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Airbus A320 > Limitations > Flashcards

Limitations Flashcards

(59 cards)

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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

25
Min Autopilot Use Heights
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
Max Continuous Load per Gen
100% (90 kva)
27
Max Continuous Load per TR
200 A
28
Max Slat/Flap Altitude
20,000 ft
29
Min/Max Fuel Temps
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
Min Fuel Tank Quantity for Takeoff
1500 kg (3307 lb)
31
Normal Hydraulic Pressure
3000 psi +/-200 psi | 2500 psi on RAT
32
Max brake temp for takeoff
300C
33
APU Start Limit
After 3 consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt
34
Max APU Rotor Speed
Max N (ECAM Display) - 107%
35
APU EGT Limits
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
APU Envelope
``` 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
APU BLEED limits
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
MAX EGT Takeoff and Go Around
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
MAX Continuous Thrust EGT
IAE: 610C CFM: 915C NEO: 1043C
40
MAX Starting EGT
IAE: 635C CFM: 725C NEO: 1018C
41
MAX Continuous Oil Temp
155C NEO: 151C
42
MAX Transient Oil Temp
165C (15 mins)
43
MIN Starting Oil Temp
-40C
44
MIN Oil Temp for Takeoff
50C NEO: 52C
45
MIN Oil Pressure
60 PSI NEO: 65 PSI
46
MAX N1
100%
47
MAX N2
100%
48
MAX Operational Altitude
FL398 NEO: FL414
49
MIN Oil Temp before IDLE is exceeded
-10C
50
Engine Starter Limits
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
Speed limit for MAX reverse
70 knts
52
Min Oil Quantity
IAE: 11 qts + est. 0.3 qts/hr CFM: 9.5 qts + est. 0.5 qts/hr NEO: 14 qts
53
Icing Conditions
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
Takeoff Pitch Limits (struts not compressed)
A320 - 13.5° NEO - 13.7° A321 - 11.2°
55
Correction if operational CG is below 27%
- Reduce Flex Temp 2° | - Increase V1, Vr, and V2 by 1
56
Severe Turbulence Speed per QRH
FL200 - FL310: 275 kts FL330 and above: Mach 0.76 Lower Altitudes: 250 kts
57
MAX crosswind for engine start
35 kts
58
Least Risk Bomb Location
Center of the RH AFT cabin door
59
Total flight time on Batts only
30 mins

Airbus A320 (25 decks)

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