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Limitations Flashcards

1
Q

VMO/MMO

A

350 KIAS/ .82M

FM 1.20.1

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2
Q

Maximum Operation Pressure Altitude
and temperature range

A

39,100 feet from -70°C to -30°C

FM 1.30.1

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3
Q

Maximum Landing Weight

A319
A320
NEO

A

A319 - 137.7
A320 - 142.2
NEO - 174.6

FM1.20.9

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4
Q

A319 Maximum Landing Weight

A

A319 - 137.7

FM 1.20.9

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5
Q

A320 Maximum Landing Weight

A

A320 - 142.2

FM 1.20.9

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6
Q

Maximum Tailwind Component

A319 Takeoff/Landing

A320 Takeoff/Landing
A320s N4901U and N1902U Takeoff

NEO Takeoff/Landing

A

A319
Takeoff/Landing - 10 knots

A320
Takeoff - 15 knots ( 10 knots N4901U and N1902U)
Landing - 10 knots

NEO
Takeoff - 15 knots
Landing - 15 knots

FM 1.20.9

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7
Q

Maximum Crosswind Component Dry Runway

Narrow Runway

A

Takeoff and Landing:
38 knots

Narrow Runway*:
38 knots

FM 1.20.10

  • Narrow Runway: < 148 ft but >= 100 ft (FM 1.20.8)
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8
Q

Severe Turbulence Operating Speeds

A

If anticipating severe turbulence, the PF should target .76 Mach while the PM references table on pg 1.20.4 Limitations for the best penetration speed

FM 1.20.4

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9
Q

Minimum Flight Deck Oxygen

If pressure does not allow for an observer, do you need an MEL

A

If oxygen is below 1250, reference the aircraft specific table

You do not need an MEL if pressure does not all for an observer

FM 1.30.2

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10
Q

Engine Anti-Ice Use Required

Ground Operations
Climb/Cruise
Descent/Approach

A

Ground Operations:
<= 10°C OAT and visible moisture*

Climb/Cruise:
<= 10°C TAT and >= -40°C SAT and visible moisture present

Descent/Approach:
<= 10°C TAT and visible moisture

  • Visible Moisture on ground: Any ramps, taxiways or runways where surface snow, standing water, or slush may be ingested by the engines or freeze on the engines, nacelles, or engine sensor probes OR clouds, fog/mist with vis <= 1 mile, rain, snow, sleet or ice crystals
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11
Q

Autopilot Minimum Engagement Height

After Takeoff
Non-ILS/GLS Approach with FINAL APP or FPA (non-NEO)
Nonautoland ILS with CAT 1 FMA
Nonautoland ILS with CAT 2 or 3 FMA
(NEO) Non-ILS/GLS approach with F-G/S

A

After Takeoff: 100 AGL
Non-ILS Approach: 250 AGL
Nonautoland ILS with CAT 1 FMA: 160 AGL
Nonautoland ILS with CAT 2 or 3 FMA: 80 AGL
(NEO) Non-ILS/GLS approach with F-G/S: 200 AGL

FM 1.30.8
When charted, mode reversion point is represented by the “M” in the chart profile. When not charted, the mode reversion is 50 ft AGL

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12
Q

Autopilot Minimum Engagement Height

After Takeoff

A

100 AGL

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13
Q

Autopilot Minimum Engagement Height

Non-ILS Approach

A

250 AGL or the missed approach point (whichever occurs earlier)

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14
Q

Autopilot Minimum Engagement Height

Nonautoland ILS with CAT 1 FMA

A

160 AGL

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15
Q

Autopilot Minimum Engagement Height

Nonautoland ILS with CAT 2 or 3 FMA

A

80 AGL

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16
Q

Autopilot Disengagement after Autoland (one or two autopilots)

A

Rollout

FM 1.30.10

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17
Q

Maximum EGT - Start

A

635°C

FM 1.30.11

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18
Q

Time between consecutive engine start attempts

Maximum Continuous Engagement (Cranking)

Max Start Attempt Time for Manual Start

A

First: 15 seconds
Second: 15 seconds
Third: 30 minutes

Max Crank Time: 5 minutes followed by 30 minutes off

For manual starts: observe 2-minute max start attempt

Start attempt timing is from start valve opening until closing. For automatic starts, the FADEC controls start attempt timing: follow ECAM for faults.

FM 1.30.13

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19
Q

Minimum Engine Oil Quantity Before Start

NEO exception

A

14.0 quarts*

If NEO, minimum oil quanity when >= -30°C before start

* If less than this, reference the aircraft specific table

FM 1.30.13

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20
Q

Maximum Flaps/Slats Extended Altitude

A

20,000 MSL

FM 1.30.14

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21
Q

Aircraft Approach Category

A

Straight-in Instrument Approaches: Cat C
Circling: Cat D

FM 1.30.18

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22
Q

Engine warm up time after start

Engine cool down before shutdown

A

If engine has been shutdown for > 2 hours:
5 min

If engine has been shutdown for <= 2 hours:
2 minutes
(ensures center tank pump test is complete)

Engine cooldown prior to shutdown:
3 minutes
(regardless of reverse setting on landing)

FM 3.50.1 / FM 3.210.3

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23
Q

Maximum landing gear extension speed (UAL)

FM 1.30.24

A

240 kts

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24
Q

Maximum landing gear retraction speed

FM 1.30.24

A

220

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25
Q

Maximum Landing Gear Extended Speed / Mach (VLE)

A

280 kts / .67M

26
Q

Max runway slope

A

+/-2°

27
Q

Max Pressure altitude for takeoff and landing

A

9200ft

28
Q

Aircraft Category
Straight-in
Circling

A

Straight-in: Cat C
Circling: Cat D

29
Q

APU Start Limits

FM Limitations 1.30.13

A

Between each start attempt: 1 min
After 3 consecutive attempts: 60 minutes

30
Q

APU Starting Altitudes
Using normal electrics
Using battery power only
One pack operation
For engine start
Two pack operation

FM Limitations 1.30.13

A

Using normal electrics: 39,000 ft (improved below 31,000)
Using battery power only: 25,000 ft
One pack operation: 20,000 ft
For engine start: 20,000 ft
Two pack operation: 15,000 ft

31
Q

Minimum APU Oil Quantity

A

ECAM

32
Q

Speed brake altitude limit

Speed brake speed limit with slats retracted

FM Limitations 1.30.15

A

Altitude Limit:
Do not use below 1000 ft AGL

In flight with slats retracted:
Do not use below 200 KIAS

33
Q

Best climb rate
Best climb angle

A

Best climb rate:
280 KIAS

Best climb rate:
Green Dot

34
Q

Flaps Speeds (319/320)

Flap Speeds (NEO)

A

319/320
1: 230
1+F: 215
2: 200
3: 185
4: 177

NEO
1: 243
1+F: 225
2: 215
3: 195
4: 185

35
Q

Max Landing Gear Extension Altitude

A

25,000 MSL

36
Q

Max brake temperature before takeoff

A

300° C

37
Q

Limits on use of OPEN DES or DES

A

Do not use OPEN DES or DES below:
- 1000 AGL
- MDA

38
Q

Contaminated runway thrust limitation

FM Limitations 1.20.7

A

Reduced thrust is prohibited

39
Q

Runways conditions in which operations are prohibited

FM Limitations 1.20.11

A
  1. Runway CC 0
  2. Control/Braking Action Nil
  3. Wet Ice
  4. Slush over ice
  5. Dry or wet snow over ice
  6. Water on top of compacted snow
40
Q

Autoland Max Winds (Headwind, Tailwind, Crosswind)
A319
A320
NEO

FM 1.30.10 Limitations

A

319
Headwind: 20 kts (15 kts SE)
Tailwind: 10 kts (5kts Flaps 3 or FE > 5750)
Xwind: 20 kts (15kts UA), 10kts SE

320
Headwind: 30 kts
Tailwind: 10 knots
Xwind: 20 kts (15kts UA)

NEO
Headwind: 15 kts
Tailwind: 10 kts
Xwind: 10 kts

41
Q

ILS Autoland Minimums

CAT II (with CAT 3 SINGLE or DUAL)
CAT III (with CAT 3 SINGLE)
CAT III with DH ( with CAT 3 SINGLE)
CAT III without DH (with CAT 3 DUAL)

FM 1.30.10 Limitations

A

CAT II (with CAT 3 SINGLE or DUAL):
DH 100 ft minimum
CAT III (with CAT 3 SINGLE):
DH 50 ft minimum
CAT III with DH ( with CAT 3 SINGLE):
AH 100 ft
CAT III without DH (with CAT 3 DUAL):
AH 100, RVR 300 ft

42
Q

ILS APPR mode limitation

FM 3.160.2 Normals - ILS Approaches

A

Do not arm the ILS approach mode > 8000 AGL

  • radio altimeter signals are not available above this altitude and with the APPR button armed, the AP and FDs disengage
43
Q

Minimum AP altitude for all other phases of flight (ex. circle to land)

FM 1.30.8 Limitations

A

500 ft AGL (900 AGL NEO)

44
Q

Engine Types
319 (40XX)
319 (48XX)
320

A

319 (40XX):
IAE 2522-A5
319 (48XX)
IAE 2524-A5
320
IAE 2527-A5

45
Q

Minimum Oil Pressure

FM 1.30.16 Limitations

A

60 PSI

46
Q

Max oil temp for continuous operation
Max for transient operation (up to 15 min)
Minimum temperature prior to takeoff
Minimum temperature before IDLE is exceeded

FM 1.30.16 Limitations

A

Max oil temp for continuous operation: 155°C
Max for transient operation (up to 15 min): 165°C
Minimum temperature prior to takeoff: 50°C
Minimum temperature before IDLE is exceeded: -10°C

47
Q

EGT Limits
Start
Takeoff/Go Around
Max Continuous

FM 1.30.16 Limitations

A

Start: 635°C
Takeoff/Go Around: 635°C for 5min (10min SE)
Max Continuous: 610°C

48
Q

Hydraulic max operating pressure

FM 1.30.27 Limitations

A

3000+/-200 PSI

49
Q

Tire Limit Speed

FM 1.20.5 Limitations

A

195 kt GS

50
Q

Max windshield wiper operation speed

FM 1.20.5 Limitations

A

230 kts

51
Q

Max speed window open in flight

FM 2.10.13 Non-normals

A

200 kts

52
Q

Fuel Imbalance at Takeoff
Inner tank imbalance (outer tanks balanced)
Outer tank imbalance (inner tanks balanced)

FM 1.30.25

A

Inner tank imbalance (outer tanks balanced): 1102 lbs
Outer tank imbalance (inner tanks balanced): 815 lbs

53
Q

NEO MLW

A

174.6

54
Q

AP Minimum Engagement Height
(NEO) Non-ILS approach with F-G/S

A

200 ft AGL or reversion point

FM 1.30.8
When charted, mode reversion point is represented by the “M” in the chart profile. When not charted, the mode reversion is 50 ft AGL

55
Q

APU Starting Altitudes
Using normal electrics

FM Limitations 1.30.13

A

Using normal electrics: 39,000 ft (improved below 31,000)

56
Q

APU Starting Altitudes
Using battery power only

FM Limitations 1.30.13

A

Using battery power only: 25,000 ft

57
Q

APU Starting Altitudes
One pack operation

FM Limitations 1.30.13

A

One pack operation: 20,000 ft

58
Q

APU Starting Altitudes
For engine start

FM Limitations 1.30.13

A

For engine start: 20,000 ft

59
Q

APU Starting Altitudes
Two pack operation

FM Limitations 1.30.13

A

Two pack operation: 15,000 ft

60
Q

Maximum Landing Gear Extended Mach (VLE)

A

.67M

U (13 decks)

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