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Airbus > Lim A320 > Flashcards

Lim A320 Flashcards

1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS. Clean configuration?

A

-1 g to +2.5 g

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2
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS. Other configuration?

A

0g to +2 g

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3
Q

Runway slope (mean) limitation

A

±2 %

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4
Q

Runway altitude limitation

A

9200 ft

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5
Q

Nominal runway width

A

45 m

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6
Q

Minimal runway width

A

30 m

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7
Q

Maximum demonstrated crosswind (takeoff and landing)

A

38kn (gust included)

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8
Q

Maximum tailwind for takeoff.CEO

A

15 kn

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9
Q

Maximum tailwind for takeoff. NEO

A

10 kn

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10
Q

Maximum tailwind for landing. All

A

15 kn

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11
Q

The maximum wind for passenger door operation is

A

65kn

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12
Q

The maximum wind for FWD and AFT cargo door operation is

A

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

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13
Q

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

A

65 kn

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14
Q

COCKPIT WINDOW OPEN MAXIMUM SPEED

A

200 kn

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15
Q

Maximum speed with the landing gear extended (VLE)

A

280 kn/M 0,67

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16
Q

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

A

250 kn/M.60

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17
Q

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

A

220 kn /M 0.54

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18
Q

Maximum ground speed

A

195kn

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19
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL)

A

115 kn

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20
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL) CEO

A

114 kn

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21
Q

WIPERS MAXIMUM OPERATING SPEED

A

230 kn

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22
Q

With passengers on board, it is not recommended to exceed ____ min without air conditioning supply.

A

20 min

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23
Q

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time?

A

Yes

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24
Q

Maximum positive differential pressure

A

9,0 PSI

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25
Q

Maximum negative differential pressure

A

-1,0 PSI

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26
Q

Safety relief valve setting

A

8,6 PSI

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27
Q

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time?

A

Yes

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28
Q

The autopilot can be used with the following minimum values: at take off

A

100 ft AGL and at least 5 s after liftoff

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29
Q

The autopilot can be used with the following minimum values: In approach with F-G/S  mode

A

200 ft AFL

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30
Q

The autopilot can be used with the following minimum values: In approach with FINAL APP, V/S or FPA mode

A

250 ft AGL

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31
Q

The autopilot can be used with the following minimum values: in circling approach

A

500 ft AGL for aircraft category C (600 ft AGL for aircraft category D)

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32
Q

The autopilot can be used with the following minimum values: After a manual go-around

A

100 ft AGL

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33
Q

The autopilot can be used with the following minimum values: In all other phases

A

900 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 900 ft AGL

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34
Q

NAV mode may be used after takeoff provided that:

A

‐ GPS PRIMARY  is available, or
‐ The flight crew checked the FMGS takeoff updating.

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35
Q

NAV mode may be used in terminal area provided that:

A

‐ GPS PRIMARY  is available, or
‐ the appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed, or
‐ FMS navigation is crosschecked with navaid raw data.

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36
Q

DEGRADED SITUATION

If GPS PRIMARY LOST  is displayed on the ND and MCDU, the navigation accuracy remains sufficient for RNP operations provided that…

A

the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.

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37
Q

RNAV APPROACH

An RNAV(RNP) approach may be performed, with GPS PRIMARY not available…3

A

…only if the radio navaid coverage supports the RNP value and HIGH accuracy is displayed on the MCDU with the specified RNP, and an operational approval is obtained.

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38
Q

ILS CATEGORY II. Minimum decision height.

A

100 ft

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39
Q

S CATEGORY II. At least one autopilot must be engaged in APPR mode, and…

A

…CAT 2 or CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.

40
Q

ILS CATEGORY II. For manual landing, AP should be disconnected no later than…

A

80 ft AGL

41
Q

ILS CATEGORY III FAIL PASSIVE (SINGLE). Minimum decision height…

A

50 ft. A/THR must be used in selected or managed speed.

42
Q

ILS CATEGORY III FAIL PASSIVE (SINGLE). At least one autopilot must be engaged in APPR mode, and…

A

…CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.

43
Q

ILS CATEGORY III FAIL OPERATIONAL (DUAL). Alert height…A/THR…, autopilots…

A

100 ft AGL. A/THR must be used in selected or managed speed. Both autopilots must be engaged in APPR mode, and CAT 3 DUAL must be displayed on the FMA

44
Q

ILS CATEGORY III FAIL OPERATIONAL (DUAL). CAT III without DH:

Minimum Runway Visual Range(NEO)…

A

75 m

45
Q

ILS CATEGORY III FAIL OPERATIONAL (DUAL). CAT III with DH:

Minimum Decision Height (CEO)…/CAT III without DH:

Minimum Runway Visual Range

A

22ft/75m

46
Q

ENGINE-OUT. CAT II and CAT III fail passive autoland are only approved in

A

configuration 3 and FULL, and if engine-out procedures are completed before reaching 1 000 ft in approach.

47
Q

MAXIMUM WIND CONDITIONS FOR ILS/MLS  CAT II OR CAT III AND FOR GLS  CAT I(CEO) HEADWIND?

A

‐ 40 kt for CAT II automatic approach

‐ 30 kt for CAT III and GLS CAT I automatic approach
‐ 30 kt for automatic landing and automatic rollout

48
Q

MAXIMUM WIND CONDITIONS FOR ILS/MLS  CAT II OR CAT III AND FOR GLS  CAT I (CEO) TAILWIND?

A

10 kn

49
Q

MAXIMUM WIND CONDITIONS FOR ILS/MLS  CAT II OR CAT III AND FOR GLS  CAT I (CEO). CROSSWIND

A

‐ 25 kt for CAT II automatic approach
‐ 20 kt for CAT III and GLS CAT I automatic approach
‐ 20 kt for automatic landing and automatic rollout

50
Q

After ______ consecutive APU start attempts, the flight crew must wait ____min before a new start attempt.

A

Three attempts…60min

51
Q

APU Maximum N speed

A

107%

52
Q

Maximum EGT for APU start (below 35 000 ft)

A

1090 C

53
Q

Maximum EGT for APU start (above 35 000 ft)

A

1 120 °C

54
Q

Maximum EGT for APU running

A

675 C

55
Q

During refuel/defuel procedures, APU starts or shutdown are permitted with the following restrictions:

A

‐ If the APU failed to start or following an automatic APU shutdown, do not start the APU
‐ If a fuel spill occurs, perform a normal APU shutdown

56
Q

APU BLEED

Max altitude to assist engine start

A

20 000ft

57
Q

APU BLEED. Max altitude for air conditioning and pressurization (single pack operation)

A

22500 ft

58
Q

APU BLEED. Max altitude for air conditioning and pressurization (dual pack operation)

A

15000 ft

59
Q

Use of APU bleed air for wing anti-ice is ____ permitted.

A

NOT

60
Q

The BACF results should not be used in the case of:

A

‐ Any failure impacting aircraft performance during landing (brakes, engines, aerodynamics…) or,
‐ Runways with an average slope greater than 1 % (uphill or downhill).

61
Q

It is prohibited to use the GSM Onboard System:

A

‐ Below 3 000 m AGL (approximately 10 000 ft)
‐ In some geographical areas
Note:
The GSM Onboard System is able to identify the above-mentioned flight conditions. If the system identifies any of these conditions, it automatically turns off.

62
Q

THRUST SETTING/EGT LIMITS (NEO). Takeoff (1) and Go-around

All engines operative TIME? EGT?

A

5 minutes, 1083 C

63
Q

THRUST SETTING/EGT LIMITS (NEO). Takeoff (1) and Go-around. One eng. inoperative. Time? EGT?

A

10 minutes. 1083 C

64
Q

Maximum Continuous Thrust (MCT) (NEO). Time? EGT?

A

Not limited. 1043 C

65
Q

(NEO) THRUST SETTING/EGT LIMITS. Engines. Starting. On ground. In flight. EGT?

A

1083 C

66
Q

(CEO) THRUST SETTING/EGT LIMITS. Takeoff and Go-around. All engines operative. Time? EGT?

A

5 minutes. 650 C

67
Q

(CEO) THRUST SETTING/EGT LIMITS. Takeoff and Go-around. One engine inoperative. Time? EGT?

A

10 minutes. 650 C

68
Q

(CEO) Maximum Continuous Thrust (MCT). Time? EGT?

A

Unlimited. 610 C

69
Q

(CEO) Starting. On ground/in flight . EGT?

A

635 C

70
Q

(NEO) Maximum N1 in normal operation./ Maximum N1 permitted

A

100%/105%

71
Q

(NEO) Maximum N2 in normal operation./ Maximum N2 permitted

A

100%/105%

72
Q

(CEO) Maximum N1/ Maximum N2

A

100%/100%

73
Q

(CEO) Maximum continuous oil temperature

A

155 C

74
Q

CEO. Maximum transient oil temperature 15 minutes

A

165 C

75
Q

CEO. Minimum starting oil temperature

A

-40 C

76
Q

CEO. Minimum oil temperature before idle is exceeded

A
  • 10 C
77
Q

CEO. Minimum oil temperature before take off

A

50 C

78
Q

CEO. Minimum oil quantity

A

11 qt + estimated consumption. Average estimated consumption 0.3q/h

79
Q

CEO. Minimum oil pressure

A

60 PSI

80
Q

NEO. Maximum temperature

A

151 C

81
Q

NEO. Minimum starting temperature

A
  • 40 C
82
Q

NEO. Minimum temperature before take off

A

52 C

83
Q

NEO. Oil quantity (OAT >- 30 C)

A

14qt

84
Q

NEO. Oil quantity (OAT <- 30 C)

A

16,5 qt

85
Q

NEO. Minimum oil pressure

A

65 PSI

86
Q

NEO. Maximum oil pressure

A

270 PSI

87
Q

A standard automatic start that includes up to two start attempts, is considered ___ cycle

A

One

88
Q

NEO. For ground starts (automatic or manual), a ___s pause is required between successive cycles

A

15

89
Q

NEO. A ____min cooling period is required, subsequent to _____failed cycles, or ____ min of continuous or cumulated crank

A

15/three/15

90
Q

NEO. The starter must not be run when N2 is above____ %.

A

20

91
Q

CEO. For ground starts (automatic or manual), a ____s pause is required between successive cycles

A

15

92
Q

CEO. A ____min cooling period is required, subsequent to ______ failed cycles or ___min of continuous crank

A

30 / three / 5

93
Q

Engines. For manual start, observe a ____-minute maximum cycle time

A

Two

94
Q

Engines. For crank, observe a ___ min maximum cycle time

A

5

95
Q

Engines. The starter must not be run when N2 is above ____% on-ground and ____% in-flight.

A

10/ 18

96
Q

Maximum reverse should not be used below ___ kt. Idle reverse is permitted down to __________.

A

70/ aircraft stop

Airbus (1 decks)

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