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Airbus G4 Oral Prep (LB) > 2024 Limitations > Flashcards

2024 Limitations Flashcards

1
Q

Max Takeoff and Landing Tailwind

FCOM LIM-AG-OPS P 7/10

A

10 kts

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2
Q

Wipers Max Operating Speed

FCOM LIM-AG-SPD P6/6

A

230 kts

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3
Q

Max demonstrated crosswind (takeoff and landing)

FCOM LIM-AG-OPS P 7/10

A

38kts (gust included)

note: Airbus recommends that operators should not intentionally operate in crosswinds that exceed this value

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4
Q

Max wind for passenger door operation

FCOM LIM-AG-OPS P 7/10

A

65kts

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5
Q

Max wind for cargo door operation:

Max wind while cargo door is open:

FCOM LIM-AG-OPS P 7/10

A

40kts (50kts if nose into the wind or if doors are on the leeward side)

doors must be closed before the wind speed exceeds 65kts

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6
Q

GTK: Max Takeoff and Landing Pressure Altitude

FCOM LIM-AG-OPS P 7/10

A

9,200’

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7
Q

VMO

FCOM LIM-AG-SPD P 1/6

A

350kts

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8
Q

MMO

A

Mach .82

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9
Q

Max speed w/flight deck window open

A

200kts

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10
Q

Turbulent air penetration

VRA < 10,000’

A

250 kts

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11
Q

Rough Air Penetration Speed, VRA

A

275kts / .76mach

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12
Q

Why should we not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time?

FCOM LIM-AIR P 3/4

A

To prevent any adverse effect on the

Air Conditioning System.

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13
Q

Is APU Bleed Use with HP Air Start Unit allowed?

FCOM LIM-AIR P 1/4

A

No, to prevent adverse effect on the Bleed Air System.

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14
Q

Min height for A/P engagement during T/O:

FCOM LIM-AFS-10 P 1-2/6

A

100’ AGL or 5 seconds after liftoff.

transitioning from Ground Mode to Flight Mode

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15
Q

Min height A/P off ILS Approach when

CAT1 with CAT3 SINGLE/DUAL

is displayed on FMA

FCOM LIM-AFS-10 P 1-2/6

A

50’ below DA

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16
Q

Min height A/P off during ILS Approach when CAT1 is displayed on FMA

FCOM LIM-AFS-1R0 P 1-2/6

A

160’ AGL

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17
Q

Min height A/P off in non-precision approach using

FINAL APP, NAV FPA, NAV V/S, TRK FPA, HDG V/S

FCOM LIM-AFS-10 P 1-2/6

A

250’ AGL

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18
Q

Min height A/P off for Circling Approach

FCOM LIM-AFS-10 P 1-2/6

A

500’ AGL

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19
Q

Min A/P on after manual Go Around:

Go Around in all other phases:

FCOM LIM-AFS-10 P 1-2/6

A

100’ AGL

500’ 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 AGL.

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20
Q

Flaps/Slats max operating altitude

FCOM LIM-F_CTL P 1/2

A

FL200

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21
Q

Max fuel imbalance between inner wing tanks:

A

3,300 lbs (Allegiant)

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22
Q

Max outer wing tank fuel imbalance

A

1,521lbs

One tank empty/one tank full is allowed

provided total fuel in each wing is approximately equal.

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23
Q

Center tank fuel must be emptied before wings unless…

A

center fuel is ballast

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24
Q

Takeoff using center tank fuel is…

A

prohibited

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25
Q

WING TK LO LVL

warning ECAM must not be present when?

A

T/O

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26
Q

Do not extend landing gear above FL___

A

FL250

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27
Q

Maximum speed at which the landing gear may be extended,

VLO extension

FCOM LIM-AG-SPD P 3/6

A

250kts / M 0.60

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28
Q

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

FCOM LIM-AG-SPD P 3/6

A

220kts / M 0.54

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29
Q

Maximum speed with the landing gear extended,

VLE

FCOM LIM-AG-SPD P 3/6

A

280 kts / .67 Mach

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30
Q

Maximum Tire Speed

FCOM LIM-AG-SPD P 3/6

A

195 kts

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31
Q

Max brake temp for T/O with fans OFF

FCOM LIM-LG P 1/2

A

300˚C

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32
Q

With parking brake set, do not apply thrust in excess of…

A

75% N1

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33
Q

APU starter duty cycle

FCOM LIM-APU P 1/6

A

3/60

After 3 consecutive APU start attempts, the flight crew must wait 60 minutes before new start attempt

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34
Q

Engine Starter limits

FCOM LIM-ENG P 2/4

A

2 20 2 20 2 20 2 15

3 start attempts is one cycle

4 cycles, max 2 minutes each

rest between start cycles 20 seconds

15 minutes cooling period subsequent to four failed cycles

35
Q

Starter must not engage when N2 is above

FCOM LIM-ENG P 2/4

36
Q

Min oil quantity before engine start

A

9.5 qts (estimated used .5qts/hr)

min pressure of 13 PSI

37
Q

Nominal Runway Width

FCOM LIM-AG-OPS P 7/10

A

148’ nominal

38
Q

Cockpit Window Open Max Speed

FCOM LIM-AG-SPD P 1/6

39
Q

Max Speed and flight phase for Configuration 1

FCOM LIM-AG-SPD P 1/6

A

230

HOLDING

40
Q

Min Height for use of autopilot,

Straight-in LNAV/VNAV approach

A

applicable DA

41
Q

Min Fuel Qty for T/O

FCOM LIM-FUEL P 4/4

42
Q

Normal HYD operating pressure

A

3,000 psi +- 200

43
Q

Load Acceleration Limits: Clean Configuration

Other Configurations

FCOM LIM-AG-F_CTL P 1/2

A

Clean: -1 g to +2.5 g

Other: 0 g to +2 g

44
Q

Min / Max Takeoff pressure altitude

FCOM LIM-AG-OPS P1-6/10

A
  • 1,000’ to 9,200’ P1, 3, 4
  • 2,000’ to 9,200’ P2, 5, 6

various aircraft

45
Q

Max Pressure Altitude

FCOM LIM-AG-OPS P1-6/10

A

39,100’ or 39,800’

46
Q

Runway Slope (mean)

FCOM LIM-AG-OPS P 6/10

47
Q

Max Recommended crosswind on DAMP (<3mm) runway,

ESF or PIREP: Good

FCOM LIM-AG-OPS P 8/10

48
Q

Max recommended crosswind with compacted snow below -15° OAT,

ESF or PIREP Good to Medium:

A

148’+: 29kts

100’-148’: 10kts

49
Q

Max Recommended Crosswind on runway with
Dry snow (3mm-100mm),
wet snow (3mm-30mm),
compacted snow OAT above -15°,
Dry snow over compacted snow,
wet snow over compacted snow,
slippery when wet

ESF or PIREP: Medium

FCOM LIM-AG-OPS P 8/10

A

148’+: 25kts

100’-148’: 10kts

50
Q

Max Recommended Crosswind on runway with
Water (3mm-13mm),
Slush (3mm-13mm)

ESF or PIREP: Medium to Poor

FCOM LIM-AG-OPS P 8/10

A

148’+: 20kts

100’-148’: 10kts

51
Q

Max Recommended Crosswind on runway with
Ice (cold & dry)

ESF or PIREP: Poor

FCOM LIM-AG-OPS P 8/10

A

148’+: 15kts

100’-148’: 10kts

52
Q

Takeoff not recommended on the following runway conditions:

FCOM LIM-AG-OPS P 9/10

A

Wet Ice

Water on top of Compacted Snow

Dry Snow or Wet Snow over Ice

53
Q

Max Speed and flight phase for Configuration 1+F

FCOM LIM-AG-SPD P 1/6

A

215

TAKEOFF

54
Q

Max Speed and flight phase for Configuration 2

FCOM LIM-AG-SPD P 1/6

A

200 kts

TAKEOFF/APPROACH

55
Q

Max Speed and flight phase for Configuration 3

FCOM LIM-AG-SPD P 1/6

A

185 kts

TAKEOFF/APPROACH/LANDING

56
Q

Max Speed and flight phase for Configuration Full

FCOM LIM-AG-SPD P 1/6

A

177 kts

LANDING

57
Q

Max Speed and flight phase for Configuration 0

FCOM LIM-AG-SPD P 1/6

58
Q

Minimum Control Speed for Landing (VMCL)

FCOM LIM-AG-SPD P 3-5/6

A

All 319-111: 108 kts

All 319-112: 111 kts

All 320: 113 kts

59
Q

Taxi Speed when > 167,550 lb

FCOM LIM-AG-SPD P5/6

A

Do not exceed 20kts during a turn

60
Q

Max T/O Weight Limitation at KDCA N231NV, N232NV

FCOM LIM-AG-WHT P 3/4

A

162,038 lb

61
Q

With passengers on board, max time limit recommended without air conditioning supply:

FCOM LIM-AIR P 1/4

A

20 minutes

62
Q

During ground operations and depending on the OAT, the flight crew must limit the time that the Aircraft Electric Power Supply is used, temp and time are:

FCOM LIM-AIR P 1/4

A

OAT <= 49C (120F) = no limitation

49C (121F) to 55C (131F) = 2 hours

63
Q

Max Positive Differential Pressure

FCOM LIM-AIR P 1-3/4

64
Q

Max Negative Differential Pressure

FCOM LIM-AIR P 1-3/4

65
Q

Safety Relief Valve Pressure Setting

FCOM LIM-AIR P 1-3/4

66
Q

FMGS lateral and vertical navigation is certified for:

FCOM LIM-AFTS-10 P 2/6

A
  • After takeoff, enroute, and terminal area operations
  • Navigation within RNAV/RNP airspace
  • Missed approach procedures
  • Instrument approach procedures
    (except ILS, LOC BC, LDA and final approaches)
67
Q

What do you need to do if GPS PRIMARY LOST is desplayed on the ND and MCDU?

A

Navigation accuracy remains sufficient for RNP operations provide that the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.

(note:
Use appropriate remaining AP/FD.
Discontinue approach if GPS PRIMARY LOST is on both displays.
Ref: PRO-NOR-SOP-19-C P 9/20)

68
Q

(A319 only) If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes:

LIM-AFS-10 P 4/6

A

FINAL APP
NAV V/S
NAV/FPA
Only FD use is permitted

69
Q

Max Altitude for APU Battery Restart

70
Q

Max N speed

FCOM LIM-APU P 1/6

71
Q

Max EGT for APU start

FCOM LIM-APU P1/6

A

1038°C N227NV

varies by aircraft 900-1090°C

72
Q

Max EGT for APU running

FCOM LIM-APU P1/6

A

725°C N227NV

varies by A/C 682-725°C

73
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
74
Q

Max altitude APU Operation Electric Only

FCOM LIM-APU P 2-4/6

75
Q

Max altitude APU Operation Electric Power and Bleed Power

FCOM LIM-APU P 2-4/6

76
Q

Max Pressure Altitude for APU ground operation

FCOM LIM-APU P 2-4/6

A

9,200’ or 14,500’

depending on the plane

77
Q

Max altitude for APU to assist engine start

FCOM LIM-APU P 4-5/6

78
Q

APU Max altitude for air conditioning and pressurization (single pack ops)

FCOM LIM-APU P 4-5/6

79
Q

APU Max altitude for air conditioning and pressurization (dual pack ops)

FCOM LIM-APU P 4-5/6

80
Q

When is max reverse not allowed

FCOM LIM-ENG P 3/4

A

* in flight
* for backing
* below 70 kts

note: idle reverse is permitted down to a/c stop

81
Q

Max NWS angle

FCOM LIM-LG P 1/2

82
Q

When using ADS-B Out for ATC separations services, what must be operational?

LIM-NAV P 2/2

A

*TCAS
*ACARS

83
Q

Minimal runway width:

84
Q

Max Crosswind for Takeoff and Landing on a Dry runway?

A

All runways: 38kts

148’+: 38kts

100’-148’: 38kts

Airbus G4 Oral Prep (LB) (25 decks)

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