Limitations Flashcards

1
Q

Maneuvering Load Limits*

A

Clean: -1 to 2.5G
Other: 0 to 2G

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2
Q

A319/320 Wingspan*

A

111 ft, 10 in

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3
Q

A320 Sharklet/321 Sharklet Wingspan

A

117 ft, 5 in

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4
Q

Max Pitch Attitude with L/G Struts Compressed

A

319 - 13.9 deg
320 - 11.7
321 - 9.7

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5
Q

Max Certified Altitude

A

FL 398

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6
Q

Mean Runway Slope*

A

+/- 2%

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7
Q

Max Runway Altitude*

A

9,200 ft

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8
Q

Nominal Runway Width*

A

45 m (148 ft)

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9
Q

Max Demonstrated X-Wind (T/O & Landing)

A

38 kt including gusts

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10
Q

Max Tailwind for T/O

A

15 kt

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11
Q

Max Tailwind for Landing

A

10 kt

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12
Q

Max Wind for Pax Door Operation*

A

65 kt

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13
Q

Max Speed with Cockpit Window Open*

A

200 kts

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14
Q

Vmo / Mmo*

A

350 kts / M .82

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15
Q

Vle*

A

280 kts / M .67

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16
Q

Vlo Extension*

A

250 kts / M .60

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17
Q

Vlo Retraction*

A

220 kts / M .54

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18
Q

Max Altitude for L/G Extension

A

FL 250

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19
Q

Max Tire Speed*

A

195 kts

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20
Q

When taxi weight is higher than _____, do not exceed _____ in a turn.

A

167,550 lbs / 20 kts

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21
Q

Wipers Max Operating Speed

A

230 kts

22
Q

319 Max Landing Weight*

A

137,788 lbs

23
Q

320 Max Landing Weight*

A

145,505 lbs

24
Q

320 NEO Max Landing Weight*

A

148,591 lbs

25
Q

321 Max Landing Weight*

A

171,519 lbs

26
Q

Do not use air from APU Bleed and HP Air Start Unit at the same time

A

…to prevent adverse effect on the bleed system

27
Q

Max/Min Differential Pressure*

A

+9/-1 psi

28
Q

Min Height for Autopilot

A

T/O & G/A - 100 ft and 5 secs after liftoff
Cat 1 ILS - 160 ft
Cat 2/3 ILS - 0 ft (autoland)
Non-Precision (F-G/S, Final App, V/S, FPA) - 250 ft
Circling - 600 ft
All Other Phases - 500 ft (319/320)
900 ft (321)

29
Q

Use of the AP or FD in OPEN DES or DES mode is not permitted in approach unless….

A

FCU Altitude is set at or above the higher of:
Mins or 500 ft (319/320)
Mins or 900 ft (321)

30
Q

NAV mode in the terminal area requires:*

A

GPS Primary or
High Accuracy and Required RNP or
Cross check Navaid Raw Data

31
Q

Use of AP is not permitted on a single-engine, non-precision approach in the following modes:*

A

Final App
Nav V/S
Nav FPA

Only FD is permitted

32
Q

APU Starter Limits

A

After 3 attempts, 60 mins off

33
Q

Max Time and EGT during Engine Start*

A

319/320 - 635 C
NEO - 1,083 C
321 - 635 C

34
Q

Max Time and EGT during T/O & G/A*

A

319/320 - 5 min / 635 C (10 min single engine)
NEO - 5 min / 1,083 C (10 min single engine)
321 - 5 min / 650 C (10 min single engine)

35
Q

Max Time and EGT with MCT*

A

319/320 - unlimited/610 C
NEO - unlimited/1,043 C
321 - unlimited/610 C

36
Q

Min Oil Temp for Engine Start

A

-40 C

37
Q

Min Oil Temp to Exceed Idle

A

-10 C

38
Q

NEO Min Oil Pressure*

A

65 psi

39
Q

Non-NEO Starter Limits

A

1 attempt per cycle,
15 secs between cycles,
30 mins cooling after 3 cycles or 5 mins of continuous crank,
2 min max cycle for Manual Start
5 min max cycle for dry crank
Starter must not be run when N2 is above 10% on ground or 18% in flight

40
Q

NEO Starter Limits

A

2 attempts per cycle
35 secs between cycles (every 2 attempts)
15 mins cooling after 3 cycles or 15 mins continuous or cumulative crank
Starter must not be run when N2 is above 20%

41
Q

Max Speed for Thrust Reverse

A

Full Reverse - 70 kts

Idle Reverse - Full Stop

42
Q

Thrust Rating for T/O on Contaminated Runway

A

TOGA

Flex is not permitted

43
Q

Max Crosswind for Engine Start

A

35 kts

44
Q

Max Altitude for Slats/Flaps

A

FL200

45
Q

Jet A Fuel, if TAT reaches _____, monitor that fuel temp remains above _____

A

TAT -34 C

Fuel Temp above -36 C

46
Q

Max Fuel Imbalance 319/320

A

T/O - 1,102 lbs

In Flight & Landing - 3,306 lbs*

47
Q

Max Fuel Imbalance 321

A

T/O - 882 lbs

In Flight & Landing - 2,910 lbs*

48
Q

Max Brake Temp for T/O

A

300 C (fans off)

49
Q

321 NEO Max Landing Weight

A

174,606 lbs

50
Q

Do not use air conditioned air from the packs and the LP air conditioning unit at the same time…

A

To prevent adverse effect on the air conditioning system