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EWEU Limitations > Limitations A319 + A320 OM - B > Flashcards

Limitations A319 + A320 OM - B Flashcards

1
Q

Flight Maneuvering Load Acceleration Limits

A

Clean configuration. . . . . . . . . . . . .. . . . . . .-1 g to +2.5 g

Other configurations. . . . . . . . . . . . . . . .. . . . 0 g to +2 g

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2
Q

Runway Slope

A

Runway slope (mean). . . . . . . . . . . . . . . . . . . . . . . . .±2 %

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3
Q

Runway Altitude

A320-214 (-BHA, -BHC)
A319-132 / A320-214 (all ex. -BHA, -BHC) / A320-216

A

A320-214 (-BHA, -BHC)
Runway altitude. . . . . . . . . . . . . . . . . . . . . . .. . . . . 14 100 ft

A319-132 / A320-214 (all ex. -BHA, -BHC) / A320-216
Runway altitude. . . . . . . . . . . . . . . . . . . . . . . . . 9200 ft

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4
Q

Nominal runway width

A

45 m

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5
Q

Minimal runway width

A

30 m

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6
Q

Maximum crosswind for takeoff and landing

A

30 kt gusting up to 38 kt

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7
Q

Maximum crosswind in LVO for takeoff

A

10 kt

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8
Q

Maximum tailwind for takeoff

A

10 kt

A319-132 / A320-214 (all ex. -BNK, -BNL)
Note: Maximum for takeoff — 15 kt on selected runways. Refer to OM-C (AAL) for runways with
15 kt maximum tailwind component for takeoff

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9
Q

Maximum tailwind for landing

A

10 kt

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10
Q

Maximum wind for passenger door operation

A

65 kt

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11
Q

Maximum wind for FWD and AFT cargo door operation

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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12
Q

Maximum Recommended Crosswind on Wet and Contaminated Runways

Damp / Wet / Up to 3 mm (1/8”) of water

A

30 kt gusting up to 38 kt

Maximum Crosswind for Take off AND Landing

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13
Q

Maximum Recommended Crosswind on Wet and Contaminated Runways

Slush Up to 3 mm (1/8”)

Dry Snow Up to 3 mm (1/8”)

Wet Snow Up to 3 mm (1/8”)

Frost

PIREP “GOOD”

A

25 kt

Maximum Crosswind for Take off AND Landing

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14
Q

Maximum Recommended Crosswind on Wet and Contaminated Runways

Compacted Snow

PIREP “Good to Medium”

A

20 kt

Maximum Crosswind for Take off AND Landing

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15
Q

Maximum Recommended Crosswind on Wet and Contaminated Runways

Dry Snow More than 3 mm (1/8”), up to 100 mm (4”)

Wet Snow More than 3 mm (1/8”),

  • for takeoff up to 25 mm (1”)
  • for landing up to 30 mm (6/5”)

Compacted Snow

OAT above -15°C

Slippery when wet

PIREP “Medium”

A

15 kt

Maximum Crosswind for Take off AND Landing

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16
Q

Maximum Recommended Crosswind on Wet and Contaminated Runways

Water More than 3 mm (1/8”), up to 12.7 mm (1/2”)

Slush More than 3 mm (1/8”), up to 12.7 mm (1/2”)

PIREP “Medium to poor”

A

10 kt

Maximum Crosswind for Take off AND Landing

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17
Q

Maximum Recommended Crosswind on Wet and Contaminated Runways

Ice (cold & dry)

PIREP “Poor”

A

5 kt

Maximum Crosswind for Take off AND Landing

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18
Q

Takeoff is not recommended on the following runway conditions:

A

–Wet ice

–Water on top of Compacted Snow

–Dry Snow or Wet Snow over Ice

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19
Q

Cockpit Window Open Maximum Speed

A

200 kt

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20
Q

Maximum Flaps/Slats Speeds

FLAPS 1

A

230 kt

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21
Q

Maximum Flaps/Slats Speeds

FLAPS 1 + F

A

215 kt

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22
Q

Maximum Flaps/Slats Speeds

FLAPS 2

A

200 kt

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23
Q

Maximum Flaps/Slats Speeds

FLAPS 3

A

185 kt

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24
Q

Maximum Flaps/Slats Speeds

FLAPS FULL

A

177 kt

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25
Q

Maximum Operating Speed VMO/MMO

A

VMO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 350 kt
MMO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .0.82 M

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26
Q

Maximum speed with the landing gear extended (VLE)

A

280 kt /0.67 M

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27
Q

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

A

250 kt /0.60

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28
Q

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

A

220 kt /0.54

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29
Q

Maximum Tire Speed

A

195 kt

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30
Q

Minimum Control Speed for Landing (VMCL)

A319-132

A

A319-132

109 kt

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31
Q

Minimum Control Speed for Landing (VMCL)

A320-214

A

A320-214

113 kt

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32
Q

Minimum Control Speed for Landing (VMCL)

A320-216

A

A320-216

108 kt

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33
Q

Taxi Speed

When the taxi weight is higher than 76000 kg

(during a turn)

A

20 kt during a turn

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34
Q

Wipers Maximum Operating Speed

A

230 kt

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35
Q

RAT deployment during flight test, the airspeed must be limited to?

A

250 kt

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36
Q

AVIONICS VENTILATION
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 ?
49 °C < OAT ≤ 55 °C ?
55 °C < OAT ≤ 60 °C ?
60 °C < OAT ≤ 64 °C ?

A

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

37
Q

CABIN PRESSURE

Maximum positive differential pressure?

A

9.0 PSI

38
Q

CABIN PRESSURE

Maximum negative differential pressure ?

A

-1.0 PSI

39
Q

CABIN PRESSURE

Safety relief valve Setting PSI?

A

8.6 PSI

40
Q

Autopilot Function
The autopilot can be used with the following minimum values:

At takeoff?

A

100 ft AGL or 5 s after liftoff

41
Q

Autopilot Function
The autopilot can be used with the following minimum values:

In non-precision approach using F-LOC◄ or FG/
S◄ (FLS◄ function)

A

200 ft AGL

42
Q

Autopilot Function
The autopilot can be used with the following minimum values:

In non-precision approach using FINAL APP◄,
NAV FPA, NAV V/S, TRK FPA, HDG V/S, LOC
V/S, LOC FPA

A

250 ft AGL

43
Q

Autopilot Function
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

44
Q

Autopilot Function
The autopilot can be used with the following minimum values:

ILS/MLS◄ approach when CAT1 is displayed
on the FMA

A

160 ft AGL

45
Q

Autopilot Function
The autopilot can be used with the following minimum values:

GLS◄ approach when AUTOLAND is not displayed
on the FMA

A

160 ft AGL

46
Q

Autopilot Function
The autopilot can be used with the following minimum values:

ILS/MLS◄ approach when CAT2 or CAT3
(single or dual) is displayed on the FMA

A

0 ft AGL if autoland

47
Q

Autopilot Function
The autopilot can be used with the following minimum values:

PAR approach (Precision Approach Radar)

A

250 ft AGL

48
Q

Autopilot Function
The autopilot can be used with the following minimum values:

After a manual go-around

A

100 ft AGL

49
Q

Autopilot Function
The autopilot can be used with the following minimum values:

In all other phases

A

500 ft AGL

50
Q

Takeoff in GPS Primary ◄
For certain airports, where the difference between the local coordinate system and WGS 84
(geodesic standard used by GPS, FMS) is not negligible, a map shift may occur after takeoff.
The flight crew must………………………………. for takeoff from these airports, until a safe altitude is
reached.

A

deselect the GPS

51
Q

RNP accuracy with GPS PRIMARY◄ is

En route

A

1 NM

52
Q

RNP accuracy with GPS PRIMARY◄ is

In terminal area

A

0.5 NM

53
Q

RNP accuracy with GPS PRIMARY◄ is

In approach

A

0.3 NM

54
Q

Use of NAV Mode

After Takeoff

NAV mode may be used after takeoff provided that:

A

NAV mode may be used after takeoff provided that:

–GPS PRIMARY◄ is available, or

–The flight crew checked the FMGS takeoff updating

55
Q

Use of NAV Mode

In Terminal Area

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.

56
Q

APU Start

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

A

After three consecutive APU start attempts, the flight crew must wait 60 min before a new start
attempt

57
Q

A P U

Maximum N Speed?

A

107%

58
Q

APU EGT

Maximum EGT for APU start (below 35 000 ft)?

Maximum EGT for APU start (above 35 000 ft)?

Maximum EGT for APU running ?

A

Maximum EGT for APU start
(below 35 000 ft). . . . . . . . . . . . . . . . . . . . . . 1 090 °C

Maximum EGT for APU start
(above 35 000 ft). . . . . . . . . . . . . . . . . . . . 1 120 °C

Maximum EGT for APU running. . . . . . . . . . . .675 °C

59
Q

Electrical Power

Maximum continuous load per generator ?

A

(100 %): 90 KVA

60
Q

Electrical Power

Maximum continuous load per TRU ?

A

200 A

61
Q

THRUST SETTING/EGT LIMITS

A319-132

Takeoff(1) and Go around
All engines operative
One engine inoperative

Time Limits and EGT Limits?

A

All engines operative 5 min

One engine inoperative 10 Min

with max 635 °C

62
Q

THRUST SETTING/EGT LIMITS

A320-214 / A320-216

Takeoff(1) and Go around
All engines operative
One engine inoperative

Time Limits and EGT Limits?

A

All engines operative 5 min

One engine inoperative 10 Min

with max 950 °C

63
Q

THRUST SETTING/EGT LIMITS

A319-132

Maximum Continuous Thrust (MCT)

Time Limits and EGT Limits?

A

Not time limited

max 610 °C

64
Q

THRUST SETTING/EGT LIMITS

A320-214 / A320-216

Maximum Continuous Thrust (MCT)

Time Limits and EGT Limits?

A

Not time limited

max 915 °C

65
Q

THRUST SETTING/EGT LIMITS

A319-132

Starting EGT?

A

max 635 °C

66
Q

THRUST SETTING/EGT LIMITS

A320-214 / A320-216

Starting EGT?

A

max 725 °C

67
Q

Engine Shaft Speeds

A320-214 / A320-216

Maximum N1 ?

Maximum N2 ?

A

Maximum N1 104 %

Maximum N2 105 %

68
Q

Engine Shaft Speeds

A319-132

Maximum N1 ?

Maximum N2 ?

A

Maximum N1 100 %

Maximum N2 100 %

69
Q

Oil Temperature

A319-132

Maximum continuous temperature. ?
Maximum transient temperature (15 min) ?
Minimum starting temperature ?
Minimum temperature before IDLE is exceeded ?
Minimum temperature before takeoff ?
A

Maximum continuous temperature. . . . . . . . . . 155 °C

Maximum transient temperature (15 min). . . . . 165 °C

Minimum starting temperature. . . . . . . . . . . . . . -40 °C

Minimum temperature before IDLE is exceeded.. . -10 °C

Minimum temperature before takeoff. . . . . . . . . . 50 °C

70
Q

Oil Temperature

A320-214 / A320-216

Maximum continuous temperature. ?
Maximum transient temperature (15 min) ?
Minimum starting temperature ?

Minimum temperature before takeoff ?

A

Maximum continuous temperature. . . . . . . . . . 140 °C

Maximum transient temperature (15 min). . . . . 155 °C

Minimum starting temperature. . . . . . . . . . . . . . -40 °C

Minimum temperature before takeoff. . . . . . . . - 10 °C

71
Q

Minimum Oil Pressure

A319-132

A

60 PSI

72
Q

Minimum oil pressure

A320-214 / A320-216

A

13 PSI

73
Q

Flex Takeoff

FLEX takeoff is not permitted on ……………………?

A

Contaminated RWYs

74
Q

Flex Takeoff A319-132

TFLEX cannot be:

–Higher than TMAXFLEX, equal to ISA ……… °C.
Note: When engine anti-ice is on, the flexible temperature is limited to ISA ……….. °C

A

A319-132

–Higher than TMAXFLEX, equal to ISA + 65 °C

Note: When engine anti-ice is on, the flexible temperature is limited to ISA + 60 °C

75
Q

Flex Takeoff

A320-216

TFLEX cannot be:

–Higher than TMAXFLEX, equal to ISA ……… °C.

A

A320-216

Higher than TMAXFLEX, equal to ISA + 70 °C.

76
Q

TFLEX cannot be:

A320-214

Higher than TMAXFLEX, equal to ISA……… °C. TMAXFLEX corresponds to a reduction of………. % from the full rated takeoff thrust.

A

A320-214

Higher than TMAXFLEX, equal to ISA + 53 °C. TMAXFLEX corresponds to a reduction of
25 % from the full rated takeoff thrust.

77
Q

A319-132

CROSSWIND OPERATION ON GROUND

This engine is able to start in crosswind up to……. kt ?

A

A319-132 Only

This engine is able to start in crosswind up to 35 kt

78
Q

Maximum operating altitude with slats and/or flaps extended?

A

Maximum operating altitude with slats and/or flaps extended

20000 ft

79
Q

FUEL TEMPERATURE JET A1

MIN ?

MAX?

A

MIN -43 °C

MAX +54 °C

80
Q

FUEL TEMPERATURE JET A

MIN ?

MAX?

A

MIN -36 °C

MAX +54 °C

81
Q

Fuel Imbalance at Takeoff

Inner Tanks (Outer Tanks Balanced)

Full ——————–? kg max imbalance

3000 kg ————? kg max imbalance

1450 kg ————-? kg max imbalance

A

Full ——————–500 kg

3000 kg ————1050 kg

1450 kg ————-1450 kg

82
Q

Fuel Imbalance at Takeoff

Outer Tanks (Inner Tanks Balanced)

? kg max imbalance

A

370 kg

83
Q

Fuel Imbalance in Flight and at Landing

Inner Tanks (Outer Tanks Balanced)

Full ——————-? kg max imbalance
4300 kg ———–? kg max imbalance
2250 kg ———–? kg max imbalance

A

Full ——————-1500 kg

4300 kg ———–1600 kg

2250 kg ———– 2250 kg

84
Q

Fuel Imbalance in Flight and at Landing

Outer Tanks

Maximum Asymmetry?

A

Maximum Asymmetry

690 kg

85
Q

Minimum fuel quantity for takeoff?

A

1500 kg

86
Q

Hydraulic

MAX OPERATING PRESSURE (AT ZERO DELIVERY) ?

A

3 000 PSI ± 200 PSI

87
Q

Maximum brake temperature for takeoff (brake fans ◄ off) ?

A

300 °C

88
Q

Maximum NWS angle ?

A

85 °

EWEU Limitations (1 decks)

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