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A319/320/321 > Limitations (Rev 11) > Flashcards

Limitations (Rev 11) Flashcards

0
Q

Max wind for takeoff and landing

A

50 kts (U)

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1
Q

(Non-memory item)

What are the max landing weights?

A

137/142/171

A319 137,788
A320 142,198
A321 171,519

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2
Q

Max XW for takeoff and landing

A

29G35 kts (U)

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3
Q

Max XW for landing with vis <4000 or 3/4

A

15 kts (U)

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4
Q

Max XW (including gust) for Autoland

A

20 kts

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5
Q

Max TW for takeoff (A320/321 with IAE engines)

A

10 kts

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6
Q

Max TW for takeoff (All A319 and A320/321 with CFM engines)

A

15 kts

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7
Q

Max operating altitude

A

39,000’ (U)

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8
Q

Max TW for landing (Non-Sharklet)

A

10 kts

Sharklet is 15 kts

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9
Q

Max flap and/or slat extension altitude

A

20,000’

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10
Q

Max gear extension altitude

A

25,000’

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11
Q

Max operating airspeed (SL to FL246)

A

350 KIAS

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12
Q

Max operating Mach number (>FL246)

A

.82M (Mmo)

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13
Q

Icing conditions exist when OAT (on ground) or TAT (inflight) is __________ and visible moisture is present

A

10°C or below

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14
Q

Engine anti-ice must be on during all ground and flight ops when icing conditions exist or are anticipated, except during climb and cruise when the temp is ________

A

Below -40°C SAT

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15
Q

Engine anti-ice must be on prior to and during descent in icing conditions, including temperatures __________

A

Below -40°C SAT

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16
Q

(Non-memory item)

Open the Ram Air Inlet only if differential pressure is less than ________

A

+1.0 psi

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17
Q

(Non-memory item)

Max brake temp for takeoff

A

300°C

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18
Q

(Non-memory item)

Max taxi speed

A

30 kts (U)

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19
Q

(Non-memory item)

Max taxi speed for 90° turn

A

10 kts (U)

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20
Q

(Non-memory item)

Min Jet A fuel temp

A

-36°C

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21
Q

(Non-memory item)

If one tire is deflated on one or more gears, the speed should be limited to ________ when turning

A

7 kts

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22
Q

(Non-memory item)
If two tires are deflated on the same main gear, speed should be limited to ________ and the NWS angle limited to ________

A

3 kts; 30°

23
Q

Min height for Autopilot use after takeoff in SRS mode

A

100’ AGL

24
Q

(Non-memory item)

Min height for Autopilot use on an ILS (non-Autoland with CAT 2, CAT 3 SINGLE, or CAT 3 DUAL on FMA)

A

80’ AGL

25
Q

(Non-memory item)

Min height for Autopilot use on an ILS (non-Autoland with CAT 1 on FMA)

A

160’ AGL

26
Q

(Non-memory item)

Min height for Autopilot use after manual Go Around in SRS mode

A

100’ AGL

27
Q

(Non-memory item)

The use of OPEN DES is prohibited ______

A

Inside FAF or below 1000’ AGL during visual approach

29
Q

Max HW for Automatic Approach, Landing, and Roll Out (including gusts) (except A319 Sharklet)

A

30 kts

A319 Sharklet: 2E 20 kts, 1E 15 kts

30
Q

Max TW for Automatic Approach, Landing, and Roll Out (including gusts) (except A319 Sharklet)

A

10 kts

A319 Sharklet 5 kts

30
Q

(Non-memory item)

The aircraft is certified for an engine-out CAT III Single approach and autoland provided _________

A

Engine-out procedures are completed prior to 1000’ AFL

31
Q

Max XW for Automatic Approach, Landing, and Roll Out (including gusts) with vis 4000 or 3/4 or greater (except A319 Sharklet)

A

20 kts

A319 Sharklet: 2E 20 kts, 1E 10 kts

32
Q

(Non-memory item)

A320 engine-out autolands are authorized in CONF ______ only

A

FULL

33
Q

(Non-memory item)

A319 and A321 engine-out autolands are authorized in CONF ______

A

3 or FULL

34
Q

(Non-memory item)

With one engine inop, the use of the remaining thrust reverser is permitted provided _______

A

Not more than idle reverse thrust is used

XW is not more than 15 kts

35
Q

(Non-memory item)

Time limit for TOGA thrust

A

5 mins (2E)

10 mins (1E)

36
Q

(Non-memory item)

Start limits for CFM engines

A

4 consecutive cycles w/2 minute max duration

15 min cooling period after 4 start attempts

37
Q

(Non-memory item)

Start limits for IAE engines

A

3 consecutive cycles w/2 minute max duration on first two starts followed by 1 minute max duration on third

Pause 15 sec between start attempts

30 min cooling period after 3 start attempts or 4 min continuous cranking

38
Q

Reverse Thrust is for ______ use only

A

Ground

39
Q

(Non-memory item)

Max reverse thrust should not be used below _____

A

70 KIAS or when IAS starts to fluctuate

Idle reverse is permitted to aircraft stop

40
Q

(Non-memory item)

Min oil quantity for dispatch is ________

A

13 quarts (U)

41
Q

(Non-memory item)

The ____ tank fuel must be emptied before ______ are emptied unless the ______ tank fuel is treated as ballast

A

Center; wing; center (U)

42
Q

(Non-memory item)

Takeoff using ______ fuel is prohibited

A

Center tank

43
Q

(Non-memory item)
On the A321, if center tank is not full, dispatch with more than ______ lbs total fuel in both ACTs is prohibited, unless directed by an MEL

A

200 (U)

44
Q

(Non-memory item)

Min height for use of the Autopilot on a non-ILS approach

A

DA, DDA, or MDA

45
Q

(Non-memory item)

After ___ APU starter motor duty cycles, wait ____ before attempting ________

A

3; 60 minutes; 3 more cycles

46
Q

(Non-memory item)
In flight, the APU gen is limited to an AC load of _____ for flight altitudes ___________ with temps of ISA +20 and below

A

90 kVA; below 25,000’

47
Q

(Non-memory item)

Max altitude for APU bleed operation

A

20,000’

use for wing AI is not permitted

48
Q

(Non-memory item)
The APU may be started and operated even if the _________ ECAM advisory is displayed. MX action is required within the next ________ of APU operation

A

LOW OIL LEVEL; 10 hours

49
Q

(Non-memory item)

Resetting a tripped ________ or ________ CB is prohibited

A

Fuel boost pump or Fuel indicating system

50
Q

(Non-memory item)

Max continuous load per generator

A

100% (90 kVA)

51
Q

(Non-memory item)

Max continuous load per TRU

A

200 A

52
Q

(Non-memory item)

Max difference between altimeters and a known airport altitude

A

+/- 75’

53
Q

(Non-memory item)

Max difference between altimeters on PFD 1 and 2

A

20’

54
Q

Max allowable inflight difference between CA and FO PFD altitude displays for RVSM operations

A

200’

55
Q

Undue Activation of Alpha Protection

A

3 conditions:

  1. Continuous nose down pitch above Vls
  2. Alpha Max hides Alpha Prot strip while wings level
  3. Alpha Prot strip rapidly moves 30+ kts during maneuvers with AP on and speed brakes retracted

One ADR pb - KEEP ON
Two ADR pbs - OFF

A319/320/321 (2 decks)

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