A320 Family SOP
This SOP is valid for all aircraft types within the A320 family.
1. Introduction
1.1 Purpose
This handbook provides a structured introduction and operational guidance for the Airbus A320 fam...
1.2 Applicability
This handbook applies to the following aircraft types: Airbus A318 Airbus A319 Airbus A320 Airbu...
1.3 Philosophy
The Airbus A320 family is designed around automation and pilot monitoring. Key principles include...
1.4 Training Concept
This handbook is used as the primary training document for obtaining the virtual Airbus A320 Type...
1.5 Use of this Handbook
This handbook is intended to be used: During ground training As a reference during flight prepar...
2. Aircraft Overview
2.1 General Description
The Airbus A320 family is a series of narrow-body, twin-engine jet airliners designed for short- ...
2.2 Key Characteristics
The A320 family introduced several innovations that define modern airliner operations: Fly-By-Wir...
2.3 Cockpit Philosophy
The Airbus cockpit is designed around the concept of: βManage the flight path, monitor the automa...
2.4 Differences within the A320 Family
While cockpit operation remains largely identical, there are operational differences: A318 / A31...
2.5 Typical Operations
The A320 family is commonly used for: Short-haul routes Medium-haul routes High-frequency operat...
2.6 Summary
The Airbus A320 family combines: Advanced automation High commonality across variants Efficient ...
3. Cockpit Layout
3.1 General Layout
The Airbus A320 cockpit is designed for efficiency, clarity, and automation management. It is div...
3.2 Overhead Panel
The overhead panel is used to control and monitor aircraft systems. Main sections include: Elect...
3.3 Main Instrument Panel
This is the primary area for flight control and monitoring. Primary Flight Display (PFD) Displays...
3.4 Flight Control Unit (FCU)
The FCU is located on the glare shield and is used to control the autopilot. Functions include: ...
3.5 Pedestal
The pedestal contains systems used during active flight management. Thrust Levers Control engine...
3.6 Sidestick
Each pilot controls the aircraft using a sidestick. Characteristics: Independent for each pilot ...
3.7 Summary
The A320 cockpit is designed around: Automation Clear information display Efficient pilot intera...
4. Standard Operating Procedures (SOPs)
4.1 Cockpit Preparation
Objective To ensure the aircraft is correctly configured, powered, and programmed prior to engine...
4.2 Engine Start
Objective To safely start the engines while ensuring proper coordination with ground crew and mai...
4.3 Taxi
Objective To safely maneuver the aircraft from stand to runway while maintaining full control, si...
4.4 Takeoff
Line-Up PF: Align aircraft with runway centerline PM: Confirms runway and clearance Take...
4.5 Climb
Objective To establish a stable and efficient climb profile after takeoff. After Takeoff Flow At...
4.6 Cruise
Objective To maintain a stable and efficient flight at cruise altitude. Establishing Cruise Air...
4.7 Descent
Objective To conduct a controlled and passenger-comfort-oriented descent from cruise altitude to ...
4.8 Approach
Objective To establish a stable, controlled and smooth transition from descent into final approac...
4.9 Landing
Objective To safely land the aircraft from a stabilized approach and conduct a controlled rollout...
4.10 Taxi & Shutdown
Objective To safely taxi from the runway to the gate and perform complete aircraft shutdown while...
5. Checklists & Flows
5.1 Philosophy
Checklists are used to verify actions, not to perform them. All procedures follow the principle: ...
5.2 Cockpit Preparation
πΉ PM Flow (Overhead β Pedestal β Screens) BAT 1 + 2 β ON EXT PWR β ON Fuel Pumps β ON ADIRS (3x)...
5.3 Before Start
PM Flow Beacon β ON Doors β CLOSED Fuel Pumps β ON APU BLEED β ON πΉ PF Flow Confirm pushback ...
5.4 After Start
πΉ PM Flow ENG MODE β NORM APU BLEED β OFF APU β OFF Anti-Ice β AS REQUIRED Flaps β SET Pitch Tri...
5.5 Taxi
πΉPM Flow Flight Controls β CHECK (ECAM) Brake Temp β CHECK Taxi Lights β ON Takeoff Config β VER...
5.6 Before Takeoff
πΉ PM Flow Cabin β READY ECAM β NORMAL Takeoff Config β CHECK πΉ PF Flow Line-up briefing Final...
5.7 After Takeoff
πΉ PM Flow Gear β UP (on command) Flaps β RETRACT (on schedule) Packs β ON πΉ PF Flow Follow FD...
5.8 Approach
πΉ PM Flow Minimums β SET Nav Aids β SET ECAM β CHECK πΉ PF Flow Approach Briefing Mode setup ...
5.9 Landing
πΉ PM Flow Gear β DOWN Flaps β FULL Speed β CHECK πΉ PF Flow Stabilize approach Monitor FD β ...
5.10 After Landing
πΉ PM Flow Spoilers β RETRACT Flaps β UP APU β START πΉ PF Flow Taxi control Vacate runway β ...
5.11 Shutdown
πΉ PM Flow Engines β OFF Beacon β OFF External Power β ON πΉ PF Flow Parking Brake β SET Confir...
5.12 Key Principles
Flows must be consistent Checklists must not be skipped PF/PM roles must be respected Core Rul...
6. MCDU / FMS Guide
6.1 Objective
The MCDU (Multipurpose Control and Display Unit) is used to manage: Flight planning Navigation P...
6.2 INIT A Page
Used for basic flight initialization. Required Entries: FROM / TO β Departure & Destination FLT ...
6.3 Flight Plan Page
Route Input: Insert waypoints / airways Select SID and runway Insert STAR and approach Importa...
6.4 INIT B Page
Fuel & Weight: Block Fuel β INSERT Zero Fuel Weight β INSERT Importance: Incorrect values will...
6.5 Performance Pages
Takeoff (PERF TO) V1 / VR / V2 β INSERT FLEX Temperature β SET Thrust Reduction Altitude β SET A...
6.6 Key Pilot Tasks and common errors
Key Pilot Tasks During all phases: Monitor flight plan Check for route deviations Verify altitud...
6.7 Crosscheck Concept
Every critical input must be: Entered by PF Verified by PM Core Rule βGarbage in β Garbage out...
7. Flight Handling & Airbus Philosophy
7.1 Objective and Philosophy
Objective To understand how to properly control and manage the Airbus A320 using automation, whil...
7.2 Managed vs Selected Mode
This is the most important concept in Airbus operations. Managed Mode Aircraft follows FMGS fli...
7.3 Flight Director (FD)
The Flight Director provides guidance via crossbars on the PFD. Key Rule π The aircraft must fol...
7.4 Flight Mode Annunciator (FMA)
Located at the top of the PFD. Importance The FMA shows: Active modes Armed modes Autothrust st...
7.5 Thrust Management
The A320 uses fixed thrust detents: IDLE CL (Climb) FLX/MCT TOGA Key Concept Thrust levers ar...
7.6 Energy Management
Energy = Speed + Altitude Good Energy State On profile Correct speed Minimal corrections requir...
7.7 Automation Discipline
Pilots must: Understand active modes Anticipate aircraft behavior Intervene early Common Mista...
7.8 Manual Flying
Manual flying is required: During training In abnormal situations When automation is not appropr...
7.9 Situational Awareness
Pilots must always know: Where the aircraft is going What the aircraft is doing What will happen...
8. Abnormal Procedures
8.1 Objective and Philosophy
Objective To provide simplified guidance for handling non-normal situations in a safe and structu...
8.2 ECAM Philosophy
The ECAM system provides: Automatic failure detection System information Step-by-step actions ...
8.3 Engine Failure After Takeoff
Maintain runway track Thrust β TOGA Positive climb β Gear UP At safe altitude: Engage autopilo...
8.4 Unstable Approach and Go-Around
Unstable Approach Go-around if: Not stabilized (see SOP criteria) Incorrect speed or configurati...
8.5 TCAS (RA)
Follow TCAS commands immediately Disconnect autopilot if required
9. Performance & Limits
9.1 Objective
This chapter provides a structured understanding of the Airbus A320 performance fundamentals and ...
9.2 Takeoff Performance
V-Speeds Explained Before every departure, three critical speeds must be calculated and inserted ...
9.3 Approach & Landing Speeds
VAPP β Final Approach Speed VAPP is the target speed during final approach. It includes: Referen...
9.4 Flap Configuration & Limits
The Airbus A320 uses multiple flap configurations to adapt to different flight phases. Flap Sett...
9.5 Taxi Speed Limits
Taxi speed is critical for: Safety Passenger comfort Ground operations Standard Taxi Speeds N...
9.6 Cruise Performance
Typical Cruise Envelope Altitude: FL320 β FL390 Speed: Mach 0.76 β 0.80 Efficiency Considerati...
9.7 Descent Performance & Energy Management
Descent Characteristics Typically flown at idle thrust Vertical path controlled manually (VA SOP...
9.8 Operational Limits
Pilots must always respect: Speed limits (including flap limits) Aircraft configuration limits S...
9.9 Stabilized Approach as Performance Factor
A stabilized approach is the final expression of correct performance management. Requirements C...
9.10 Summary
Performance management in the A320 is based on: Proper planning Correct speed usage Respecting a...