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Limitações > A321 > Flashcards

A321 Flashcards

1
Q

Flight maneuvering load acceleration limits: clean

A

-1G to +2.5G

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2
Q

Flight maneuvering load acceleration limits: other than clean

A

0G to +2G

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3
Q

Environmental envelope:
Max pressure altitude

A

39800 ft

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4
Q

Environmental envelope:
min temp

A

-70ºC

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5
Q

Environmental envelope:
Max temp

A

+55ºC

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6
Q

Environmental envelope:
Takeoff and landing max alt

A

9200ft

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7
Q

Environmental envelope:
Takeoff and landing min alt

A

-2000ft

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8
Q

Runway slope (mean) limits

A

+/-2%

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9
Q

Maximum certified crosswind for takeoff

A

35kts (gust included)

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10
Q

Maximum demonstrated crosswind for landing

A

38kts (gust included)

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11
Q

Maximum tailwind for takeoff

A

10kts

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12
Q

Maximum tailwind for landing

A

10kts

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13
Q

Maximum wind for passenger door operation

A

65kts

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14
Q

maximum wind for FWD and AFT cargo doors operation

A

40kts (50 if aircraft’s nose is into the wind or if cargo doors on the leeward side)

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15
Q

Maximum cockpit window open speed

A

200kts

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16
Q

Maximum flaps/slats speeds:
Conf 1

A

243kts

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17
Q

Maximum flaps/slats speeds:
Conf 1+F

A

225kts

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18
Q

Maximum flaps/slats speeds:
Conf 2

A

215kts

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19
Q

Maximum flaps/slats speeds:
Conf 3

A

195kts

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20
Q

Maximum flaps/slats speeds:
Conf FULL

A

186kts

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21
Q

VMO

A

350kts

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22
Q

MMO

A

M 0.82

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23
Q

Maximum speed with the landing gear extended (VLE)

A

280 kts / M0.67

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24
Q

Maximum speed at which the landing gear may be exttended (VLO extension)

A

250kts / M0.60

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25
Q

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

A

220kts / M0.54

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26
Q

Maximum tire speed

A

195kts

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27
Q

Minimum control speed for landing (VMCL)

A

116kts

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28
Q

Maximum wiper operating speed

A

230kts

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29
Q

Weight limitations (321NLR):
Maximum taxi weight

A

97 400 kg

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30
Q

Weight limitations (321NLR):
Maximum takeoff weight (brake release)

A

97 000 kg

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31
Q

Weight limitations (321):
Maximum landing weight:

A

79 200 kg

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32
Q

Weight limitations (321NLR):
Maximum zero fuel weight:

A

75 600kg

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33
Q

Weight limitations (321):
Minimum weight:

A

46 600kg

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34
Q

Weight limitations (321N):
Maximum taxi weight:

A

93 900kg

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35
Q

Weight limitations (321N):
Maximum takeoff weight (brake release):

A

93 500 kg

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36
Q

Weight limitations (321N):
Maximum Zero Fuel Weight

A

75 600 kg

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37
Q

The aircraft’s electric power supply use must be limited to 2h when the OAT is

A

within 49ºC to 55ºC

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38
Q

The aircraft’s electric power supply use must be limited to 1h when the OAT is

A

within 55ºC to 60ºC

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39
Q

The aircraft’s electric power supply use must be limited to 0.5h when the OAT is

A

within 60ºC to 64ºC

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40
Q

Maximum positive differential pressure

A

9.0PSI

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41
Q

Maximum negative differential pressure

42
Q

Safety relief valve setting

43
Q

Use of Packs with LP Air cond unit

A

the flight crew must NOT use conditioned air from the packs and from the LP Air cond unit at the same time, to prevent any adverse effect on the AC system

44
Q

APU bleed use with HP Air Start Unit

A

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System

45
Q

Autopilot limitations:
at takeoff

A

100ft AGL and at least 5 s after liftoff

46
Q

Autopilot limitations:
In approach with FINAL APP, V/S or FPA mode

A

250 ft AGL

47
Q

Autopilot limitations:
In circling approach

48
Q

Autopilot limitations:
ILS approach with CAT 1 FMA

49
Q

Autopilot limitations:
ILS approach with CAT2, 3 SINGLE or DUAL FMA

A

0ft AGL if autoland

50
Q

Autopilot limitations:
After a manual go-around

51
Q

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:

A

MDA/MDH or 900ft AGL

52
Q

RNP accuracy with GPS PRIMARY is:
IF AP ON (in NAV):

A

-En route= 1NM
-In terminal area= 0.5NM
-In approach= 0.3NM

53
Q

RNP accuracy with GPS PRIMARY is:
With AP OFF and FD ON:

A

-En route= 1NM
-In terminal area= 0.51NM
-In approach= 0.3NM

54
Q

RNP accuracy with GPS PRIMARY is:
With AP OFF and FD OFF:

A

-En route= 1.1NM
-In terminal area= 0.51NM
-In approach= 0.3NM

55
Q

Maximum wind for ILS CAT II or CAT III:

A

Headwind: 15kts
Crosswind: 10kts
Tailwind: 10kts

56
Q

Autoland (Cat II and III) configuration

A

Conf 3 and Conf FULL

57
Q

Glide slope beam limits

A

-2.5º to -3.25º

58
Q

Autoland min pressure altitude

59
Q

APU Start waiting time after 3 consecutive start attempts

60
Q

APU Maximum rotor (N) speed

61
Q

APU:
-Maximum EGT for APU start (below 35000ft):

62
Q

APU
-Maximum EGT for APU start (above 35000ft):

63
Q

APU:
-Maximum EGT for APU running

64
Q

APU start/Shutdown limitation while refuelling

A

Start and shutdown is permitter, provided that:
-If fuel spill occurs, perform a normal APU shutdown

65
Q

APU battery restart Max alt

66
Q

APU use of bleed air max alt

67
Q

APU max alt to assist engine start

68
Q

APU max altitude for air cond and pressurization (single pack)

69
Q

APU max alt for ac and pressurization (both packs)

70
Q

Use of APU bleed air for wing anti-ice

A

NOT PERMITTED

71
Q

LEAP-1A:
TOGA and FLEX max EGT

72
Q

LEAP-1A:
MCT max EGT

73
Q

LEAP-1A:
Max EGT while starting on ground

74
Q

LEAP-1A:
Max EGT while starting inflight

75
Q

LEAP-1A:
Maximum N1

76
Q

LEAP-1A:
Maximum N2

77
Q

Maximum continuous OIL temperature

78
Q

Maximum transient (15min) OIL temperature

79
Q

Minimum starting OIL temperature

80
Q

Minimum Oil temperature before takeoff

81
Q

Minimum oil quantity

A

The highest of:
-10.6qt, or
-8.9qt + estimated consumption (0.45qt/h)

82
Q

Minimum oil pressure

83
Q

Maximum oil pressure

A

130.5PSI (If oil temp > 50ºC)
145PSI (If oil temp < 50ºC)

84
Q

LEAP1-A Engine starter limitations:
A standard automatic start that includes up to _ start attempts, is considered one cycle

85
Q

LEAP1-A Engine starter limitations:
For ground starts, a __ sec pause is required between successive cycles

A

60 seconds

86
Q

LEAP1-A Engine starter limitations:
Cooling period after 3 failed cycles

87
Q

LEAP1-A Engine starter limitations:
The starter must not be run when N2 is above

88
Q

FLEX limitations:
Maximum Flex temp

89
Q

Engine Start: Maximum crosswind

90
Q

Maximum operating altitude with slats and/or flaps extended:

91
Q

Minimum Fuel for takeoff=

A

1500kg + no low fuel level related ECAMS

92
Q

Maximum brake temperature for takeoff (brake fans off)

93
Q

Maximum NWS angle

94
Q

Max speed for Taxi with deflated tires:
If one tire per gear is deflated

95
Q

Max speed for Taxi with deflated tires:
If two tires are deflated on the same gear

96
Q

Max NWS angle withe deflated tires

97
Q

Ground alignment of the IRS is possible in latitutes between

A

82ºN and 82ºS

98
Q

During ground operation, when in icing conditions and the OAT is +3ºC or less, the following procedure should be applied for ice shedding:

A

(While stationary)
-Accelerate engines to 50% N1 for 5 seconds at intervals not more than 60 minutes.

99
Q

Maintenance action on the brakes is necessary if:

A

-Temp diff between 2 brakes of a gear >150ºC and one of them is >600ºC, or
-Temp diff between 2 brakes of a gear > 150ºC and one of them is at or below 60ºC, or
-Difference between the average temperature of the left gear brakes and right brakes is >200ºC
-THE TEMP OF ONE BRAKE EXCEEDS 800ºC

100
Q

Brake Fans use

A

I short turnaround or if any brake is likely to exceed 500ºC, use without delay. Otherwise, delay to 5’ after landing or entering gate, whichever happens first

Limitações (1 decks)

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