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Airbus A320 Aircraft Limitations and Performance Study Guide, Exams of Social Sciences

United States International UniversitySocial Sciences

This study guide provides essential operational limitations and performance parameters for the airbus a320 aircraft. It covers maximum weights, load factors, runway conditions, wind limitations, flap speeds, engine parameters, and autopilot minimum heights. Useful for pilots, flight engineers, and aviation students seeking to understand the a320's operational constraints and performance capabilities. It includes critical data for safe and efficient flight operations, such as fuel temperature limits, hydraulic pressure, and apu operational guidelines. The guide also details engine start cycles and reverse thrust rules, providing a comprehensive overview of the aircraft's operational parameters.

Typology: Exams

2025/2026

Available from 12/18/2025

ROCKY-B
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AIRBUS A320 STUDY GUIDE
Maximum taxi weight - Answer -170,600
Maximum takeoff weight - Answer -169,700
Maximum landing weight - Answer -142,200
Maximum zero fuel weight - Answer -134,400
Minimum Weight - Answer -82,078
Maximum Load Clean Configuration - Answer --1 to +2.5
Load Slats and Flaps Extended - Answer -0 to +2
Max Load Slat and Flaps Extended - Answer -0 to +2
Max Load Slats Extended, Flaps Retracted - Answer -0 to +2
Aircraft Ceiling - Answer -39,100
Runway Slope - Answer --2% to +2%
Max Runway Altitude - Answer -9200 feet
Normal Runway Width - Answer -150
Maximum Demonstrated xwind takeoff - Answer -29 knots gusting 38 knots
Maximum Demonstrated xwind landing - Answer -33 to 38
Maximum tail wind - Answer -10 knots
Maximum door operation - Answer -65 knots
Max wind cargo door ops open - Answer -40 knots
Max wind cargo door ops close - Answer -< 65 knots
Max Flap Speed configuration 1 - Answer -230 knots
Max Flap Speed Config 1+F - Answer -215
Max Flap Speed Config 2 - Answer -200
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AIRBUS A320 STUDY GUIDE

Maximum taxi weight - Answer - 170, Maximum takeoff weight - Answer - 169, Maximum landing weight - Answer - 142, Maximum zero fuel weight - Answer - 134, Minimum Weight - Answer - 82, Maximum Load Clean Configuration - Answer --1 to +2. Load Slats and Flaps Extended - Answer - 0 to + Max Load Slat and Flaps Extended - Answer - 0 to + Max Load Slats Extended, Flaps Retracted - Answer - 0 to + Aircraft Ceiling - Answer - 39, Runway Slope - Answer --2% to +2% Max Runway Altitude - Answer - 9200 feet Normal Runway Width - Answer - 150 Maximum Demonstrated xwind takeoff - Answer - 29 knots gusting 38 knots Maximum Demonstrated xwind landing - Answer - 33 to 38 Maximum tail wind - Answer - 10 knots Maximum door operation - Answer - 65 knots Max wind cargo door ops open - Answer - 40 knots Max wind cargo door ops close - Answer - < 65 knots Max Flap Speed configuration 1 - Answer - 230 knots Max Flap Speed Config 1+F - Answer - 215 Max Flap Speed Config 2 - Answer - 200

Max Flap Speed Config 3 - Answer - 185 Max Flap Speed Config Full - Answer - 177 VMO - Answer - 350 or .82 mach VLE - Answer - 280 or. VLO - Answer - 250 extension 220 retract Maximum Altitude for Gear Extension - Answer - 25, Maximum Tire Speed - Answer - 195 knots Maximum Windshield Wiper Speed - Answer - 230 knots Max Cockpit window open Speed - Answer - 200 knots Minimum Height Autopilot on Takeoff - Answer - 100 AGL Minimum Height Autopilot Straight in Non Prec Approach - Answer - MDA Min Height Autopilot Circling non precision approach - Answer - MDA - 100 Minimum Height Autopilot Cat1 - Answer - 160 Min Height Autopilot Go Around - Answer - 100 Min Height Auto Pilot all other phases - Answer - 500 feet Cat 2 Min Decision Height - Answer - 100 AGL Cat 3 Dual Alert Height - Answer - 100 AGL Cat 3 minimum RVR - Answer - 75 feet Max Wind AP landing rollout - Answer - HW 30, TW 10, XW 15 Max Altitude Slat and Flaps Extended - Answer - FL Maximum Continuous load per generator - Answer - 100% 90 KVA Maximum continuous load per transformer - Answer - 200 amps Max winds with Auto Pilot - Answer - 30 headwind, 10 tailwind, and 15 crossword

Max Transient Oil Temp - Answer - 165 C not longer than 15 minutes Minimum Oil Pressure - Answer - 60 PSI Max cross wind for engine start - Answer - 35 knots Max N1 and N2 - Answer - 100% for both Engine Start Cycle - Answer - 2 min then 15 off, 2 min then 15 sec off. After 4 minutes on, then 30 minutes off. Reverse Thrust Rules - Answer - No reverse thrust in flight, no reverse thrust to move backwards, no reverse thrust below 70 knots