with F-G/S mode
200 ft AGL
44
Use of autopilot in approach with FINAL APP, V/S or FPA mode
250 ft AGL
45
Use of autopilot in circling approach
500 ft AGL for aircraft category C (600 ft AGL for​aircraft category D)
46
Use of autopilot in ILS/MLS approach when CAT 1 is displayed on the FMA
160 ft AGL
47
Use of autopilot in ILS/MLS approach when CAT2, CAT3 SINGLE or CAT3 DUAL is displayed on FMA
0 ft AGL if autoland
48
Use of autopilot after manual go-around
100 ft AGL
49
Use of autopilot in all other fases
500 ft AGL The AP or FD in OP DES or DES mode can be used in approach. However, its use is only permitted if the FCU selected​altitude is set to, or above, the higher of the two: MDA/MDH or 500 ft AGL
50
RNP accuracy with GPS PRIMARY - en route
With AP on - 1 NM With AP off and FD on - 1 NM With AP off and FD off - 1.1 NM
51
RNP accuracy with GPS PRIMARY - in terminal area
With AP on - 0.5 NM With AP off and FD on - 0.51 NM With AP off and FD off - 0.51 NM
52
RNP accuracy with GPS PRIMARY - in approach
With AP on - 0.3 NM With AP off and FD on - 0.3 NM With AP off and FD off - 0.3 NM with F-LOC​​ deviation​ (Not authorized without ​F-LOC​ ​ deviation)
53
If GPS PRIMARY LOST is displayed on the ND and MCDU
The navigation accuracy remains​sufficient for RNP operations provided that, the RNP value is checked or entered on the MCDU ​and HIGH ACCURACY is displayed
54
ILS CAT II minimum decision height
100 ft (For manual landing, AP should be disconnected no later than 80 ft AGL)
55
Limit of APU start attempt
After three consecutive APU start attempts, the flight crew must wait 60 min before a new start​attempt
56
APU maximum N speed
107 %
57
APU maximum EGT for start (bellow 25 000 ft)
900 ºC
58
APU maximum EGT for start (above 25 000 ft)
982 ºC
59
Maximum EGT for APU running (with 5s confirmation shutdown)
682 ºC
60
Maximum EGT for APU running (for immediate shutdown)
700 ºC to 742 ºC
61
APU operation and normal restart envelope
41 000 ft
62
APU battery restart limit (Elec emerg config)
25 000 ft
63
Maximum altitude for use of APU BLEED
20 000 ft
64
APU BLEED maximum altitude to assist engine start
20 000 ft
65
APU BLEED maximum altitude altitude for air conditioning and pressurization (single pack operation)
20 000 ft 22 500 ft (PR-YRT, PR-YRU)
66
APU BLEED maximum altitude altitude for air conditioning and pressurization (dual pack operation)
15 000 ft
67
TOGA/FLEX/EGT time and temperature limit (all engines operative)
Time limit 5 minutes EGT limit 1060 ºC
68
TOGA/FLEX/EGT time and temperature limit (one engine inoperative)
Time limit 10 minutes EGT limit 1060 ºC
69
Maximum continuous thrust time and temperature limit
Time not limited EGT limit 1025 ºC
70
EGT temperature limit starting (on ground)
750 ºC
71
EGT temperature limit starting (in flight)
875 ºC
72
Maximum N1
101 % *Note:​ The N1 limit depends on the ambient conditions and on the configuration of the engine air​bleed. These parameters may limit N1 to a value that is less than the above-mentioned N1​value
73
Maximum N2
116.5 %
74
Oil temperature - maximum continuous temperature
140 ºC
75
Oil temperature - maximum transient temperature (15 min)
155 ºC
76
Oil temperature - minumum starting temperature
-40 ºC -29 ºC (PR-YRA, PR-YRB, PR-YRC, PR-YRD, PR-YRE, PR-YRF, PR-YRH, PR-YYI, PR-YYJ, PR-YYK, PR-YYL)
77
Oil temperature - minumum temperature before takeoff
19 ºC
78
Minimum oil quantity
The minimum oil quantity is the highest value of: ​‐​ 10.6 qt, or​ ‐​ 8.9 qt + estimated consumption.​ Maximum estimated consumption = 0.45 qt/h
79
Minimum oil pressure
17.4 PSI
80
Maximum oil pressure (when oil temperature is above 50 °C)
130.5 PSI
81
Maximum oil pressure (when oil temperature is bellow 50 °C)
145 PSI
82
Starter attempts and time for cooling
‐​ A standard automatic start that includes up to three start attempts, is considered one cycle​ ‐​ For ground starts (automatic or manual), a 60 s pause is required between successive cycles ​‐​ A 15 min cooling period is required, subsequent to three failed cycles ​‐​ The starter must not be run when N2 is above 63 %
83
Maximum reverse thrust speed limitation
Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop
84
FLEX temperature limitation
TFLEX cannot be: ​‐​ Higher than TMAXFLEX, equal to ISA + 55 °C. (+50 ºC on LEAP 1A 29K) (+52 ºC on LEAP 1A 32K) ​‐​ Lower than the flat temperature (TREF).​ ‐​ Lower than the actual OAT.
85
Engine crosswind limitation for start
45 kt
86
Engine crosswind limitation for takeoff
35 kt (gust included)
87
Maximum altitude with flaps/slats extended
20 000 ft
88
Fuel imbalance at takeoff - inner tanks (outer tanks balanced) - A320
Full - 500 kg (1 102 lb) 3 000 kg (6 613 lb) - 1 050 kg (2 314 lb) 1 450 kg (3 196 lb) - 1 450 kg ( 3 196 lb)
89
Outer tanks maximum assimetry (inner tanks ballanced)
370 kg (815 lb)
90
Fuel imbalance in flight and at landing - inner tanks (outer tanks balanced) - A320
Full - 1 500 kg (3 306 lb) 4 300 kg (9 479 lb)​ - 1 600 kg (3 527 lb) 2 250 kg (4 960 lb)​ 2 250 kg (4 960 lb) *There is no limitation below 2 250 kg​(4 960 lb)
91
Outer tanks maximum assimetry
690 kg (1 521 lb) The maximum fuel imbalance in the outer wing fuel tanks (one full/one empty) is allowed provided​that:​ ‐​The fuel quantity of the outer and inner wing fuel tanks of one side is equal to the fuel quantity of​the outer and inner wing fuel tanks on the other side, or​ ‐​On the side of the lighter outer tank, the fuel quantity of the inner tank is more than the fuel​quantity of the opposite inner tank. The difference between the fuel quantity in the inner tanks​should not be more than 3 000 kg (6 613 lb). ​*Note:​ In exceptional conditions (i.e. fuel system failure), the above-mentioned values for​maximum fuel imbalance may be exceeded without significant effect to the aircraft​handling qualities. The aircraft remains fully controllable in all flight phases
92
Fuel imbalance at takeoff - A321
Full​ - 400 kg (882 lb) 3 000 kg (6 614 lb)​ - 400 kg (882 lb) 700 kg (1 543 lb)​ - 700 kg (1 543 lb)
93
Fuel imbalance in flight and at landing
Full​ - 1 320 kg (2 910 lb) 4 000 kg (8 818 lb)​ - 1 450 kg (3 196 lb) 2 350 kg (5 180 lb)​ - 2 350 kg (5 180 lb) *Note:​ In exceptional conditions (i.e. fuel system failure), the above-mentioned values for​maximum fuel imbalance may be exceeded without significant effect to the aircraft​handling qualities. The aircraft remains fully controllable in all flight phases.
94
Minimum fuel quantity for takeoff
1 500 kg (3 307 lb) The ECAM alerts that are related to fuel low level in the wing tanks (FUEL WING TK LO LVL, etc.)​must not appear for takeoff
95
Use of rain repellent
Moderate or heavy rain
95
Maximum brake temperature for takeoff (brake fan off)
300 ºC
96
Maximum NWS angle
±85 °
97
Maximum tire speed during turn if one tire per gear is deflated
7 kt
98
Maximum tire speed during turn if two tires on the same main gear is deflated
3 kt
99
Maximum NWS with tire deflated
30 º

A320 (3 decks)

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