Minimum Idle, Approach Idle and Reverse Idle Thrust – FADEC Control – Airbus A320
MINIMUM IDLE THRUST It is selected on ground when reverse is not selected It is selected in flight when the…
Beta Target and Sideslip Guidance – Engine Failure A320
In the event of an engine failure after takeoff or go around, the FAC (Flight Augmentation Computer) adjusts the sideslip…
Technical Questions: Landing Gear – Aircraft Systems
What is the purpose of auto brakes? Establish and maintain a consistent deceleration rate during landing, enhancing passenger comfort and…
Ice and Rain Protection: Airbus A320 Aircraft Systems
The Airbus A320 is equipped with sophisticated ice and rain protection systems to ensure safe and efficient operations in various…
Understanding OEBs: A Guide for A320 Pilots
OEBs are temporary directives issued to flight crews that must be applied under specific conditions to manage potential risks in…
Handling of MEL: Airbus A320
The Minimum Equipment List (MEL) is a critical document used to ensure the safe operation of aircraft when certain equipment…
Hydraulics: Airbus A320 Aircraft Systems
The aircraft features three hydraulic systems: green, yellow, and blue. The green and yellow systems are powered by engine-driven pumps,…
Fuel Penalty Factor – ELEC EMER CONFIG Procedure – A320
In the A320, the EMER ELEC CONFIG occurs when both the main generators fail or when an associated bus is…
Erroneous Mach Target Indicator on PFD (only for aircrafts equipped with DBUS) – A320
Issue: When the flight crew utilizes DBUS, the backup Mach target displayed on the right side of the speed tape…
Landing Gear: Airbus A320 Aircraft Systems
The landing gear system of the A320 consists of two main landing gears that retract inboard and one nose landing…