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72 Cards in this Set
- Front
- Back
Max Runway slope |
+/- 2% |
|
Max runway altitude |
8000’ |
|
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 dor |
65 knots 40 kts (50 kts if nose oriented) |
|
Load Acceleration Limits
|
Clean configuration -1g to +2.5g |
|
Max takeoff Weight A320 |
MTOW 77 000 kgs |
|
Max landing weight A320 |
64 500 kgs |
|
Max Operating Speeds (Vmo/Mmo)
|
- Vmo 350 knots |
|
Turbulent air penetration speed A319/A320
|
- Below FL200, maintain 250 knots.
- At or above FL200, maintain 275 knots / 0.76 Mach. |
|
Max Flaps/Slats Extended Speeds (Vfe) AA319/A320 |
Lever Position - Slats Flaps - Max Speed Lp1 - 18/0 -230 KIAS Holding |
|
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
|
|
A320/A321 Taxi Speed |
Max speed during a turn if weight > 76 000 kgs = 20 knots |
|
Max Design Maneuvering Speed (Va)
|
Va = 0.78 Mach (above 30,000 pressure altitude) |
|
Cabin Pressure
Max positive differential pressure Max negative differential pressure |
+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' ... unless FCU is set to |
|
Engine Inoperative Approaches
(limitations on these approaches) (good to know) |
The following are not authorized with an engine inoperative:
- Autolands (CAT I,II, or III). - The use of an autopilot to fly a non-precision approach using NAV or FINAL APP lateral modes. Only FD is permitted in this case. |
|
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) |
For Jet A only, if TAT reaches -34°C, monitor ECAM FUEL page that fuel temp. remains warmer than -36°C.
|
|
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
|
|
Parking Brake Limitation
(Good to know) |
Do not set EPR above 1.19 on both engines with the parking brake on.
|
|
APU Start Limitations (cycles)
|
The APU starter duty cycle is 3 consecutive start attempts. After the third start attempt, wait 60 minutes before attempting 3 more cycles. |
|
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
|
APU may be started and operated up to max certified pressure altitude of 39,100'.
|
|
Max altitude for battery assisted APU start
(emergency electrical configuration) |
FL250
|
|
Max altitude for APU bleed extraction
|
- FL200 with one pack operating
- FL150 with two packs operating |
|
Maxi EGT start |
Below 25 000' 900°C Above 25 000' 982℃ |
|
Maxi EGT with APU running |
682°C with 5 sec conf time shutdown 700℃ to 742℃ for immed SD |
|
Electric power extraction |
90 KVA |
|
Powerplant
T/O and G/A Stating |
5 min/10 min 890℃ Unlimited 855 ℃ 725 ℃ |
|
Powerplant |
-10°C
|
|
Powerplant |
-10°C |
|
Powerplant
Max continuous oil temp |
140°C |
|
Powerplant |
155°C (15 min) |
|
Powerplant
Min starting oil temp |
-40°C |
|
Powerplant
Min oil quantity |
11qts + est. consumption (~0.3 qt/hr)
|
|
Powerplant |
13 psi |
|
Power plant starter limitations |
4 consecutive cycles: 2 minutes each, followed by a 3rd cycle of 1 minute. |
|
Reverse Thrust Limitations |
- Not permitted in flight. |
|
Reduced Thrust Takeoff Limitations |
1. Takeoff at reduced thrust is only permitted, if the airplane meets all applicable performance requirements at the planned takeoff weight, with the operating engines at the thrust available for the flex temperature. |
|
Powerplant Starting |
Engine is capable of starting in crosswinds up to 35 knots.
|
|
Limitation on use of electrical outlets
|
Use of aircraft electrical outlets is prohibited during takeoff and landing.
|
|
Basic Forward CG Clean Config CG in TO/APP/LDG Config |
23 % 25 % |
|
Max Taxi Weight |
77400 Kgs |
|
Max Zero Fuel Weight
|
60 500 Kgs |
|
Turning limit speed with 1 tire deflated |
7 kts |
|
Turning limit speed and steering angle limit with 2 tire deflated |
3 kts and 30 ℃ |
|
Maxi N rotor Speed |
107 % (actual N Speed 105) |
|
Minimum Weight |
37230 Kgs |
|
Maximum unbalaced for the inner/Outer tanks |
2250/690 kgs |
|
Maximum positive Cabin differential pressure |
9 Psi |
|
EGT LIMIT FOR START |
725 deg |
|
Maxi crosswind speed for Rwy contaminated by ice cold and dry |
15 kts |
|
Maxi crosswind speed for Rwy contaminated by Slush or water more than 3 mm |
20 kts |
|
Maximum inbalanced for the inner Tanks when the heavier is full |
1500 kgs |
|
The flexible temperature for reduced Thrust T/O must not be higher than T Max Flex |
ISA + 45 DEG C |