320 Limitations Flashcards

1
Q

VMO/MMO

A

350 KIAS / .82 Mach

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2
Q

Maximum Pressure Altitude

A

39,100 feet

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3
Q

Maximum pressure altitude takeoff/landing

A

9200 feet

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4
Q

Runway slope

A

+-2%

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5
Q

Minimum runway width

A

100 feet

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6
Q

Are Autolands authorized on narrow runway’s?

A

No

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7
Q

Maximum landing weight for 319, 320, NEO aircraft?

A

319: 137.7
320: 142.2
321: 174.6

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8
Q

Maximum tailwinds for 319, 320, 321 aircraft?

A

319: takeoff and landing 10 kts
320: takeoff 15 kts landing 10kts
321: takeoff 15kts landing 15kts

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9
Q

Maximum crosswind takeoff and landing (dry runway)

A

Takeoff 38 kts landing 38 kts

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10
Q

Turbulence speed recommended

A

Above FL20 .76 Mach/275 kts
Below FL20 250 kts

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11
Q

Maximum wind for passenger door operation

A

65 kts

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12
Q

Oxygen requirements

A

(40XX, 41XX, 42XX, 46XX, 47XX) 850 PSI
(48XX, 49XX) 1230 PSI

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13
Q

Maximum speed cockpit window

A

200kts

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14
Q

Maximum windshield wiper speed

A

230kts

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15
Q

Negative cabin differential

A

-1.0 PSI

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16
Q

Maximum (safety relief) differential

A

8.6 PSI

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17
Q

APU with HP ground unit allowed?

A

It is prohibited

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18
Q

Avionics ventilation should not be powered for more than (blank) without a cooling system when outside air temperature is above (blank)

A

2 hours
49C

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19
Q

When do we use engine anti-ice

A

Ground operations 10C or less and visible moisture
Climb/cruise 10C or less to -40 SAT and visible moisture
Descent/approach 10C or less and with visible moisture

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20
Q

What is the autoland demonstrated capability?

A

CAT 2 and CAT3 ILS beam
Glide slope angles -2.5 and -3.15 inclusive
Airport elevation up to 6500 feet
Rollout mode has been demonstrated on dry and wet pavement

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21
Q

Auto land wind requirements dual and single engine 319 and 320?

A

319: headwind 20kts, tailwind 10kts, crosswind 20kts
319 SE: headwind 15kts, tailwind 5kts (flaps 3) or field elevation is >5750, crosswind 10kts

320: headwind 30kts, tailwind 10kts, crosswind 20kts
320 SE: crosswind 15kts

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22
Q

Autopilot minimum engagement height after takeoff?

A

100 feet

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23
Q

Autopilot minimum engagement height in all other phases?

A

1000 feet

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24
Q

Autopilot minimum engagement height non ILS approach’s?

A

250 feet or DDA/DH whichever occurs earlier.
200 feet (NEO)

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25
Q

Autopilot minimum engagement height non auto land ILS CAT 1 and NEO GLS non auto land with CAT 1?

A

160 feet AGL

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26
Q

Autopilot minimum engagement height CAT 2 or 3 FMA?

A

80 feet AGL

27
Q

Autopilot minimum engagement height go around?

A

100 feet

28
Q

Autopilot minimum engagement height circle to land?

A

500 feet

29
Q

Autopilot disengagement in autoland?

A

Rollout

30
Q

Maximum continuous load per generator?

A

100% (90 KVA)

31
Q

Maximum TRU load?

A

200 amps

32
Q

Maximum engine start EGT?

A

635

33
Q

Maximum engine EGT during takeoff/go-around?

A

635

34
Q

Maximum engine EGT continuous?

A

610

35
Q

Minimum oil pressure?

A

60 psi

36
Q

Maximum oil temperature continuous?

A

155C

37
Q

Maximum oil temperature for up to 15 minutes?

A

165C

38
Q

An engine shutdown for more than 2 hours must operate at or near idle before takeoff to avoid thermal shock?

A

5 minutes

39
Q

Both engines must operate at or near idle a minimum of how many minutes to ensure center tank test complete?

A

2 minutes

40
Q

Allow engines to operate at or near idle for how many minutes before shutdown?

A

3 minutes

41
Q

Engine starter limitations?

A

3 consecutive start attempts 1and 2 15 sec off. Third attempt max crank time 5 minutes and 30 minutes off

42
Q

Minimum oil quantity before start?

A

14 quarts

43
Q

Minimum oil temperature prior to start?

A

-40C

44
Q

Minimum oil temperature for takeoff?

A

+50C

45
Q

APU start using battery power only?

A

25,000 feet

46
Q

APU start using normal electrics?

A

39,000 feet

47
Q

APU two pack operation?

A

15,000 feet

48
Q

APU one pack operation?

A

20,000 feet

49
Q

APU engine start?

A

20,000 feet

50
Q

APU Honeywell one pack operation?

A

22,500 feet

51
Q

APU starter limitations?

A

3 consecutive start attempts 1 minute cool down after each attempt. 3rd attempt requires 60 minute cool down.

52
Q

Maximum flaps or slats altitude?

A

20,000 feet MSL

53
Q

Flight maneuvering load limits?

A

Clean configuration -1.0g to +2.5g
With slats and flaps 0.0g to +2.0g

54
Q

Speed brake limitations?

A

Meteorological conditions do not use below 1000 feet AGL
In flight with slats retracted do not use below 200kts

55
Q

Approach category for 319 and 320?

A

Straight in approaches CAT C
Circling approaches CAT D

56
Q

RVSM requirements

A

2 ADR
Transponder
1 FWC
1 autopilot
2 PFDs
FCU

57
Q

Takeoff with center tank fuel supplying the engines is?

A

Prohibited

58
Q

Maximum hydraulic operating pressure?

A

3000 psi

59
Q

Landing gear limitations?

A

Retraction VLO 220 KIAS
Extension VLO 250 KIAS
Extended VLE 280 KIAS

60
Q

When takeoff is higher than 167,500lbs do not exceed in a turn

A

20kts

61
Q

Maximum tire speed

A

195 kts ground speed

62
Q

Maximum brake temperature for takeoff

A

300C

63
Q

How do we handle non-normal situations

A

Fly the aircraft
Silence the warning
Confirm the emergency

64
Q

Stabilized approach criteria

A

Plan:
Not later than 1500 feet AGL/RA or the FAF, whichever occurs later:
Landing gear down
Airspeed no greater than 180 KIAS
Report: not later than 1000 feet:
Final landing configuration/Landing checklist complete
Airspeed within +15 or -5 KIAS of target speed
On vertical and lateral profile with no more than 1200 fpm
Reject:
At 500 feet: PF 500 callout Stable or unstable, going around