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60 Cards in this Set

  • Front
  • Back

Max Runway slope

+/- 2%

Max runway altitude for TO and LGD

9200’

Nominal runway width

45 m

Max crosswind demonstrated

38 knots (gust included)

Max tailwind

10 knots

Max wind for pax door operation


Max wind cargo doors

65 knots


40 kts (50 kts if nose oriented)

Load Acceleration Limits

Clean configuration -1g to +2.5g
Slats and flaps extended 0g to +2.0g
Slats extended and flaps retracted 0g to +2.0g

Max takeoff Weight

MTOW


71500 kgs


77000 kgs

Max landing weight A320

64 500 kgs

Max Operating Speeds (Vmo/Mmo)

- Vmo 350 knots
- Mmo 0.82 Mach

Maneouvering speed
295 / M.78

Max Flaps/Slats Extended Speeds (Vfe)

Lp1 - 230 KIAS
Lp1+F - 215 KIAS
Lp2 - 200 KIAS
Lp3 - 185 KIAS
FULL -177 KIAS

Max speed with landing gear extended
(Vle)

280 knots / 0.67 Mach

Max landing gear extension (operating) speed (Vlo)
250 knots
Max landing gear retraction speed
220 knots

Max altitude landing gear may be extended

FL250

Tires Max ground speed
195 knots
Max speed for windshield wiper in use
230 knots

Taxi Speed

Max speed during a turn if weight over 76 000 kgs = 20 knots

Max Design Maneuvering Speed (Va)

Va = 295 KIAS 0.78 Mach

Cabin Pressure
Max positive differential pressure
Max negative differential pressure
+9 / +8.6 psi
-1.0 psi

Ram Air (limitations)

Only open the ram air inlet if differential pressure is lower than 1.0 psi.
Ground Air Conditioning
Low Pressure Ground Unit
(Limitations)

- Do not use conditioned air simultaneously from PACK and LP ground unit (to avoid chattering of non-return valves).
- Airflow supplied by the ground cart shall not exceed 1,2 kg/s.

Ground Air Conditioning
High Pressure Ground Unit
(Limitations)
- Do not use HP ground unit when the APU is supplying bleed air to avoid bleed system damage.
- An HP ground unit may be used for air conditioning provided the air supply is confirmed to be free from oil contamination.

Min height for autopilot engagement



- Take off with SRS Mode


- Straight-in non precis APP


- S-I LNAV/VNAV


- Circling AP


- ILS APP (without CAT 2/3 displayed)


- G/A (A/P or FD Eng)


- Others




- Takeoff with SRS mode 100’ AGL (prevent 5s after Lift off)


- S-I np APP MDA (MDH)


- S-I LNAV/VNAV DA


- Circling MDA-100


- ILS. 160' AGL
- Go-around 100’ AGL


- Others 500ft

Limitation on use of certain AP or FD modes

Use of AP or FD in OP DES or DES mode is not authorized during approach below minimums MDA(MDH) or 500'

When can NAV mode be used in the terminal area?
NAV mode may be used in the terminal area, provided:
- GPS PRIMARY is available,
- HIGH accuracy is displayed, or
- Navaid raw data is monitored.

Glideslope angle for autoland

within -2.5° to -3.15° (A320/A321)

Max wind Cat 2/3 for autoland Conf 3 and Full

Based on surface wind reports incl. gusts.
- Tailwind 10 knots
- Crosswind 20 knots/ 15 S
- Headwind 30 knots

Generator / TR Limitation

Max continuous load per generator:
100% (90 kVA)

Max continuous load per TR:
200 A
Max altitude with flaps and/or slats extended
20,000'
Fuel Temperature
(Note on Jet A)
-43 / +54
Fuel Management Limitations

(Good to know)
- Takeoff using the center tank is prohibited.
- Center tanks must be emptied before the wing tanks under normal conditions.
Hydraulic operating pressure
3000 psi +/- 200 psi
Max brake temperature for takeoff (brake fans off)
300°C
APU Start Limitations (cycles)

3 cycles / 60 m

Limitation on bleed extraction from the APU
Air bleed extraction from the APU for wing and anti-ice is not permitted.
APU start envelope with normal A/C power supply
FL410
Max altitude for battery assisted APU start
(emergency electrical configuration)
FL250

Max altitude for APU bleed extraction

- FL225 with one pack operating


- FL200 engine start
- FL150 with two packs operating

Electric power extraction

90 KVA

Powerplant
Time / EGT Limits



T/O and G/A
Maximum Continuous (MCT)


Starting

CFM:


TOGA: 5 min/10 min 950℃


MCT: Unlimited 915 ℃


Start: 725 ℃

Powerplant
Min oil temp prior to takeoff

-10°C

Maximum continuous oil temp

CFM: 140°C


IAE: 155°C

Powerplant
Max transient oil temp

155°C (15 min)

Powerplant
Min starting oil temp

-40°C

Powerplant
Min oil quantity

CFM: 9,5 -0,5/h


IAE: 11 -0,3/h

Powerplant
Min oil pressure at Ground Iddle

13 psi

Power plant starter limitations

4x2m /Pause 20s/ Cooling 15m
No running engagement of the starter, when N2 is above 20%.

Reverse Thrust Limitations

- Not permitted in flight.
- Not permitted to back up the aircraft.
- Max reverse should not be used less than 70 knots permetted down to aircraft stop.

CG T/O LDG

15-37%

Max Taxi Weight

71900 Kgs


73900 Kgs


77400 Kgs

Max Zero Fuel Weight


61 000 Kgs

N1/ N2

104% / 105%

Minimum Weight

37230 Kgs

Maximum unbalaced for the inner/Outer tanks

Full / 1500


4300 /1600


2250 / 2250


Outer 690 kgs

Maximum positive Cabin differential pressure

9 Psi

EGT LIMIT FOR START

CFM: 725 deg


IAE: 635 deg

Maximum inbalanced for the inner Tanks when the heavier is full

1500 kgs

Max Flex

53