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A320 Limitations > Limitations > Flashcards

Limitations Flashcards

1
Q

NAV mode may be used in the terminal area, provided:

A
  • GPS PRIMARY
    or
  • The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed
    or
  • FMS navigation is cross-checked with NAVAID raw data
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2
Q

Runway Slope (mean)

A

+/-2%

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3
Q

Max crosswind for start

A

35kts

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4
Q

Max operating altitude with slats and/or flaps extended is

A

20,000ft

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5
Q

Minimum Height For Use Of Autopilot

Take off with SRS

A

100 ft AGL.
Note: Takeoff with SRS mode - An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff.

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6
Q

Minimum Height For Use Of Autopilot

ILS approach when CAT 2 or CAT 3 is not displayed on the FMA

A

160 ft AGL

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7
Q

Minimum Height For Use Of Autopilot

Straight-in non-precision approach

A

Applicable Minimum

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8
Q

Maximum wind for passenger door operation

A

65kts

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9
Q

Takeoff and GA (TOGA and FLEX)

Thrust Setting/EGT Limits

A

Takeoff and GA (TOGA and FLEX)
319 and 320 / 321 / NEO

635 °C / 650 °C / 1,083°C

5 min (10 min engine failure.)

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10
Q

Maximum brake temperature for takeoff (brake fans (if installed) off)

A

300 C

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11
Q

RunwayAltitude

A

9,200ft

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12
Q

NominalRunwayWidth

A

45m(148ft)

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13
Q

VLE

A

280kts (M .67)

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14
Q

Oil Temperature (CEO)

A

Starting
-40 °C

Above Idle
-10°C

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15
Q

APU Starter

A

After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.

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16
Q

Minimum Height For Use Of Autopilot

UseoftheAPorFDinOPENDESor DES mode is not permitted in approach, unless the FCU altitude is set at or above:

A

Highest of:

Minimums or 500 ft (A319/A320) Minimum or 900 ft (A321)

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17
Q

Fuel Temp

A

For JET A only, if TAT reaches -34C , monitor on FUEL SD page that fuel temperature remains higher than -36C

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18
Q

Reverser Limits

A

Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.

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19
Q

VLO (extension)

A

250kts (M .60)

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20
Q

Cabin Pressure
• Maxpositivedifferentialpressure
• Maxnegativedifferentialpressure

A
  1. 0psi

- 1.0psi

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21
Q

Max Landing (320)

22
Q

Max Landing (657-687)

23
Q

MCT

Thrust Setting/EGT Limits

A

MCT
CEO / NEO

610 °C / 1,043°C

24
Q

Max Taxi speed (A320CEO)

A

When the taxi weight is higher than 67,550lbs (76,000kg): Caution: Do not exceed a taxi speed of 20 kt during a turn.

25
Q

Non-Precision Approaches with Engine-Out (319 and 657-668, 670, 671)

A 
If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes: 
FINAL APP
NAV V/S
NAV/FPA.
Only FD use is permitted.
26
Q

Minimum Height For Use Of Autopilot

Circling Approach

A

100 feet below Applicable Circling Minimums

27
Q

Max Landing (502-536)

A

137,788 lb

28
Q

Minimum Oil Pressure (901-905)

29
Q

Max Alt for landing gear extended

30
Q

VLO (retraction)

A

220kts (M .54)

31
Q

Fuel Imbalance, Inner tanks when one is full

A

TO / Flight&Landing
319 and 320s: (At TO / Flight and Landing)
1,102 / 3306

321:
882 / 2910

32
Q

Minimum Height For Use Of Autopilot

All other phases

A

500 ft AGL (A319/A320) 900 ft AGL (A321)

33
Q

Maximum Certified Altitude

34
Q

Max speed for Windshield Wipers

35
Q

STARTING (On Ground and Inflight)

Thrust Setting/EGT Limits

A

STARTING
CEO / NEO

635 °C / 1,083°C

36
Q

Wingspans

A

Non-Sharklet
111feet,10inches

Sharklet
117feet,5inches

37
Q

Maximum demonstrated crosswind

A

38kts (gust included)

38
Q

Reduced Thrust Takeoff Limits

A

FLEX takeoff is not permitted on contaminated runways

39
Q

Max crosswind with CAT II and III

A

Crosswind: 15 kts

40
Q

Max tire speed

41
Q

APU With HP Ground 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.

42
Q

Starter Limitations

A

ALL CEO / NEO:

One Cycle = 1 / 2 consecutive start attempts

(CEO)Man start, 2 mins max start / 5 mins crack

For Ground Starts (auto or man), between cycle pause: 15 s / 35 s

After 3 cycles or 5 / 15 min continuous cranking (or cumulated NEO)
Cooling Period = 30 min / 15 min

Do not start, when
N2 is above 10% GND, 18 % FLT / 20%

43
Q

Tailstrike Pitch Attitudes

A

L/G Struts Compressed
319 - 13.9 degrees
320 - 11.7 degrees
321 - 9.7 degrees

44
Q

Max tailwind for:
Takeoff
Landing

A

Takeoff - 15kts

Landing - 10kts

45
Q

APU Bleed use with 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.

46
Q

Packs use with the LP Air Conditioning Unit

A

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.

47
Q

What is the reduced usable fuel capacity of the Center Tank on 697 and 698 (Invicta-FRS system)

A

reduced usable capacity of up to 42.9 gallons

48
Q

ELAC Functions

A

Normal Elevators
Normal Ailerons
Normal Pitch and Roll

Alternate Pitch

Direct Pitch and Roll

Abnormal Attitude
Aileron Droop
Autopilot orders

49
Q

SEC Functions

A

Normal Roll

Alternate Pitch

Direct Pitch and Roll

Abnormal Attitude
Speed Brakes

50
Q

FAC Functions

A

Rudder Limitations
Turn Coordination
Rudder Dampening
Rudder Trim

Aircraft envelope

Windshear

Low Energy Warning

A320 Limitations (7 decks)

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