Limitations (Rev 11)

Question 0

Max wind for takeoff and landing

Answer 0

50 kts (U)

Question 1

(Non-memory item)

What are the max landing weights?

Answer 1

137/142/171

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

Question 2

Max XW for takeoff and landing

Answer 2

29G35 kts (U)

Question 3

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

Answer 3

15 kts (U)

Question 4

Max XW (including gust) for Autoland

Answer 4

20 kts

Question 5

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

Answer 5

10 kts

Question 6

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

Answer 6

15 kts

Question 7

Max operating altitude

Answer 7

39,000’ (U)

Question 8

Max TW for landing (Non-Sharklet)

Answer 8

10 kts

Sharklet is 15 kts

Question 9

Max flap and/or slat extension altitude

Answer 9

20,000’

Question 10

Max gear extension altitude

Answer 10

25,000’

Question 11

Max operating airspeed (SL to FL246)

Answer 11

350 KIAS

Question 12

Max operating Mach number (>FL246)

Answer 12

.82M (Mmo)

Question 13

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

Answer 13

10°C or below

Question 14

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 ________

Answer 14

Below -40°C SAT

Question 15

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

Answer 15

Below -40°C SAT

Question 16

(Non-memory item)

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

Answer 16

+1.0 psi

Question 17

(Non-memory item)

Max brake temp for takeoff

Answer 17

300°C

Question 18

(Non-memory item)

Max taxi speed

Answer 18

30 kts (U)

Question 19

(Non-memory item)

Max taxi speed for 90° turn

Answer 19

10 kts (U)

Question 20

(Non-memory item)

Min Jet A fuel temp

Answer 20

-36°C

Question 21

(Non-memory item)

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

Answer 21

7 kts

Question 22

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

Answer 22

3 kts; 30°

Question 23

Min height for Autopilot use after takeoff in SRS mode

Answer 23

100’ AGL

Question 24

(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)

Answer 24

80' AGL

Question 25

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

Answer 25

160' AGL

Question 26

(Non-memory item) | Min height for Autopilot use after manual Go Around in SRS mode

Answer 26

100' AGL

Question 27

(Non-memory item) | The use of OPEN DES is prohibited ______

Answer 27

Inside FAF or below 1000' AGL during visual approach

Question 29

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

Answer 29

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

Question 30

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

Answer 30

10 kts | A319 Sharklet 5 kts

Question 30

(Non-memory item) | The aircraft is certified for an engine-out CAT III Single approach and autoland provided _________

Answer 30

Engine-out procedures are completed prior to 1000' AFL

Question 31

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

Answer 31

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

Question 32

(Non-memory item) | A320 engine-out autolands are authorized in CONF ______ only

Answer 32

FULL

Question 33

(Non-memory item) | A319 and A321 engine-out autolands are authorized in CONF ______

Answer 33

3 or FULL

Question 34

(Non-memory item) | With one engine inop, the use of the remaining thrust reverser is permitted provided _______

Answer 34

Not more than idle reverse thrust is used XW is not more than 15 kts

Question 35

(Non-memory item) | Time limit for TOGA thrust

Answer 35

5 mins (2E) 10 mins (1E)

Question 36

(Non-memory item) | Start limits for CFM engines

Answer 36

4 consecutive cycles w/2 minute max duration 15 min cooling period after 4 start attempts

Question 37

(Non-memory item) | Start limits for IAE engines

Answer 37

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

Question 38

Reverse Thrust is for ______ use only

Answer 38

Ground

Question 39

(Non-memory item) | Max reverse thrust should not be used below _____

Answer 39

70 KIAS or when IAS starts to fluctuate Idle reverse is permitted to aircraft stop

Question 40

(Non-memory item) | Min oil quantity for dispatch is ________

Answer 40

13 quarts (U)

Question 41

(Non-memory item) | The ____ tank fuel must be emptied before ______ are emptied unless the ______ tank fuel is treated as ballast

Answer 41

Center; wing; center (U)

Question 42

(Non-memory item) | Takeoff using ______ fuel is prohibited

Answer 42

Center tank

Question 43

(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

Answer 43

200 (U)

Question 44

(Non-memory item) | Min height for use of the Autopilot on a non-ILS approach

Answer 44

DA, DDA, or MDA

Question 45

(Non-memory item) | After ___ APU starter motor duty cycles, wait ____ before attempting ________

Answer 45

3; 60 minutes; 3 more cycles

Question 46

(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

Answer 46

90 kVA; below 25,000'

Question 47

(Non-memory item) | Max altitude for APU bleed operation

Answer 47

20,000' | use for wing AI is not permitted

Question 48

(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

Answer 48

LOW OIL LEVEL; 10 hours

Question 49

(Non-memory item) | Resetting a tripped ________ or ________ CB is prohibited

Answer 49

Fuel boost pump or Fuel indicating system

Question 50

(Non-memory item) | Max continuous load per generator

Answer 50

100% (90 kVA)

Question 51

(Non-memory item) | Max continuous load per TRU

Answer 51

200 A

Question 52

(Non-memory item) | Max difference between altimeters and a known airport altitude

Answer 52

+/- 75'

Question 53

(Non-memory item) | Max difference between altimeters on PFD 1 and 2

Answer 53

20'

Question 54

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

Answer 54

200'

Question 55

Undue Activation of Alpha Protection

Answer 55

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