A320 / A321 LIMITATIONS (IBS fleet)

A320 / A321 (IBS fleet). AIRCRAFT GENERAL. FLIGHT MANEUVERING LOAD ACCELERATION LIMITS. Other configurations: 0.0 g to +2.0 g. 0.5 g to +2.0 g. -1.0 g to +2.5 g. -1.5 g to +2.0 g.

A320 / A321 (IBS fleet). Maximum Taxi Weight: 75900 kg (167330 lb) ; 73900 kg (162921 lb) ; 89400 kg (197093 lb) ; 77400 kg (170637 lb) ; 71900 kg (158512 lb). 75500 kg (166448 lb) ; 73500 kg (162039 lb) ; 89000 kg (196211 lb) ; 77000 kg (169755 lb) ; 71500 kg (157630 lb). 64500 kg (142198 lb) ; 75500 kg (166449 lb). 61000 kg (134481 lb) ; 71500 kg (157630 lb). 37230 kg (82079 lb) ; 47500 kg (104720 lb).

A320 / A321 (IBS fleet). Maximum Takeoff Weight (brake release): 75900 kg (167330 lb) ; 73900 kg (162921 lb) ; 89400 kg (197093 lb) ; 77400 kg (170637 lb) ; 71900 kg (158512 lb). 75500 kg (166448 lb) ; 73500 kg (162039 lb) ; 89000 kg (196211 lb) ; 77000 kg (169755 lb) ; 71500 kg (157630 lb). 64500 kg (142198 lb) ; 75500 kg (166449 lb). 61000 kg (134481 lb) ; 71500 kg (157630 lb). 37230 kg (82079 lb) ; 47500 kg (104720 lb).

A320 / A321 (IBS fleet). Maximum Landing Weight: 75900 kg (167330 lb) ; 73900 kg (162921 lb) ; 89400 kg (197093 lb) ; 77400 kg (170637 lb) ; 71900 kg (158512 lb). 75500 kg (166448 lb) ; 73500 kg (162039 lb) ; 89000 kg (196211 lb) ; 77000 kg (169755 lb) ; 71500 kg (157630 lb). 64500 kg (142198 lb) ; 75500 kg (166449 lb). 61000 kg (134481 lb) ; 71500 kg (157630 lb). 37230 kg (82079 lb) ; 47500 kg (104720 lb).

A320 / A321 (IBS fleet). If Taxi Weight is higher than 76000 kg (167550 lb)... Do not exceed a taxi speed of 20 kt during a turn. Do not exceed a taxi speed of 25 kt during a turn. Do not exceed a taxi speed of 30 kt during a turn. Do not exceed a taxi speed of 35 kt during a turn.

A320 / A321 (IBS fleet). Maximum Zero Fuel Weight: 75900 kg (167330 lb) ; 73900 kg (162921 lb) ; 89400 kg (197093 lb) ; 77400 kg (170637 lb) ; 71900 kg (158512 lb). 75500 kg (166448 lb) ; 73500 kg (162039 lb) ; 89000 kg (196211 lb) ; 77000 kg (169755 lb) ; 71500 kg (157630 lb). 64500 kg (142198 lb) ; 75500 kg (166449 lb). 61000 kg (134481 lb) ; 71500 kg (157630 lb). 37230 kg (82079 lb) ; 47500 kg (104720 lb).

A320 / A321 (IBS fleet). Minimum Weight: 75900 kg (167330 lb) ; 73900 kg (162921 lb) ; 89400 kg (197093 lb) ; 77400 kg (170637 lb) ; 71900 kg (158512 lb). 75500 kg (166448 lb) ; 73500 kg (162039 lb) ; 89000 kg (196211 lb) ; 77000 kg (169755 lb) ; 71500 kg (157630 lb). 64500 kg (142198 lb) ; 75500 kg (166449 lb). 61000 kg (134481 lb) ; 71500 kg (157630 lb). 37230 kg (82079 lb) ; 47500 kg (104720 lb).

A320 / A321 (IBS fleet). AIRCRAFT GENERAL. FLIGHT MANEUVERING LOAD ACCELERATION LIMITS. Clean configuration: -1.0 g to +2.5 g. -1.5 g to +2.0 g. 0.0 g to +2.0 g. 0.5 g to +2.0 g.

A320 / A321 (IBS fleet). AIRPORT OPERATIONS AND WIND LIMITATIONS. RUNWAY SLOPE. Runway slope (mean)... ± 2.0 %. ± 2.5 %. ± 2.2 %. ± 2.3 %.

A320-214/216 / A321-213 (IBS fleet). OPERATIONAL PARAMETERS. ENVIRONMENTAL ENVELOPE. Maximum pressure altitude (between -70 ºC and -28 ºC approx): 39800 ft. 38900 ft. 39100 ft. 38100 ft.

A320 / A321 (IBS fleet) maximum demonstrated crosswind (takeoff and landing): 38 kt (including gust). 38 kt. 39 kt (including gust). 39 kt.

A320 / A321 (IBS fleet). AIRCRAFT GENERAL. OPERATIONAL PARAMETERS. TAILWIND TAKEOFF. Maximum tailwind for takeoff: 10 kt. 15 kt. 20 kt. 30 kt.

A320 / A321 (IBS fleet). AIRCRAFT GENERAL. OPERATIONAL PARAMETERS. PASSENGER AND CARGO DOORS OPERATION. The maximum wind for passenger door operation is... 65 kt. 45 kt. 60 kt. 40 kt.

A320 / A321 (IBS fleet). AIRCRAFT GENERAL. OPERATIONAL PARAMETERS. PASSENGER AND CARGO DOORS OPERATION. The maximum wind for FWD and AFT cargo door operation is __ kt (or __ kt, if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side): 40 ; 50 kt. 45 ; 50 kt. 40 ; 55 kt. 45 ; 55 kt.

A320 / A321 (IBS fleet). AIRCRAFT GENERAL. OPERATIONAL PARAMETERS. PASSENGER AND CARGO DOORS OPERATION. The FWD and AFT cargo doors must be closed before the wind speed exceeds... 65 kt. 60 kt. 55 kt. 50 kt.

A320 / A321 (IBS fleet) minimum control speeds: Vmcg. 110 kt. 103 kt. 130 kt. 101 kt.

A320 / A321 (IBS fleet) maximum flaps/slats speed at TAKEOFF: CONF 1+F. 230 kt. 215 kt. 200 kt. 185 / 195 kt. 177 / 190 kt.

A320 / A321 (IBS fleet) maximum flaps/slats speeds at TAKEOFF / APPROACH: CONF 2. 230 kt. 215 kt. 200 kt. 185 / 195 kt. 177 / 190 kt.

A320 / A321 (IBS fleet) maximum flaps/slats speeds at TAKEOFF / APPROACH /LANDING: CONF 3. 230 kt. 215 kt. 200 kt. 185 / 195 kt. 177 / 190 kt.

A320 / A321 (IBS fleet) maximum flaps/slats speeds at LANDING: FULL. 230 kt. 215 kt. 200 kt. 185 / 195 kt. 177 / 190 kt.

A320 / A321 (IBS fleet) maximum flaps/slats speeds at HOLDING: CONF 1. 230 kt. 215 kt. 200 kt. 185 / 195 kt. 177 / 190 kt.

A320 / A321 (IBS fleet) gear down speeds: maximum speed or Mach No. with landing gear extended (VLE): 280 kt / M .67. 250 kt / M .37. 230 kt / M .34. 285 kt / M .43.

A320 / A321 (IBS fleet) gear down speeds: maximum speed at which the landing gear may be extended (VLO): 250 kt / M 0.60. 230 kt / M 0.58. 280 kt / M 0.72. 220 kt / M 0.54.

A320 / A321 (IBS fleet) gear down speeds: maximum speed at which the landing gear may be retracted (VLO)... 250 kt / M 0.60. 230 kt / M 0.58. 220 kt / M 0.54. 280 kt / M 0.78.

A320 / A321 (IBS fleet) maximum altitude at which the landing gear may be extended... 25000 ft. 20000 ft. 22000 ft. 21000 ft.

A320 / A321 (IBS fleet) ground speed maximum tire speed... 195 kt. 193 kt. 196 kt. 194 kt.

A320 / A321 (IBS fleet) maximum operating speed (VMO)... 350 kt. 380 kt. 330 kt. 320 kt.

A320 / A321 (IBS fleet) maximum operating Mach No. (MMO)... M 0.82. M 0.81. M 0.80. M 0.83.

A320 / A321 (IBS fleet) maximum speed for windshield wipers usage... 200 kt. 220 kt. 230 kt. 250 kt.

A320 / A321 (IBS fleet) maximum speed with open cockpit window... 200 kt. 230 kt. 250 kt. 220 kt.

A320 / A321 (IBS fleet) maximum taxi speed if weight is higher than 76000 kg... 20 kt. 25 kt. 30 kt. 35 kt.

A320 / A321 (IBS fleet) cabin pressure: maximum differential pressure values... Positive +9.0 PSI ; Negative -1.0 PSI. Positive +9.6 PSI ; Negative -1.0 PSI. Positive +9.0 PSI ; Negative -1.6 PSI. Positive +9.6 PSI ; Negative -1.6 PSI.

A320 / A321 (IBS fleet) AIR BLEED/COND/PRESS/VENT. CABIN PRESSURE. Safety relief valve setting... 8.6 PSI. 9.6 PSI. 8.0 PSI. 9.0 PSI.

A320 / A321 (IBS fleet) minimum height for use of autopilot on takeoff with SRS mode... 100 ft AGL. 100 ft AMSL. 50 ft AGL. 50 ft AMSL.

A320 / A321 (IBS fleet) maximum continuous load per generator... 100 % (90 kVA). 110 % (90 kVA). 100 % (95 kVA). 110 % (95 kVA).

A320 / A321 (IBS fleet) maximum continuous load per TR (continuous)... 200 A. 210 A. 220 A. 230 A.

A320 / A321 (IBS fleet). FLIGHT CONTROLS. MAXIMUM ALTITUDE FLAPS/SLATS EXTENDED. Maximum operating altitude with slats and/or flaps extended... 20000 ft. 21000 ft. 22000 ft. 25000 ft.

A320-216 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): Full. Maximum Asymmetry... 500 kg (1102 lb). 1050 kg (2314 lb). 1320 kg (2910 lb). 1500 kg (3306 lb). No limitation.

A320-216. FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): 3000 kg (6613 lb). Maximum Asymmetry... 500 kg (1102 lb). 1050 kg (2314 lb). 1450 kg (3196 lb). 2250 kg (4960 lb). No limitation.

A320-216 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): 1450 kg (3196 lb). Maximum Asymmetry... 500 kg (1102 lb). 1050 kg (2314 lb). 1450 kg (3196 lb). 1300 kg (3527 lb). No limitation.

A320-216 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. OUTER TANKS (INNER TANKS BALANCED). Maximum Asymmetry... 370 kg (815 lb). 1050 kg (2314 lb). 1450 kg (3196 lb). 690 kg (1521 lb). No limitation.

A320-216 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): Full. Maximum Asymmetry... 1450 kg (3196 lb). 1500 kg (3306 lb). 1600 kg (3527 lb). 2350 kg (5180 lb). No limitation.

A320-216 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): 4300 kg (9479 lb). Maximum Asymmetry... 1450 kg (3196 lb). 1500 kg (3306 lb). 1600 kg (3527 lb). 2350 kg (5180 lb). No limitation.

A320-216 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): 2250 kg (4960 lb). Maximum Asymmetry... 1450 kg (3196 lb). 1500 kg (3306 lb). 1600 kg (3527 lb). 2250 kg (4960 lb). No limitation.

A320 / A321 (IBS fleet) hydraulic normal operating pressure... 3000 ± 200 PSI. 3000 ± 100 PSI. 3000 ± 150 PSI. 3000 ± 250 PSI.

A320 / A321 (IBS fleet). LANDING GEAR. BRAKE TEMPERATURE. Maximum brake temperature for takeoff... 300 ºC ; 150 ºC (with brake fan). 350 ºC ; 150 ºC (with brake fan). 350 ºC ; 100 ºC (with brake fan). 300 ºC ; 100 ºC (with brake fan).

A320 / A321 (IBS fleet) nose wheel steering: when using the hand wheels, the nose wheel steering angle is limited to... 75 ºC. 95 ºC. 85 ºC. 70 ºC.

A320 / A321 (IBS fleet) nose wheel steering: or towing and pushback, the nose wheel steering angle is limited to... 75 ºC. 95 ºC. 85 ºC. 70 ºC.

A320 / A321 (IBS fleet). ENGINES. THRUST SETTING/EGT LIMITS. Operating Conditions: Takeoff(1) and Go-around. Time limit: All engines operative (5 min) / One engine inoperative (10 min). EGT Limit: 950 ºC. 915 ºC. 725 ºC. 890 ºC.

A320 / A321 (IBS fleet). ENGINES. THRUST SETTING/EGT LIMITS. Operating Conditions: Maximum Continuous Thrust (MCT). Time limit: Not limited. EGT Limit: 915 ºC. 950 ºC. 725 ºC. 855 ºC.

A320 / A321 (IBS fleet). ENGINES. SHAFT SPEEDS. Maximum N1: 102 %. 104 %. 105 %. 103 %.

A320 / A321 (IBS fleet). ENGINES. THRUST SETTING/EGT LIMITS. Operating Conditions: Starting (On ground/In flight). EGT Limit: 890 ºC. 855 ºC. 725 ºC. 915 ºC.

A320 / A321 (IBS fleet). ENGINES. SHAFT SPEEDS. Maximum N2: 102 %. 104 %. 105 %. 100 %.

A320 / A321 (IBS fleet). OPERATIONAL PARAMETERS. ENVIRONMENTAL ENVELOPE. Maximum Takeoff and Landing pressure altitude (between -47 ºC and +38 ºC approx): 9200 ft. 9000 ft. 8200 ft. 8000 ft.

A320 / A321 (IBS fleet). ENGINES. OIL. OIL TEMPERATURE. Maximum continuous temperature: 140 ºC. 145 ºC. 150 ºC. 155 ºC.

A320 / A321 (IBS fleet). ENGINES. OIL. OIL TEMPERATURE. Maximum transient temperature (15 min): 150 ºC. 145 ºC. 165 ºC. 155 ºC.

A320 / A321 (IBS fleet). ENGINES. OIL. OIL TEMPERATURE. Minimum starting temperature: -40 ºC. -45 ºC. -50 ºC. -55 ºC.

A320 / A321 (IBS fleet). ENGINES. OIL. OIL TEMPERATURE. Minimum temperature for takeoff: -10 ºC. -15 ºC. -20 ºC. -25 ºC.

A320 / A321 (IBS fleet). ENGINES. OIL. The oil quantity must be at or above... 9.5 qt. 9.4 qt. 9.3 qt. 9.6 qt.

A320 / A321 (IBS fleet). ENGINES. OIL. The average estimated consumption is... 0.5 qt/h. 0.4 qt/h. 0.3 qt/h. 0.6 qt/h.

A320 / A321 (IBS fleet). ENGINES. OIL. OIL PRESSURE. MIN/MAX Oil Pressure (ECAM Indication). Minimum Oil Pressure (between N2 0 % and 105 % aprox.): 13 PSI. 14 PSI. 15 PSI. 12 PSI.

A320-214/216 (IBS fleet). OPERATIONAL PARAMETERS. ENVIRONMENTAL ENVELOPE. Minimum Takeoff and Landing pressure altitude (between -38 ºC and +55 ºC approx): -2000 ft. -1000 ft. -2200 ft. -1200 ft.

A320-214 (IBS fleet). OPERATIONAL PARAMETERS. ENVIRONMENTAL ENVELOPE. Maximum pressure altitude (between -70 ºC and -28 ºC approx): 39100 ft. 39800 ft. 38900 ft. 38700 ft.

A320-214 / A321 (IBS fleet). OPERATIONAL PARAMETERS. ENVIRONMENTAL ENVELOPE. Minimum Takeoff and Landing pressure altitude (between -38 ºC and +55 ºC approx): -1000 ft. -1500 ft. -2000 ft. -2500 ft.

A320 (IBS fleet). AIRCRAFT GENERAL. SPEEDS. MINIMUM CONTROL SPEEDS. MINIMUM CONTROL SPEED FOR LANDING (VMCL): 113 kt - 108 kt. 110 kt - 108 kt. 103 kt - 102 kt. 113 kt - 105 kt.

A321(IBS fleet). AIRCRAFT GENERAL. SPEEDS. MINIMUM CONTROL SPEEDS. MINIMUM CONTROL SPEED FOR LANDING (VMCL): 114 kt - 112 kt. 114 kt - 110 kt. 112 kt - 110 kt. 113 kt - 112 kt.

A320 / A321 (IBS fleet). AIRCRAFT GENERAL. OPERATIONAL PARAMETERS. TAILWIND TAKEOFF. Maximum tailwind for landing: 25 kt. 10 kt. 15 kt. 20 kt.

A320 / A321 (IBS fleet). AUTOMATIC ENGINE START: ENG MASTER 2...ON. ON ECAM UPPER DISPLAY <---> ON ECAM LOWER DISPLAY: - N2 increases <---> Corresponding start valve in line. Bleed pressure indication green. Oil pressure increases; - At 16 % <---> N2 Indication of the active igniter (A or B). - At 22 % N2 ‐ FF increases. - 15 s (maximum) after fuel is on - EGT increases ‐ N1 increases. - At 50 % N2 <---> Start valve starts closing. (It is fully closed between 50 % and 56 % N2). Igniter indication off. ENG MASTER 2...ON. ON ECAM UPPER DISPLAY <---> ON ECAM LOWER DISPLAY: - N2 increases <---> Corresponding start valve in line. Bleed pressure indication green. Oil pressure increases; - At 16 % N2 ‐ FF increases. - At 22 % <---> N2 Indication of the active igniter (A or B). - 15 s (maximum) after fuel is on - EGT increases ‐ N1 increases. - At 50 % N2 <---> Start valve starts closing. (It is fully closed between 50 % and 56 % N2). Igniter indication off. ENG MASTER 2...ON. ON ECAM UPPER DISPLAY <---> ON ECAM LOWER DISPLAY: - N1 increases <---> Corresponding start valve in line. Bleed pressure indication green. Oil pressure increases; - At 16 % <---> N1 ‐ FF increases. - At 22 % N1 Indication of the active igniter (A or B). - 15 s (maximum) after fuel is on - EGT increases ‐ N2 increases. - At 50 % N1 <---> Start valve starts closing. (It is fully closed between 50 % and 56 % N1). Igniter indication off. ENG MASTER 2...ON. ON ECAM UPPER DISPLAY <---> ON ECAM LOWER DISPLAY: - N2 increases <---> Corresponding start valve in line. Bleed pressure indication green. Oil pressure increases; - At 15 % <---> N2 Indication of the active igniter (A or B). - At 22 % N2 ‐ FF increases. - 16 s (maximum) after fuel is on - EGT increases ‐ N1 increases. - At 50 % N2 <---> Start valve starts closing. (It is fully closed between 50 % and 56 % N2). Igniter indication off.

A320 / A321 (IBS fleet) operating speeds: Green dot = 2 x weight (in tones) + 85 kt. Green dot = 2 x weight (in tones) + 80 kt. Green dot = 2 x weight (in tones) + 83 kt. Green dot = 2 x weight (in tones) + 82 kt.

A320 / A321 (IBS fleet) APU in flight restart: APU battery (emergency configuration): 25000 ft; Normal configuration: 41000 ft. APU battery (emergency configuration): 22000 ft; Normal configuration: 40000 ft. APU battery (emergency configuration): 22000 ft; Normal configuration: 41000 ft. APU battery (emergency configuration): 25000 ft; Normal configuration: 39000 ft.

A320 / A321 (IBS fleet) wingspan: 34.1 m. 31.4 m. 35.1 m. 31.5 m.

A320 / A321 (IBS fleet) minimal runway width: 30 m. 31 m. 45 m. 43 m.

A320 FWD and AFT cargo doors must be closed before the wind speed exceeds... 65 kt. 40 kt. 50 kt. 38 kt.

A320 / A321 (IBS fleet) Maximum recommended crosswind on wet and contaminated runways: >Runway Surface Conditions: - Damp. - Wet (up to 3 mm (1/8'') of water). - Slush (up to 3 mm (1/8'')). - Dry snow (up to 3 mm (1/8'')). - Wet snow (up to 3 mm (1/8'')). - Frost. >ESF (Estimated Surface Friction) or PIREP (Pilot Report of Braking Action): - Good. >Maximum Crosswind for Takeoff (Gust included) / Maximum Crosswind for Landing (Gust included) is ... 38 kt / 38 kt. 29 kt / 29 kt. 25 kt / 25 kt. 20 kt / 20 kt. 15 kt / 15 kt.

A320 Maximum recommended crosswind on wet and contaminated runways: >Runway Surface Conditions: - Compacted snow (OAT at or below -15 °C). >ESF (Estimated Surface Friction) or PIREP (Pilot Report of Braking Action): - Good to medium. >Maximum Crosswind for Takeoff (Gust included) / Maximum Crosswind for Landing (Gust included) is ... 38 kt / 38 kt. 29 kt / 29 kt. 25 kt / 25 kt. 20 kt / 20 kt. 15 kt / 15 kt.

A320 Maximum recommended crosswind on wet and contaminated runways: >Runway Surface Conditions: - Dry snow (more than 3 mm (1/8''), up to 100 mm (4'')). - Wet snow (more than 3 mm (1/8''), up to 30 mm (6/5'')). - Compacted snow (OAT above -15 °C). - Dry snow over compacted snow. - Wet snow over compacted snow. - Slippery when wet. >ESF (Estimated Surface Friction) or PIREP (Pilot Report of Braking Action): - Medium. >Maximum Crosswind for Takeoff (Gust included) / Maximum Crosswind for Landing (Gust included) is ... 38 kt / 38 kt. 29 kt / 29 kt. 25 kt / 25 kt. 20 kt / 20 kt. 15 kt / 15 kt.

A320 Maximum recommended crosswind on wet and contaminated runways: >Runway Surface Conditions: - Water (more than 3 mm (1/8''), up to 12.7 mm (1/2'')). - Slush (more than 3 mm (1/8''), up to 12.7 mm (1/2'')). >ESF (Estimated Surface Friction) or PIREP (Pilot Report of Braking Action): - Medium to poor. >Maximum Crosswind for Takeoff (Gust included) / Maximum Crosswind for Landing (Gust included) is ... 38 kt / 38 kt. 29 kt / 29 kt. 25 kt / 25 kt. 20 kt / 20 kt. 15 kt / 15 kt.

A320 Maximum recommended crosswind on wet and contaminated runways: >Runway Surface Conditions: - Ice (cold & dry). >ESF (Estimated Surface Friction) or PIREP (Pilot Report of Braking Action): - Poor. >Maximum Crosswind for Takeoff (Gust included) / Maximum Crosswind for Landing (Gust included) is ... 38 kt / 38 kt. 29 kt / 29 kt. 25 kt / 25 kt. 20 kt / 20 kt. 15 kt / 15 kt.

A320 / A321 AIR BLEED/COND/PRESS/VENT (IBS fleet). GENERAL: With passengers on board, it is not recommended to exceed_____without air conditioning supply. The lack of fresh air supply will significantly reduce the cabin’s air quality. 20 min. 25 min. 30 min. 35 min.

A320 / A321 AIR BLEED/COND/PRESS/VENT (IBS fleet). APU BLEED USE WITH HP AIR START UNIT: The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System. The flight crew must not use bleed air from the APU BLEED and from the LP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System. The flight crew is allowed to use bleed air from the APU BLEED and from the HP Air Start Unit at the same time. The flight crew is allowed to use bleed air from the APU BLEED and from the LP Air Start Unit at the same time.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. AVIONICS VENTILATION: During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows for OAT ≤ 49 °C: No limitation. 2 h. 1 h. 0.5 h.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. AVIONICS VENTILATION: During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows for 49 °C < OAT ≤ 55 °C: No limitation. 2 h. 1 h. 0.5 h.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. AVIONICS VENTILATION: During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows for 55 °C < OAT ≤ 60 °C: No limitation. 2 h. 1 h. 0.5 h.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. AVIONICS VENTILATION: During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must limit the time that the aircraft electric power supply is used, in normal avionics ventilation system configuration, as follows for 60 °C < OAT ≤ 64 °C: No limitation. 2 h. 1 h. 0.5 h.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. CABIN PRESSURE: Maximum differential pressure (Δp) and safety valve setting tolerance: ± 7 hPa (0.1 PSI). ± 6 hPa (0.1 PSI). ± 8 hPa (0.1 PSI). ± 9 hPa (0.1 PSI).

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU START: After 3 consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt. After 4 consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt. After 6 consecutive APU start attempts, the flight crew must wait 30 min before a new start attempt. After 4 consecutive APU start attempts, the flight crew must wait 30 min before a new start attempt.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. ROTOR SPEED: Maximum N speed: 107 %. 106 %. 105 %. 104 %.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. EGT: Maximum EGT for APU start (below 35000 ft): 1090 °C. 1120 °C. 1085 ºC. 675 °C.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. EGT: Maximum EGT for APU start (above 35000 ft): 1090 ºC. 1120 ºC. 675 ºC. 1085 ºC.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. EGT: Maximum EGT for APU running: 1090 ºC. 1120 ºC. 1085 ºC. 675 ºC.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU BLEED. Max altitude to assist engine start: 20000 ft. 22500 ft. 22000 ft. 15000 ft.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU BLEED. Max altitude for air conditioning and pressurization (single pack operation): 22500 ft. 22000 ft. 20000 ft. 15000 ft.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU BLEED. Max altitude for air conditioning and pressurization (dual pack operation): 15000 ft. 22000 ft. 22500 ft. 20000 ft.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. CABIN PRESSURE: Outflow valve closure: 15000 ft. 20000 ft. 22000 ft. 25000 ft.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. CABIN PRESSURE: Max cabin alt selection : 14000 ft. 15000 ft. 20000 ft. 22500 ft.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. CABIN PRESSURE: Cab Alt Warning: 9550 ft (± 350 ft). 9250 ft (± 350 ft). 9550 ft (± 250 ft). 9350 ft (± 350 ft).

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. CABIN PRESSURE: Max Norm Cab Alt: 8000 ft. 9000 ft. 9200 ft. 8200 ft.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. CABIN PRESSURE: Min Cabin Alt Selection: -2000 ft. -2200 ft. -2500 ft. -2250 ft.

A320 / A321 (IBS fleet). AIR BLEED/COND/PRESS/VENT. CABIN PRESSURE: Max Operating Altitudes: 39100 ft / 39800 ft. 39200 ft / 39800 ft. 39100 ft / 39700 ft. 39200 ft / 39850 ft.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU BLEED. OPERATIONAL ENVELOPE. Max APU Operation and Normal Restart Limit pressure altitude (between -72 ºC / -22 ºC aprox.): 41000 ft. 40000 ft. 39000 ft. 39500 ft.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU BLEED. OPERATIONAL ENVELOPE. APU Elec Power Only pressure altitude interval (between -72 ºC / -60 ºC (top of the graph) and -22 ºC / +5 ºC aprox. (bottom of the graph)): 41000 ft / 22500 ft. 41000 ft / 25000 ft. 40000 ft / 22500 ft. 40000 ft / 25000 ft.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU BLEED. OPERATIONAL ENVELOPE. APU Bleed Air and Elec Power Only pressure altitude interval (between -60 ºC / -58 ºC and +5 ºC / +58 ºC aprox.): 22500 ft / -2000 ft. 25000 ft / -2000 ft. 20000 ft / -2000 ft. 20000 ft / -2000 ft.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU BLEED. OPERATIONAL ENVELOPE. APU Battery Restart Limit (Elec Emerg Config) pressure altitude: 25000 ft. 22500 ft. 20000 ft. 22000 ft.

A320 / A321 (IBS fleet). AUXILIARY POWER UNIT. GENERAL. APU BLEED. OPERATIONAL ENVELOPE. APU Ground Operation pressure altitude interval (between -58 ºC and +24 ºC / +58 ºC aprox.): 14750 ft / -1000 ft. 14500 ft / -1500 ft. 14250 ft / -1250 ft. 14250 ft / -1100 ft.

A320 / A321 (IBS fleet). COMMUNICATION. GSM ONBOARD. The use of mobile phones is prohibited in the toilets and the cockpit. It is prohibited to use the GSM Onboard System: ‐ Below _____ (approximately ____). ‐ In some geographical areas (refer to the “Regional Operation Data for the Onboard Mobile Telephony System” document for the identification of these geographical areas). 3000 m AGL; 10000 ft. 3000 m AMSL; 10000 ft. 3300 ft AGL; 1000 m. 3300 ft AMSL; 1000 m.

A320 / A321 (IBS fleet). ENGINES. OIL. OIL PRESSURE. MIN/MAX Oil Pressure (ECAM Indication). Cold Start Bypass Valve Opens at... 305 PSI. 304 PSI. 300 PSI. 307 PSI.

A320 / A321 (IBS fleet). ENGINES. OIL. OIL PRESSURE. MIN/MAX Oil Pressure (ECAM Indication). Maximum Normal Oil Pressure at N2 105 %... 90 PSI. 100 PSI. 95 PSI. 80 PSI.

A320 / A321 (IBS fleet). ENGINES. OIL. OIL PRESSURE. MIN/MAX Oil Pressure (ECAM Indication). Minimum Normal Ground Oil Pressure (N2 105 % aprox.): 35 PSI. 50 PSI. 40 PSI. 45 PSI.

A320 / A321 (IBS fleet). ENGINES. STARTER: ‐ A standard automatic start that includes up to___start attempts, is considered one cycle. ‐ For ground starts (automatic or manual), a___pause is required between successive cycles. ‐ A___cooling period is required, subsequent to___failed cycles. ‐ The starter must not be run when N2 is above___. three; 20 s; 15 min; four; 20 %. three; 15 s; 20 min; four; 20 %. three; 20 s; 15 min; four; 15 %. four; 20 s; 15 min; three; 25 %.

A320-216 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank) < 2250 kg (4960 lb). Maximum Asymmetry... 1500 kg (3306 lb). 1600 kg (3527 lb). 2250 kg (4960 lb). No limitation. 1450 kg (3196 lb).

A320-216 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. OUTER TANKS. Maximum Asymmetry... 690 kg (1521 lb). 1500 kg (3306 lb). 1600 kg (3527 lb). 2250 kg (4960 lb). No limitation.

A320-214 (IBS fleet). ENGINES. REDUCED THRUST TAKEOFF. FLEX TAKEOFF. Takeoff at reduced thrust, so-called as FLEX takeoff, is permitted only if the airplane meets all performance requirements at the takeoff weight, with the operating engines at the thrust available for the flexible temperature (TFLEX). Takeoff at reduced thrust is permitted with any inoperative item affecting the performance only if the associated performance shortfall has been applied to meet the above requirements. FLEX takeoff is not permitted on contaminated runways. TFLEX cannot be: ‐ Higher than TMAXFLEX, equal to___. TMAXFLEX corresponds to a reduction of___from the full rated takeoff thrust. ‐ ___than the flat temperature (TREF). ‐ ___than the actual OAT. ISA +53 °C ; 25 % ; Lower ; Lower. ISA +52 °C ; 25 % ; Higher ; Lower. ISA +52 °C ; 23 % ; Lower ; Lower. ISA +53 °C ; 23 % ; Lower ; Lower.

A320-216 (IBS fleet). ENGINES. REDUCED THRUST TAKEOFF. FLEX TAKEOFF. Takeoff at reduced thrust, so-called as FLEX takeoff, is permitted only if the airplane meets all performance requirements at the takeoff weight, with the operating engines at the thrust available for the flexible temperature (TFLEX). Takeoff at reduced thrust is permitted with any inoperative item affecting the performance only if the associated performance shortfall has been applied to meet the above requirements. FLEX takeoff is not permitted on contaminated runways. TFLEX cannot be: ‐ Higher than TMAXFLEX, equal to___. TMAXFLEX corresponds to a reduction of___from the full rated takeoff thrust. ‐ ___than the flat temperature (TREF). ‐ ___than the actual OAT. ISA +70 °C ; 25 % ; Lower ; Lower. ISA +75 °C ; 25 % ; Lower ; Lower. ISA +75 °C ; 25 % ; Higher ; Lower. ISA +70 °C ; 23 % ; Lower ; Lower.

A321-213 (IBS fleet). ENGINES. REDUCED THRUST TAKEOFF. FLEX TAKEOFF. Takeoff at reduced thrust, so-called as FLEX takeoff, is permitted only if the airplane meets all performance requirements at the takeoff weight, with the operating engines at the thrust available for the flexible temperature (TFLEX). Takeoff at reduced thrust is permitted with any inoperative item affecting the performance only if the associated performance shortfall has been applied to meet the above requirements. FLEX takeoff is not permitted on contaminated runways. The flexible takeoff thrust must never be below the MCT at___. TFLEX cannot be: ‐ Higher than TMAXFLEX, equal to___. ‐ ___than the flat temperature (TREF). ‐ ___than the actual OAT. ISA +40 °C ; ISA + 43 °C ; Lower ; Lower. ISA +43 °C ; ISA + 40 °C ; Lower ; Lower. ISA +43 °C ; ISA + 40 °C ; Higher ; Lower. ISA +40 °C ; ISA + 43 °C ; Higher ; Lower.

A320 / A321 (IBS fleet). ENGINES. REVERSE THRUST. Selection of the reverse thrust is prohibited in flight. Backing the aircraft with reverse thrust is not permitted. Maximum reverse should not be used below___. Idle reverse is permitted down to aircraft stop. 70 kt. 75 kt. 60 kt. 65 kt.

A320 / A321 (IBS fleet). FUEL. CERTIFIED FUEL. In accordance with engine manufacturers and fuel specifications the fuel system is certified with... JET A, JET A1, JET B, JP4, JP5, JP8, N° 3 JET, RT, and TS-1. JET A, JET A1, JET B, JP1, JP5, JP8, N° 3 JET, RT, and TS-1. JET A, JET A1, JET B, JP4, JP2, JP8, N° 3 JET, RT, and TS-1. JET A, JET A1, JET B, JP4, JP5, JP7, N° 3 JET, RT, and TS-1.

A320 / A321 (IBS fleet). FUEL. FUEL TEMPERATURE. The minimum temperatures of JET A1/JP8/N°3 JET, JET A, JP5, RT TS-1, JET B, JP4 are respectively... -43 °C, -36 °C, -42 °C, -45 °C, -45 °C, -46 °C, -54 °C. -36 °C, -43 °C, -42 °C, -45 °C, -45 °C, -46 °C, -54 °C. -36 °C, -42 °C, -43 °C, -45 °C, -45 °C, -46 °C, -54 °C. -43 °C, -36 °C, -42 °C, -45 °C, -45 °C, -54 °C, -46 °C.

A320 / A321 (IBS fleet). FUEL. FUEL TEMPERATURE. The maximum temperatures of JET A1/JP8/N°3 JET, JET A, JP5, RT TS-1(___), JET B, JP4 (___) are... 54 ºC ; 49 ºC. 49 ºC ; 54 ºC. 59 ºC ; 44 ºC. 44 ºC ; 59 ºC.

A320-214/216 (IBS fleet). FUEL. FUEL TEMPERATURE LIMITS WHEN JP4 AND JET B FUELS ARE USED. If the wing fuel temperature exceeds 30 °C at engine start, the altitude must be limited to___until the center tank is empty. 35000 ft. 30000 ft. 25000 ft. 22500 ft.

A320-214/216 (IBS fleet). FUEL. FUEL TEMPERATURE LIMITS WHEN JP4 AND JET B FUELS ARE USED. If the wing fuel temperature exceeds 40 °C at engine start, the altitude must be limited to___until the center tank is empty. 35000 ft. 30000 ft. 25000 ft. 22500 ft.

A320-214/216 (IBS fleet). FUEL. FUEL TEMPERATURE LIMITS WHEN JP4 AND JET B FUELS ARE USED. If the wing fuel temperature exceeds 49 °C at engine start, the altitude must be limited to___until the center tank is empty. 35000 ft. 30000 ft. 25000 ft. 22500 ft.

A321(IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. Tank Fuel Quantity (Heavier Tank): 2350 kg (5180 lb). Maximum Asymmetry... 1500 kg (3306 lb). 1600 kg (3527 lb). 2250 kg (4960 lb). 2350 kg (5180 lb). No limitation.

A321(IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. Tank Fuel Quantity (Heavier Tank): Full. Maximum Asymmetry... 1200 kg (2646 lb). 1320 kg (2910 lb). 1450 kg (3196 lb). 2250 kg (4960 lb). No limitation.

A321(IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. Tank Fuel Quantity (Heavier Tank): 3400 kg (7496 lb). Maximum Asymmetry... 600 kg (1323 lb). 1050 kg (2314 lb). 1600 kg (3527 lb). 2350 kg (5180 lb). No limitation.

A321(IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. Tank Fuel Quantity (Heavier Tank): 4000 kg (8818 lb). Maximum Asymmetry... 1200 kg (2646 lb). 1450 kg (3196 lb). 1050 kg (2314 lb). 2250 kg (4960 lb). No limitation.

A321(IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. Tank Fuel Quantity (Heavier Tank): Full. Maximum Asymmetry... 600 kg (1323 lb). 1200 kg (2646 lb). 1450 kg (3196 lb). 2350 kg (5180 lb). No limitation.

A321(IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. Tank Fuel Quantity (Heavier Tank): 1200 kg (2646 lb). Maximum Asymmetry... 600 kg (1323 lb). 1200 kg (2646 lb). 1450 kg (3196 lb). 1300 kg (3527 lb). No limitation.

A321(IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. Tank Fuel Quantity (Heavier Tank) < 2350 kg (5180 lb). Maximum Asymmetry... 1500 kg (3306 lb). 1600 kg (3527 lb). 2250 kg (4960 lb). 1450 kg (3196 lb). No limitation.

A320 / A321 (IBS fleet). FUEL. MINIMUM FUEL QUANTITY FOR TAKEOFF. Minimum fuel quantity for takeoff... 1500 kg (3307 lb). 1600 kg (3527 lb). 1450 kg (3196 lb). 1050 kg (2314 lb).

A320 / A321 (IBS fleet). ICE AND RAIN PROTECTION. DEFINITION OF ICING CONDITIONS. ‐ Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is at or below___and visible moisture in any form is present (such as clouds, fog with visibility of one nautical mile or less, rain, snow, sleet or ice crystals). ‐ Icing conditions also exist when the OAT on the ground and for takeoff is at or below___and operating on ramps, taxiways or runways where surface snow, standing water or slush may be ingested by the engines, or freeze on engines, nacelles or engine sensor probes. -10 ºC. 10 ºC. -15 ºC. 15 ºC.

A320 / A321 (IBS fleet). ICE AND RAIN PROTECTION. DEFINITION OF ICING CONDITIONS. DEFINITION OF SEVERE ICE ACCRETION. Ice accretion is considered severe when the ice accumulation on the airframe reaches approximately 5 mm (0.2 in) thick or more. Ice accretion is considered severe when the ice accumulation on the airframe reaches approximately 2 mm (0.5 in) thick or more. Ice accretion is considered severe when the ice accumulation on the airframe reaches approximately 5 mm (0.5 in) thick or more. Ice accretion is considered severe when the ice accumulation on the airframe reaches approximately 5 mm (0.25 in) thick or more.

A320 / A321 (IBS fleet). LANDING GEAR. NOSEWHEEL STEERING (NWS). Towbarless operation on the nose landing gear (towing and pushback) is approved when using the accepted towbarless towing vehicles listed in the Airbus WISE ISI 09.11.00001, with the following information: Maximum NWS angle ± 85°. Maximum NWS angle ± 95°. Maximum NWS angle ± 75°. Maximum NWS angle ± 70°.

A320 / A321 (IBS fleet). LANDING GEAR. TAXI WITH DEFLATED OR DAMAGED TIRES. To vacate the runway or taxi at low speed with tire(s) deflated (not damaged), all of the following limitations apply: ‐ If maximum one tire per gear is deflated (consider three gears) Maximum taxi speed during turn___. ‐ If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed___. ‐ For the nosewheel steering (NWS) angle Maximum NWS angle___. 7 kt; 3 kt; 30º. 5 kt; 3 kt; 35º. 7 kt; 4 kt; 30º. 7 kt; 3 kt; 35º.

A320 / A321 (IBS fleet). NAVIGATION. INERTIAL REFERENCE SYSTEM (IRS). IR GROUND ALIGNMENT. Depending on the kind of device the ground alignment of the IRS is possible in latitudes between___and___. 73° North and 73° South; 82° North and 82° South. 72° North and 72° South; 83° North and 83° South. 72° North and 73° South; 82° North and 83° South. 73° North and 72° South; 83° North and 82° South.

A320 / A321 (IBS fleet). NAVIGATION. INERTIAL REFERENCE SYSTEM (IRS). MAGNETIC (MAG) REFERENCE. If all ADIRUs have the same magnetic variation table: In NAV mode, depending on the kind of device, the IR will not provide valid magnetic heading and magnetic track angle: - North of 73° North, and South of 60° South; - North of 73° North, between 90° West and 120° West (magnetic polar region), and North of 82° North, and South of 60° South. - North of 73° North, and South of 82° South; - North of 73° North, between 90° West and 120° West (magnetic polar region), and North of 60° North, and South of 60° South. - North of 73° North, and South of 60° South; - North of 73° North, between 90° East and 120° East (magnetic polar region), and North of 82° North, and South of 60° South. - North of 73° North, and South of 82° South; - North of 73° North, between 90° East and 120° East (magnetic polar region), and North of 60° North, and South of 60° South.

A320 / A321 (IBS fleet). NAVIGATION. INERTIAL REFERENCE SYSTEM (IRS). MAGNETIC (MAG) REFERENCE. If one ADIRUs have the different magnetic variation table: In NAV mode the IR will not provide valid magnetic heading and magnetic track angle: North of 60° North, between 30° West and 160° West, and North of 73° North, and South of 55° South. North of 60° North, between 55° West and 160° West, and North of 73° North, and South of 30° South. North of 60° North, between 30° East and 160° East, and North of 73° North, and South of 55° South. North of 60° North, between 55° East and 160° East, and North of 73° North, and South of 30° South.

A320 / A321 (IBS fleet). OXYGEN. MINIMUM FLIGHT CREW OXYGEN PRESSURE. With respect to the REF Temperature / MIN Bottle Pressure (PSI) table, on ground, the REF Temperature formula is... REF Temperature = (OAT + Cockpit TEMP) / 2. REF Temperature = (OAT - Cockpit TEMP) / 2. REF Temperature = (OAT + Cockpit TEMP) x 2. REF Temperature = (OAT - Cockpit TEMP) x 2.

A320 / A321 (IBS fleet). OXYGEN. MINIMUM FLIGHT CREW OXYGEN PRESSURE. With respect to the REF Temperature / MIN Bottle Pressure (PSI) table, in flight, the REF Temperature formula is... REF Temperature = CAB TEMP (°C) - 10 °C, or REF Temperature = CAB TEMP (°F) - 18 °F. REF Temperature = CAB TEMP (°C) - 18 °C, or REF Temperature = CAB TEMP (°F) - 10 °F. REF Temperature = CAB TEMP (°C) + 10 °C, or REF Temperature = CAB TEMP (°F) + 18 °F. REF Temperature = CAB TEMP (°C) + 18 °C, or REF Temperature = CAB TEMP (°F) + 10 °F.

A320 / A321 (IBS fleet). OXYGEN. MINIMUM FLIGHT CREW OXYGEN PRESSURE. With respect to the REF Temperature / MIN Bottle Pressure (PSI) table, the minimum Bottle Pressure covers: ‐ Preflight checks. ‐ The use of oxygen, when only one flight crewmember is in the cockpit. ‐ Unusable quantity (to ensure regulator operation with minimum pressure). ‐ Normal system leakage. ‐ The most demanding case among the following: • Protection after loss of cabin pressure, with mask regulator on NORMAL (diluted oxygen): ▪ During emergency descent for all flight crewmembers and observers for___min. ▪ During cruise at FL 100 for two flight crewmembers for___min. • Protection against smoke with 100 % oxygen for all flight crewmembers and observers during___min at 8000 ft cabin altitude. 13; 107; 15. 13; 15; 107. 15; 106; 13. 15; 107; 13.

A320 / A321 (IBS fleet). SURVEILLANCE. GPWS / PREDICTIVE GPWS <*I. The predictive GPWS <*I functions should be inhibited (TERR pushbutton to OFF, on the GPWS panel) when the aircraft position is less than... 15 NM from the airfield: ‐ For operations from/to runways not incorporated in the predictive GPWS database. ‐ For specific approach procedures, which were previously identified as potentially causing false terrain alerts. 10 NM from the airfield: ‐ For operations from/to runways not incorporated in the predictive GPWS database. ‐ For specific approach procedures, which were previously identified as potentially causing false terrain alerts. 20 NM from the airfield: ‐ For operations from/to runways not incorporated in the predictive GPWS database. ‐ For specific approach procedures, which were previously identified as potentially causing false terrain alerts. 5 NM from the airfield: ‐ For operations from/to runways not incorporated in the predictive GPWS database. ‐ For specific approach procedures, which were previously identified as potentially causing false terrain alerts.

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): Full. Maximum Asymmetry... 500 kg (1102 lb). 1050 kg (2314 lb). 1320 kg (2910 lb). 1500 kg (3306 lb). No limitation.

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): 3000 kg (6613 lb). Maximum Asymmetry... 500 kg (1102 lb). 1050 kg (2314 lb). 1450 kg (3196 lb). 2250 kg (4960 lb). No limitation.

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): 1450 kg (3196 lb). Maximum Asymmetry... 500 kg (1102 lb). 1050 kg (2314 lb). 1450 kg (3196 lb). 1300 kg (3527 lb). No limitation.

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE AT TAKEOFF. OUTER TANKS (INNER TANKS BALANCED). Maximum Asymmetry... 370 kg (815 lb). 1050 kg (2314 lb). 1450 kg (3196 lb). 690 kg (1521 lb). No limitation.

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): Full. Maximum Asymmetry... 1450 kg (3196 lb). 1500 kg (3306 lb). 2350 kg (5180 lb). 1600 kg (3527 lb). No limitation.

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): 4300 kg (9479 lb). Maximum Asymmetry... 1450 kg (3196 lb). 1500 kg (3306 lb). 1600 kg (3527 lb). 2350 kg (5180 lb). No limitation.

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank): 2250 kg (4960 lb). Maximum Asymmetry... 1450 kg (3196 lb). 1500 kg (3306 lb). 1600 kg (3527 lb). 2250 kg (4960 lb). No limitation.

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. INNER TANKS (OUTER TANKS BALANCED). Tank Fuel Quantity (Heavier Tank) < 2250 kg (4960 lb). Maximum Asymmetry... 1500 kg (3306 lb). 1600 kg (3527 lb). 2250 kg (4960 lb). No limitation. 1450 kg (3196 lb).

A320-214 (IBS fleet). FUEL. MAXIMUM ALLOWED FUEL IMBALANCE. FUEL IMBALANCE IN FLIGHT AND AT LANDING. OUTER TANKS. Maximum Asymmetry... 690 kg (1521 lb). 1500 kg (3306 lb). 1600 kg (3527 lb). 2250 kg (4960 lb). No limitation.

A320 / A321 (IBS fleet). OPERATIONS MANUAL PARTE B. ASUNTOS DE LA AERONAVE. PROCEDIMIENTOS NORMALES. The use of TCAS shall be as per AIRBUS policy: The flight crew shall select... ABV in climb (+9900 ft / -2700 ft). ABV in climb (+9700 ft / -2900 ft). ALL in climb (+9900 ft / -2700 ft). ALL in climb (+9900 ft / -2700 ft).

A320 / A321 (IBS fleet). OPERATIONS MANUAL PARTE B. ASUNTOS DE LA AERONAVE. PROCEDIMIENTOS NORMALES. The use of TCAS shall be as per AIRBUS policy: The flight crew shall select... ABV in climb (+9700 ft / -2900 ft). ALL in cruise (+9700 ft / -2900 ft). ALL in cruise (+2700 ft / -2700 ft). ALL in climb (+2900 ft / -2700 ft).

A320 / A321 (IBS fleet). OPERATIONS MANUAL PARTE B. ASUNTOS DE LA AERONAVE. PROCEDIMIENTOS NORMALES. The use of TCAS shall be as per AIRBUS policy: The flight crew shall select... BLW, if the cruise altitude is within 2000 ft of FL410, or in descent (+2700 ft / -9900 ft). BLW, if the cruise altitude is within 2000 ft of FL410, or in descent (+2900 ft / -9700 ft). BLW, if the cruise altitude is within 2000 ft of FL410, or in descent (+9900 ft / -2700 ft). BLW, if the cruise altitude is within 2000 ft of FL410, or in descent (+9700 ft / -2900 ft).