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Airbus A320 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Taxi Weight

A

75,900 kg (167,300 lb)

77,400 kg (170,600 lb) - NEO

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2
Q

Max Takeoff Weight

A

75,500 kg (166,000 lb)

77,000 kg (169,800 lb) - NEO

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3
Q

Max Landing Weight

A

66,000 kg (145,500 lbs)

66,300 kg - NEO

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4
Q

Max Zero Fuel Weight

A

62,500 kg (137,800)

62,800 kg - NEO

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5
Q

Min Weight

A

37,230 kg (82,100 lb)

40,300 kg (88,800 lb) - NEO

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6
Q

Load Factor Limits

A

Clean Configuration -1g to 2.5g
Slats and Flaps Extended 0g to 2g
Slats Extended/Flaps Retracted 0g to 2g

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7
Q

Runway Slope Limit

A

+/- 2%

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8
Q

Runway Altitude Operation Limit

A

9200 ft

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9
Q

Min and Nominal Runway Width

A

Nominal: 45 meters
Min: 30 meters

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10
Q

Maximum Demonstrated Crosswind

A

Takeoff and Landing: 38 kts (gust included)

Damp runway: 38 kts (gust included)
Compacted snow: 29 kts (gust included)
Snow over 3mm: 25 kts (gust included)
Water over 3mm: 20 kts (gust included)
Ice: 15 kts (gust included)

FOM: 30 kts (gust included)

CATII: 15 knts

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11
Q

Max Tailwind (T/O and Landing)

A

10 kts (5 mps)

some aircraft 15 knts for takeoff

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12
Q

MAX WIND FOR PASSENGER AND CARGO DOORS OPERATION

A

Passenger Door - 65 knts (32 mps)
Cargo Door - 40 knts (20 mps)

cargo doors must be closed before 65 kts

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13
Q

MAXIMUM OPERATING SPEED VMO/MMO

A

350 knts up to Fl246

0.82 Mach to Fl390

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14
Q

MAXIMUM FLAPS/SLATS SPEEDS

A 
1 - 230 kts
1+F - 215 knts
2 - 200 knts
3 - 185 knts
Full - 177 knts
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15
Q

Vle

A

280 knts/0.67 Mach

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16
Q

Vlo

A

Extended - 250 knts

Retracted - 220 knts

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17
Q

MAXIMUM TIRE SPEED

A

195 knts

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18
Q

Maximum Landing Gear Extension Altitude

A

25,000 ft

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19
Q

MINIMUM CONTROL SPEED FOR LANDING (VMCL)

A

109 knts

NEO: 116 knts

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20
Q

WIPERS MAXIMUM OPERATING SPEED

A

230 knts

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21
Q

COCKPIT WINDOW OPEN MAXIMUM SPEED

A

200 knts

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22
Q

Maximum PositiveDifferential Pressure

A

9.0 psi

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23
Q

Maximum Negative Differential Pressure

A

-1 psi

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24
Q

Cabin Press Safety Relief Valve Setting

A

8.6 psi

25
Q

Min Autopilot Use Heights

A

Takeoff with SRS mode: 100ft AGL or 5 sec after liftoff

Landing Straight-in NPA: 200ft AGL (F-LOC/FLS); 250ft AGL (others)
Circling Approach: 500ft AGL
ILS with CAT 1: 160ft AGL
ILS with CAT 2 or 3: 0 AGL if autoland
Go Around: 100ft AGL
All other phases: 500ft AGL
Go Around: 100ft AGL
26
Q

Max Continuous Load per Gen

A

100% (90 kva)

27
Q

Max Continuous Load per TR

A

200 A

28
Q

Max Slat/Flap Altitude

A

20,000 ft

29
Q

Min/Max Fuel Temps

A

Jet A:

Min: -36C
Max: 54C

NEO - Min: -36C
Max: 55C

if TAT reaches -34C monitor ECAM FUEL page that fuel temp remains above -36C

30
Q

Min Fuel Tank Quantity for Takeoff

A

1500 kg (3307 lb)

31
Q

Normal Hydraulic Pressure

A

3000 psi +/-200 psi

2500 psi on RAT

32
Q

Max brake temp for takeoff

A

300C

33
Q

APU Start Limit

A

After 3 consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt

34
Q

Max APU Rotor Speed

A

Max N (ECAM Display) - 107%

35
Q

APU EGT Limits

A

Maximum EGT for APU start (below 35 000 ft)………….1090 °C Maximum EGT for APU start (above 35 000 ft)………….1120 °C Maximum EGT for APU running………..675 °C

36
Q

APU Envelope

A 
Bleed Air and Elec Power: -2000’ to FL225
Electric Power only: FL225 to FL410
APU Batt Start Limit (elec emerg): FL250
APU norm. Restart and Op Limit: FL410
Ground Starting: -1000’ to 14,500’

Max altitude to assist engine start………….20 000 ft
Max altitude for air cond and press (single pack operation)………22 500 ft
Max altitude for air cond and press (dual pack operation)………..15 000 ft

37
Q

APU BLEED limits

A

Max altitude to assist engine start…………………20 000 ft

Max altitude for air conditioning and pressurization (single pack operation)……………………22 500 ft

Max altitude for air conditioning and pressurization (dual pack operation)……………………15 000 ft

38
Q

MAX EGT Takeoff and Go Around

A

IAE: 635C limited to 5 mins (10 mins during engine failure)

CFM: 950C limited to 5 mins (10 mins during engine failure)

NEO: 1083C limited to 5 mins (10 mins during engine failure)

39
Q

MAX Continuous Thrust EGT

A

IAE: 610C

CFM: 915C

NEO: 1043C

40
Q

MAX Starting EGT

A

IAE: 635C

CFM: 725C

NEO: 1018C

41
Q

MAX Continuous Oil Temp

A

155C

NEO: 151C

42
Q

MAX Transient Oil Temp

A

165C (15 mins)

43
Q

MIN Starting Oil Temp

A

-40C

44
Q

MIN Oil Temp for Takeoff

A

50C

NEO: 52C

45
Q

MIN Oil Pressure

A

60 PSI

NEO: 65 PSI

46
Q

MAX N1

A

100%

47
Q

MAX N2

A

100%

48
Q

MAX Operational Altitude

A

FL398

NEO: FL414

49
Q

MIN Oil Temp before IDLE is exceeded

A

-10C

50
Q

Engine Starter Limits

A

One start = one cycle
NEO: up to 3 starts = one cycle

15s pause between cycles
NEO: 35s pause between cycles

30 min after 3 failed cycles
NEO: 15 mins after 3 failed cycles or 15 mins continuous crank

2 mins max cycle time (manual start)
5 mins max cycle time (crank)

Must not run started with N2 above 10% (18% in flight)
NEO: N2 above 20%

51
Q

Speed limit for MAX reverse

A

70 knts

52
Q

Min Oil Quantity

A

IAE: 11 qts + est. 0.3 qts/hr

CFM: 9.5 qts + est. 0.5 qts/hr

NEO: 14 qts

53
Q

Icing Conditions

A

Below 10C OAT (gnd) or 10C TAT (Flight) w/ visible moisture

Flight:

During Climb - Engine Ice ON in ice conditions except during climb or cruise with SAT

54
Q

Takeoff Pitch Limits (struts not compressed)

A

A320 - 13.5°
NEO - 13.7°
A321 - 11.2°

55
Q

Correction if operational CG is below 27%

A
  • Reduce Flex Temp 2°

- Increase V1, Vr, and V2 by 1

56
Q

Severe Turbulence Speed per QRH

A

FL200 - FL310: 275 kts

FL330 and above: Mach 0.76

Lower Altitudes: 250 kts

57
Q

MAX crosswind for engine start

A

35 kts

58
Q

Least Risk Bomb Location

A

Center of the RH AFT cabin door

59
Q

Total flight time on Batts only

A

30 mins

Airbus A320 (25 decks)

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