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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 |
|
Max takeoff Weight |
MTOW 71500 kgs 77000 kgs |
|
Max landing weight A320 |
64 500 kgs |
|
Max Operating Speeds (Vmo/Mmo)
|
- Vmo 350 knots |
|
Maneouvering speed
|
295 / M.78
|
|
Max Flaps/Slats Extended Speeds (Vfe) |
Lp1 - 230 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). |
|
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 - 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. |
|
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 |
|
Electric power extraction |
90 KVA |
|
Powerplant
T/O and G/A Starting |
CFM: TOGA: 5 min/10 min 950℃ MCT: Unlimited 915 ℃ Start: 725 ℃ |
|
Powerplant |
-10°C |
|
Maximum continuous oil temp |
CFM: 140°C IAE: 155°C |
|
Powerplant |
155°C (15 min) |
|
Powerplant
Min starting oil temp |
-40°C |
|
Powerplant |
CFM: 9,5 -0,5/h IAE: 11 -0,3/h |
|
Powerplant |
13 psi |
|
Power plant starter limitations |
4x2m /Pause 20s/ Cooling 15m |
|
Reverse Thrust Limitations |
- Not permitted in flight. |
|
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 |