Limitations A320 Flashcards

1
Q

Max wind for Takeoff and Landing

A

50 Kts (Including gusts)

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2
Q

Max x-wind for Takeoff and Landing

A

35 Kts (Including gusts)

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3
Q

Max x-wind for Landing Vis <4000 or 3/4

A

15 Kts

10 Kts single engine

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4
Q

Max x-wind for Auto Land Vis >= 4,000 or 3/4

A

20 Kts

10 Kts single engine

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5
Q

Max tailwind component for takeoff (A320, A321 with IAE Engines)

A

10 Kts

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6
Q

Max tailwind component for takeoff (A319 and A320, A321 with CFM Engines)

A

15 Kts

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7
Q

Max tailwind component for landing ( non sharklet )

A

10 Kts

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8
Q

Max tailwind component for landing ( sharklet )

A

15 Kts

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9
Q

Max runway slope ( up hill, downhill )

A

+2.0%up, -2.0% down

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10
Q

Max operating altitude

A

39,000 feet

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11
Q

Maximum takeoff and landing pressure altitude ( except A319 with Sharklets )

A

9,200 feet

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12
Q

Maximum takeoff and landing pressure altitude ( A319 with Sharklets )

A

14,100 feet

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13
Q

Maximum takeoff and landing pressure altitude

A
  • 1,000 feet
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14
Q

Maximum operating altitude with flaps and/or flaps extended

A

20,000 feet

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15
Q

Maximum gear extension altitude

A

25,000 feet

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16
Q

Maximum operating airspeed ( SL to FL 246 )

A

350 Kts

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17
Q

Maximum operating Mach number ( > FL 246 )

A

.82M (Mmo)

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18
Q

Tire limit groundspeed

A

195 KIAS

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19
Q

Maximum taxi speed

A

30 Kts (A)

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20
Q

Maximum taxi speed for 90 degree turn

A

10 Kts (A)

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21
Q

Maximum airspeed for windshield wiper operation

A

230 KIAS (M)

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22
Q

Maximum airspeed with flight deck window open

A

200 KIAS

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23
Q

Maximum gear extension speed (Vlo)

A

250 KIAS

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24
Q

Maximum gear extended speed (Vle)

A

280 KIAS

25
Q

Maximum gear retraction speed (Vlo)

A

220 KIAS

26
Q

Definition of Icing Conditions

A
  • OAT (on the ground and for takeoff) or TAT (inflight) is 10c or below, and
  • Visible moisture in any form is present such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals or
  • When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by engines, freeze on engines, nacelles, or engine sensor probes.
27
Q

Engine Anti-Ice System

A

Engine anti-ice must be on during all ground and flight ops when icing conditions exist except during climb and cruise when the temperature is below -40°C SAT
- Engine anti-ice must be on prior to and during descent in icing conditions, including temperatures below -40°C SAT

28
Q

Maximum Flap Operating Speeds A319/320

A
1 -   230
1+F - 215
2 - 200
3 - 185
Full - 177
29
Q

Maximum Flap Operating Speeds A321

A
1 -   235
1+F - 225
2 - 215
3 - 195
Full - 190
30
Q

Cargo Compartment

A

No animals in cargo compartment except A321T

31
Q

Maximum brake temp for takeoff

A

300℃

32
Q

Minimum height for use of autopilot after takeoff in SRS mode

A

100 feet AGL

33
Q

Minimum height for use of autopilot ( Enroute )

A
500 feet (A319, A320)
900 feet (A320)
34
Q

Minimum height for use of autopilot Non-ILS

A

250 feet RA

35
Q

Minimum height for use of autopilot ILS ( non-autoland with CAT 2 CAT 3 SINGLE, CAT 3 DUAL annunciated on the FMA)

A

80 feet AGL

36
Q

Minimum height for use of autopilot ILS ( non-autoland with CAT 1 on the FMA)

A

160 feet AGL

37
Q

Minimum height for use of autopilot after a Manual Go-around in SRS mode

A

100 feet AGL

38
Q

Reverse Thrust

A

Maximum reverse thrust should not be used below 70 KIAS (or when indicated airspeed starts to fluctuate). Idle reverse is permitted to aircraft stop.

39
Q

APU Starter Limit

A

After 3 cycles wait 60 minutes before attempting 3 more cycles.

40
Q

Max Altitude for APU bleed air operation

A

20,000 feet

- Air bleed extraction for wing anti-icing is not permitted

41
Q

Engine start cycles for CFM engines

A

4 consecutive 2 min cycles each

- 15 minute cooling after 4 cycles

42
Q

Engine start cycles for IAE engines

A

3 consecutive cycles, two of 2 minutes duration followed by a third of one minute.
- 15 sec between start attempts 30 minute cooling period following 3 start attempts (or 4 min continuous cranking)

43
Q

Maximum headwind for autoland A320, A321

A

30 knots

44
Q

Turbulence Penetration Speed (A319, A320)

  • at or above 20,000 ft
  • below 20,000 ft
A

275 KIAS/.76M

250 KIAS

45
Q

Turbulence Penetration Speed (A321)

  • at or above 20,000 ft
  • below 20,000 ft
A

300 KIAS

270 KIAS

46
Q

Wing tanks A319/A320/A321

A

27,500 lbs

47
Q

Center tanks A319/A320/A321

A

14,500 lbs

48
Q

Additional Center tank A321

A

10,500 lbs

49
Q

Total usable fuel A319/A320

A

42,000 lbs

50
Q

Total usable fuel A321

A

52,500 lbs

51
Q

Maximum headwind for autoland A319

A

20 knots

15 knots Single engine

52
Q

Maximum tailwind for autoland A320/A321

A

10 Knots

53
Q

Max tailwind auto land A319 shark let below 5,750 and full config

A

10 Knots

54
Q

Max tailwind auto land A319 all other configurations

A

5 Knots

55
Q

Max Ramp weight A319

A

167,330

56
Q

Max Ramp weight A320

A

170,637

57
Q

Max Ramp weight A321 w/o sharklets

A

205,911

58
Q

Max Ramp weight A321 with sharklets

A

207,014