A320 Neo Limitations for Pilots

FLIGHT MANEUVER LOAD ACCELERATION LIMITS CLEAN. -1 G TO +2.5 G. 0 G TO 2.0 G.

FLIGHT MANEUVER LOAD ACCELERATION LIMITS OTHER CONFIGURATIONS. -1 G TO +2.5 G. 0 G TO +2.0 G.

RUNWAY SLOPE. +/-2%. +/-2.5%.

RUNWAY ALTITUDE. 13100 FT. 14100 FT.

NOMINAL RUNWAY WIDTH. 30 mt. 45 mt.

MINIMAL RUNWAY WIDTH. 30 mt. 45 mt.

MAXIMUM DEMOSTRATED CROSSWIND. 40 kts. 38 kts.

TAILWIND FOR TAKEOFF AND LANDING. 15 kts. 10 kts.

TAILWIND GREATER THAN 10 KTS. FLAPS FULL RECOMENDED. FLAPS 3 RECOMENDED.

MAXIMUM WIND FOR PASSENGER DOOR. 65 KTS. 40 KTS.

MAXIMUM WIND FOR CARGO DOOR. 65 KTS. 40 KTS.

MAXIMUM COCKPIT WINDOW SPEED. 190 kts. 200 kts.

Vmo. 360 kts. 350 kts.

Mmo. 0.83. 0.82.

WIPERS MAXIMUM OPERATIONG SPEED. 230 kts. 240 kts.

MINIMUM CONTROL SPEED FOR LANDING (VMCL). 120 kts. 116 kts.

MAXIMUM TIRE SPEED. 195 kts. 185 kts.

TAXI WITH DEFLATED OR DAMAGED TIRES, IF MAXIMUM ONE TIRE PER GEAR IS DEFLATED (CONSIDERING THREE GEARS) MAXIMUM TAXI. 7 kts. 3 kts.

TAXI WITH DEFLATED OR DAMAGED TIRES, IF TWO TIRES ARE DEFLATED ON THE SAME MAIN GEAR (MAXIMUM ONE MAIN GEAR) MAXIMUM. 3 kts. 7 kts.

TAXI WITH DEFLATED OR DAMAGED TIRES, FOR THE NOSEWHEEL STEERING (NWS) ANGLE MAXIMUM NWS ANGLE. 20°. 30°.

MAXIMUM BRAKE TEMPERATURE FOR TAKEOFF. 300 °C. 350°C.

AFTER THREE CONSECUTIVE APU START ATTEMPTS, THE FLIGHT CREW MUST WAIT ____ MINUTES BEFORE A NEW START ATTEMPT. 30'. 60'.

MAXIMUM N SPEED. 107%. 108%.

MAXIMUM EGT FOR APU START ABOVE 35.000FT. 1120°C. 1130°C.

MAXIMUM EGT FOR APU START BELOW 35.000FT. 1080°C. 1090°C.

MAXIMUM EGT FOR APU RUNNING. 675°C. 685°C.

MAXIMUM ALTITUDE TO ASSIST ENGINE START. 20000 ft. 25000ft.

MAXIMUM ALTITUDE FOR AIR CONDITIONING AND PRESSURIZATION SINGLE PACK OPERATION. 22500 ft. 23500 ft.

MAXIMUM ALTITUDE FOR AIR CONDITIONING AND PRESSURIZATION DUAL PACK OPERATION. 16000 ft. 15000 ft.

USE OF APU BLEED AIR FOR WING ANTI-ICE IS?. NOT PERMITED. PERMITED.

ENVIROMENTAL ENVELOPE, TAKE OFF AND LANDING. -2000 ft to 14100 ft. -2000 ft to 14200 ft.

ENVIROMENTAL ENVELOPE, OPERATIONAL. 14200 ft to 39800 ft. 14100 ft to 39800 ft.

MAXIMUM TAXI WEIGHT. 77400 kg. 77500 kg.

MAXIMUM TAKE OFF WEIGHT. 77000 kg. 77400 kg.

MAXIMUM LANDING WEIGHT. 67400 kg. 64300 kg.

MAXIMUM ZERO FUEL WEIGHT. 67400 kg. 64300 kg.

MINIMUM WEIGHT. 40300 kg. 40200 kg.

A STANDARD AUTOMATIC START INCLUDES UP TO TWO START ATTEMPTS, IS CONSIDER ______CYCLE. ONCE. TWICE.

FOR GROUND STARTS (AUTOMATIC OR MANUAL), A ______ PAUSE IS REQUIRE BETWEEN SUCCESSIVE CYCLES. 35 SEC. 35 MIN.

A _____ COOLING PERIOD IS REQUIRED, SUBSEQUENT TO THREE FAILED CYCLES, OR 15 MIN OF CONTINUOUS OR CUMULATED CRANK. 15 MIN. 25 MIN.

THE STARTER MUST NOT BE RUN WHENM N2 IS ABOVE __%. 20%. 25%.

TAKEOFF AND GO-AROUND ALL ENGINES OPERATIVE TIME LIMIT____, EGT LIMIT____. 5 MIN, 1083 °C. 5 MIN, 1090 °C.

TAKEOFF AND GO-AROUND, ONE ENGINE INOPERATIVE TIME LIMIT___, EGT LIMIT___. 10 MIN, 1120°c. 10 MIN, 1083° C.

MAXIMUM CONTINUOUS THRUST (MCT), TIME LIMIT___, EGT LIMIT___. LIMITED 5 MIN, 1043°C. NOT LIMITED, 1043°C.

STARTING ON GROUND AND IN FLIGHT EGT LIMIT ___. 1090°C. 1083°C.

MAXIMUM N1 IN NORMAL OPERATION. 100%. 110%.

MAXIMUM N1 PERMITTED. 100%. 105%.

MAXIMUM N2 IN NORMAL OPERATION. 100%. 105%.

MAXIMUM N2 PERMITTED. 105%. 100%.

MAXIMUM OIL TEMPERATURE. 151°C. 150°C.

MINIMUM STARTING OIL TEMPERATURE. -30°C. -40°C.

MINIMUM OIL TEMPERATURE BEFORE TAKEOFF. 52°C. 50°C.

OIL QUANTITY OAT AT OR ABOVE -30 ºC. 14 QT. 16.5 QT.

OIL QUANTITY OAT BELOW -30 ºC. 16.5 QT. 16 QT.

MINIMUM OIL PRESSURE. 65 PSI. 75 PSI.

MAXIMUM OIL PRESSURE. 260 PSI. 270 PSI.

AUTOPILOT FUNCTION AT TAKE OFF. 100 FT AGL - 5 S AFTER L/O. 200 FT AGL - 5 AFTER L/O.

AUTOPILOT FUNCTION IN APPROACH WITH F-G/S. 400 FT AGL. 200 FT AGL.

AUTOPILOT FUNCTION IN APPROACH WITH FINAL APP, V/S OR FPA. 250 FT AGL. 200 FT AGL.

AUTOPILOT FUNCTION IN CIRCLING APPROACH. 200 FT AGL. 500 FT AGL.

AUTOPILOT FUNCTION ILS/MLS CAT1 DISPLAYED FMA. 160 FT AGL. 170 FT AGL.

AUTOPILOT FUNCTION ILS/MLS CAT2, CAT3 SINGLE, CAT3 DUAL FMA. 0 FT AGL IF NOT AUTOLAND. 0 FT AGL IF AUTOLAND.

AUTOPILOT FUNCTION GLS CAT1 DISPLAYED FMA. 160 FT AGL. 150 FT AGL.

AUTOPILOT FUNCTION GLS AUTOLAND DISPLAYED FMA. 0 FT AGL IF AUTOLAND. 20 FT AGL IF AUTOLAND.

AUTOPILOT FUNCTION LPV APPR1 DISPLAYED FMA. 160 FT AGL. 150 FT AGL.

AUTOPILOT FUNCTION AFTER MANUAL GO AROUND. 200 FT AGL. 100 FT AGL.

AUTOPILOT FUNCTION IN ALL OTHER PHASES. 500 FT AGL. 200 FT AGL.

AVIONICS VENTILATION OAT ≤ 49 °C. NO LIMITATION. 2 H.

AVIONICS VENTILATION 49 °C < OAT ≤ 55 °C. NO LIMITATION. 2 H.

AVIONICS VENTILATION 55 °C < OAT ≤ 60 °C. 1 H. 2 H.

AVIONICS VENTILATION 60 °C < OAT ≤ 64 °C. 0.5 H. 1 H.

MAXIMUM SPEED 0 FLAPS. VMO / MMO CRUISE. VMO / MMO DESCEND.

MAXIMUM SPEED FLAPS 1. 230 KTS HOLDING. 230 KTS CRUISE.

MAXIMUM SPEED 1+F. 215 KTS APPROACH. 215 KTS TAKE OFF.

MAXIMUM SPEED FLAPS SLATS 2. 200 KTS TAKE OFF / APPROACH. 210 KTS TAKE OFF / APPROACH.

MAXIMUM SPEED SLAT/FLAP 3. 185 KTS TAKEOFF/APPROACH/LANDING. 190 KTS TAKEOFF/APPROACH/LANDING.

MAXIMUM SPEED FULL SLAT/FLAP. 177 LANDING. 167 LANDING.

MAXIMUM NWS ANGLE. +/- 85°. +/- 75°.

MINIMUM FUEL QUANTITY FOR TAKE OFF. 1400 KG. 1500 KG.

MAXIMUM ALTITUDE WITH SLATS/FLAPS EXTENDED. 20000 FT. 19000 FT.

HYDRAULIC FLUID NORMAL OPERATING PRESSURE. 3000 PSI (+/- 100). 3000 PSI (+/- 200).

RNP ACCURACY WITH GPS PRIMARY EN ROUTE WITH A/P ON. 1 NM. 3 NM.

RNP ACCURACY WITH GPS PRIMARY EN ROUTE WITH AUTOPILOT OFF AND FD ON. 1 NM. 0.3 NM.

RNP ACCURACY WITH GPS PRIMARY IN TERMINAL AREA WITH AUTOPILOT OFF AND FD ON. 0.51 NM. 1 NM.

RNP ACCURACY WITH GPS PRIMARY IN APPROACH AREA WITH AUTOPILOT OFF AND FD ON. 0.3 NM. 0.5 NM.

RNP ACCURACY WITH GPS PRIMARY WITH AUTOPILOT OFF AND FD OFF EN ROUTE. 1.1 NM. 3 NM.

RNP ACCURACY WITH GPS PRIMARY WITH AUTOPILOT OFF AND FD OFF IN TERMINAL AREA. 3 NM. 0.51 NM.

RNP ACCURACY WITH GPS PRIMARY WITH AUTOPILOT OFF AND FD OFF IN APPROACH. 0.3 NM WITH F-LOC/ NOT AUTHORIZED WITHOUT F-LOC. 0.3 NM WITH F-LOC AUTHORIZED WITHOUT F-LOC.

RNP ACCURACY WITH GPS PRIMARY IN TERMINAL AREA. 0.5 NM. 0.3 NM.

RNP ACCURACY WITH GPS PRIMARY IN APPROACH. 0.3 NM. 0.5 NM.

MAXIMUM SPEED WITH THE LANDING GEAR EXTENDED (VLE). 280 KTS / M 0.67. 250 KTS / M 0.60.

MAXIMUM SPEED AT WICH THE LANDING GEAR MAY BE EXTENDED (VLO) EXTENSION. 220 KTS / M 0.54. 250 KTS / M 0.60.

MAXIMUM SPEED AT WICH THE LANDING GEAR MAY BE RETRACTED (VLO) RETRACTION. 220 KTS / M 0.54. 210 KTS / M 0.52.

MAXIMUM BRAKE TEMPERATURE FOR TAKE OFF. 150°C. 300°C.

MAXIMUM PEDALS ANGLE. 6°. 10°.

MAXIMUM NW EFFECTIVE ANGLE. 85°. 75°.

TURBULENCE SPEED UP TO FL 200. 260 KTS. 250 KTS.

TURBULENCE SPEED UP TO FL 310. 275 KTS. 285 KTS.

TURBULENCE SPEED UP TO FL 390. 0.76 M. 0.75 M.

MAXIMUM FUEL ASYMETRY INNER TANKS FULL IN FLIGHT AND LANDING. 1500 KG. 1600 KG.

MAXIMUM FUEL ASYMETRY INNER TANKS WITH 4300 KG IN FLIGHT AND LANDING. 1600 KG. 1500KG.

MAXIMUM FUEL ASYMETRY INNER TANKS WITH 2250 KG IN FLIGHT AND LANDING. 2250 KG. 2200 KG.

MAXIMUM FUEL ASYMETRY INNER TANKS WITH FUEL AT TAKE OFF. 500 KG. 600 KG.

MAXIMUM FUEL ASYMETRY INNER TANKS WITH 3000 KG AT TAKE OFF. 1450 KG. 1050 KG.

MAXIMUM FUEL ASYMETRY INNER TANKS WITH 1450 KG AT TAKE OFF. 1450 KG. 1050.

OUTER TANKS INNER BALANCE MAXIMUM ASYMETRY. 350 KG. 370 KG.

OUTER TANKS INNER BALANCE MAXIMUM ASYMETRY. 690 KG. 600 KG.

MINIMUM FUEL TEMPERATURE. -43°C. -40°C.

MAXIMUM FUEL TEMPERATURE. 60°C. 55°C.

MAXIMUM REVERSE SHOULD NOT BE USED BELOW. 70 KTS. 60 KTS.

MINIMUM HEIGHT FOR USE AUTOPILOT IN PAR (PRECISION APPROACH RADAR ) APPROACH. 250 FT AGL. 500 FT AGL.