Limitations Flashcards

1
Q

**Max Landing Weight **

A

320: Classic/Sharklet: 145,505 lbs

319: 137,788 lbs
321: 171,519 lbs

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2
Q

Max Zero Fuel Weight

A

320: Classic/Sharklet: 137,788 lbs

319: 128,970 lbs
321:
Classic/Sharklet: 162,701 lbs

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3
Q

Max field elevation for Autoland

A

6500 ft

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4
Q

Max FLEX temp for Takeoff

A

ISA +55°C

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5
Q

Max Certified Altitude

A

FL398

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6
Q

Turbulent Air Penetration Speeds

A
  • At or below FL150: 250 knots
  • FL150-FL310: 275 kts
  • Above FL310: .76M
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7
Q

Max runway slope

A

+- 2%

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8
Q

Max Runway altitude

A

9,200’

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9
Q

Max Demonstrated Crosswind

A

38 kts (gust included)

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10
Q

Max Tailwind for takeoff

A

15 kts

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11
Q

Max Tailwind for landing

A

10 kts

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12
Q

Max wind speed for passenger door operation

A

65 kts

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13
Q

Max Landing Gear extended Speed (Vle)

A

280 kts/M.67

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14
Q

Max Landing Gear Extension (Vlo extend)

A

250 kts

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15
Q

Max Landing Gear Retraction speed (Vlo retract)

A

220 kts

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16
Q

Max atitude landing gear can be extended

A

FL250

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17
Q

Max airspeed windshield wipers can be used

A

230 kts

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18
Q

Max taxi speed to make a turn considering weight

A

If weight is greater than 167,550 lbs Max turning speed is 20 kts

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19
Q

Max positive cabin differential

A

+8.6 psi

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20
Q

Max negative cabin pressure differential

A

-1.0 psi

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21
Q

Min height for use of autopilot for takeoff in SRS mode

A

100’ AGL

22
Q

Min height for use of autopilot for a straight-in non-precision approach

A

Applicable minimums

23
Q

Min height for use of autopilot for a circling approach

A

Applicable minimums -100 ft

24
Q

Min height for use of autopilot for an ILS approach where CAT 2 or CAT 3 is not displayed on the FMA

A

160 ft AGL

25
Q

Min height for use of autopilot for Go-Around (AP or FD engagement)

A

100 ft AGL

26
Q

Min height for use of autopilot for all other phases of flight

A

500 ft AGL

27
Q

Max Taxi Weight

A

Classic: 170,637 lbs
Sharklet: 172,842 lbs

319: 167,330 lbs
321:
Classic: 205,911 lbs
Sharklet: 207, 014 lbs

28
Q

Max Takeoff Weight

A

Classic: 169,755 lbs
Sharklet: 171,960 lbs

319: 166,448 lbs
321:
Classic: 205,029 lbs
Sharklet: 206,132 lbs

28
Q

Use of the AP or FD in OPEN DES or DES mode is not permitted in approach, unless the FCU altitude is set at or above

A

Highest of:

319/320: Minimum or 500 ft
321: Minimum or 900 ft

29
Q

Max brake temperature for takeoff

A

300°C

30
Q

APU starter limit

A

After 3 starter motor duty cycles, must wait 60 min before attempting 3 more cycles

31
Q

Max altitude APU bleed air if both PACKs are operating

A

15,000’

32
Q

Max altitude for APU bleed if one PACK is operating

A

FL200

33
Q

Can APU bleed air be used for wing anti-ice?

A

No

34
Q

Max altitude APU can be started using battery power

A

FL250

35
Q

Min Oil temperature for starting

A

-40°C

36
Q

Min oil temperature before exceeding idle thrust

A

-10°C

37
Q

Min oil quantity

A

11 qts +estimated consumption (~.3 qts/hr)

38
Q

Engine Starter limits

A

Cycle 1-2………2 min each
Cycle 3………….1 min

15 second resting period between each attempt

39
Q

Engine cooling period, following 3 start attempts or 4 minutes of continuous cranking

A

30 minutes

40
Q

No running engagement of the starter when

A

N2 is above
10% on ground; or
18% in flight

41
Q

Max crosswind for engine start

A

35 kts

42
Q

Min speed for Max thrust reverse

A

70kts

43
Q

When is a reduced thrust takeoff not permitted?

A

Contaminated Runway

44
Q

Nominal Runway Width

A

148 ft
Note: (A319, A320, A321 Sharklet can operate to runways as narrow as 98 ft when operated in accordance with the “Operations on Narrow Runways” procedure.)

45
Q

Max crosswind on wet or contaminated runways

A

Damp/wet: 38 kts

Slush/Dry snow/ wet snow of 1/8”: 29 kts
Compacted snow if OAT at or below -15°C: 29 kts

Dry snow(1/8"-4")/wet snow(1/8"-6/5")/slippery when wet: 25kts
Compacted snow OAT above -15°C: 25 kts

Water/Slush(1/8”-1/2”): 20kts

Ice (cold & dry): 15kts

46
Q

Max Tire Speed

A

195 kts

47
Q

Max Cockpit Window Open

A

200 kts

48
Q

Air conditioning with LP Ground Unit

A

Do not use conditioned air simultaneously from PACKS and LP ground unit ( to avoid chattering of non-return valves)

49
Q

Is the use of autopilot permitted on Non-Precision Approaches with Engine Out?

A

320: yes

319/321: NO

50
Q

Air Conditioning with HP Ground Unit

A

Do not use HP ground unit when the APU is supplying bleed air to avoid bleed system damage