Black Friday Week – 20% off all home-use products
New

A330 Level 3 CBT for Aircraft Engineers

Full aircraft systems training built for maintenance teams and technical instructors. The walkaround and exterior aircraft guide is coming soon.

Email us to get access View systems index

What you will learn

  • Architecture and function of A330 systems at Level 3 depth.
  • Controls, indications, protections, and computer logic.
  • Maintenance interfaces and test features.

How it is used

  • Self-study with progress tracking for each ATA.
  • Classroom facilitation for Part-147 or in-house training.
  • Refresher or cross-type differences support.

Delivery

  • Windows and macOS installers. Internet connection required.
  • Tablet/iPad build available on request.
  • Organization rollout and license options on demand.

Applicability / Engine families

  • A330-200 and A330-300 variants.
  • Engines: Rolls-Royce Trent 700, Pratt & Whitney PW4000, General Electric CF6.
  • A330neo with Rolls-Royce Trent 7000: module planned (coming soon).

Coverage follows the applicable aircraft and engine manufacturer data for these variants.

A330 Level 3 CBT – Systems index

1 - System Overview
1.1 Purpose of the Air Conditioning System
1.2 Pressurized Areas Supplied
1.3 System Functions
1.4 Airflow Sources
1.5 Pack Structure and Function
1.6 Emergency Operation
2 - Pack Air Flow Regulation
2.1 Primary Functions
2.2 Key Component: Flow Control Valve (FCV)
2.3 Sensors Used for Airflow Monitoring
2.4 Ozone Converter
2.5 Regulation Modes
2.6 FCV Shut-Off Conditions
2.7 Indications and Fault Handling
3 - Pack Temperature Control
3.1 Key Components
3.2 Temperature Sensors and Monitoring
3.3 Temperature Regulation Logic
3.4 Redundancy and Fail-Safe Design
3.5 Degraded & Abnormal Operation
3.6 Pneumatic Backup Mode
3.7 ACM Seizure (Bypass Mode)
3.8 Heat Exchanger Contamination Detection
4 - Emergency Ram Air Inlet
4.1 Location and Architecture
4.2 Operation Overview
4.3 Activation Conditions
4.4 Closing the Inlet
4.5 Use Case
5 - Cockpit & Cabin Temperature Control
5.1 System Control Overview
5.2 Inputs Used to Compute Temperature Demand
5.3 Air Distribution Zones
5.4 Regulation Logic
5.5 Trim Air System
5.6 Zone Controller (ZC) Redundancy and Monitoring
5.7 Abnormal Operation and Protection
6 - Air Recirculation System
6.1 Main Purposes
6.2 Components and Flow Path
6.3 System Control
6.4 Avionics Ventilation Integration
6.5 Ground and Abnormal Operation
6.6 System Protection and Monitoring
7 - Air Distribution & Ventilation
7.1 Cockpit Air Distribution
7.2 Cabin Air Distribution
7.3 Lavatory and Galley Ventilation
7.4 Aft Galley Heating (if installed)
7.5 General Ventilation Considerations
8 - Cargo Compartment Ventilation
8.1 System Overview
8.2 Forward Cargo Compartment
8.3 Aft Cargo Compartment
8.4 Bulk Cargo Compartment
8.5 System Control
8.6 Fault Monitoring
9 - Avionics & Equipment Ventilation
9.1 Airflow Sources and Components
9.2 Air Path and Exhaust Control
9.3 System Control and Monitoring
9.4 Ground and In-Flight Operation
9.5 Air Conditioning Bay Ventilation
10 - Pressurization System
10.1 General Operation
10.2 Automatic Control
10.3 Manual Control
10.4 Ground Safety Function - RPCU
10.5 Safety Valves and Pressure Protection
11 - Maintenance Tips & Procedures
11.1 Air Conditioning System Maintenance (General)
11.2 Pressurization System - Maintenance Note
11.3 Deactivation - Turbofan Supply Line
11.4 Deactivation - Avionics Ventilation Overboard Extract Valve
11.5 Deactivation - Pack Flow Control Valve
1 - System Overview
1.1 Purpose and Scope
1.2 Control Law Types
1.3 Major Components
2 - Autopilot Functions
2.1 Modes of Operation
2.2 Engagement/Disengagement Logic
2.3 Flight Director Integration
3 - Flight Control Computers
3.1 FCC Architecture
3.2 Data Inputs and Outputs
3.3 Redundancy and Failover
4 - Autothrust
4.1 Autothrust Modes
4.2 Engagement Criteria
4.3 Fault Handling
5 - Navigation Integration
5.1 Flight Management System Interface
5.2 LNAV/VNAV Logic
5.3 Approach and Landing Modes
6 - Abnormal & Degraded Modes
6.1 Failures and Protections
6.2 Reversion Modes
6.3 Crew Actions
7 - Maintenance & Fault Monitoring
7.1 Built-in Tests
7.2 Fault Codes and Interpretation
7.3 Maintenance Access and Data
1 - Communication System - Overview and Line Maintenance Briefing
1.1 System Overview
1.2 RMP Frequency Selection
1.3 ACP Transmission Mode Selection
1.4 ACP Reception Mode Selection
1.5 ACP Operation
1.6 Flight Interphone System Operation
1.7 Service Interphone System Operation
1.8 Service and Flight Interphone Operation
1.9 Maintenance Tips
1.10 Cabin & Service Interphone Operation
1.11 VHF Communication on Batteries Only
2 - Radio Management
2.1 Communication Architecture
2.2 System Description
2.3 Normal Operation
2.4 Reconfiguration Logic
3 - HF - High Frequency Communications
3.1 General
3.2 Main System Components
3.3 System Architecture
3.4 Interface of the HFDR Transceivers
3.5 HFDR Operating Characteristics
4 - VHF - Very High Frequency Communications
4.1 General
4.2 Main Components
4.3 System Architecture
4.4 SELCAL System
4.5 Interface of the VDR Transceivers
4.6 Data Transmission
4.7 Characteristics
5 - Audio Management - AMU Architecture and Emergency Switching
5.1 Audio Management Unit (AMU) Architecture
5.2 Audio Card Functions
5.3 Cockpit Amplifier Cards
5.4 SELCAL/BITE Card
5.5 Flight Interphone Card
5.6 Emergency Switching
5.7 Emergency Modes
6 - SELCAL / CALL - Selective Calling & Call Systems
6.1 General
6.2 SELCAL Operation
6.3 Ground Call
6.4 Attendant Call
7 - SATCOM - Satellite Communication System
7.1 System Overview
7.2 Avionics Subsystem
7.3 Antenna Subsystem
7.4 Interfaces
8 - Passenger Address System (PA)
8.1 System Overview
8.2 Announcement Sources
8.3 PA Call Types and Zones
8.4 Feedback and Indications
8.5 PA Priority Logic
9 - Cabin and Flight Crew Interphone System
9.1 System Purpose
9.2 Cockpit Operation
9.3 Cabin Operation
9.4 Call Priorities
9.5 Visual and Aural Indications
9.6 Conference and Reset Functions
9.7 Service Interphone System
10 - Passenger Call System
10.1 Overview
10.2 Call Activation Logic
10.3 Visual and Aural Indications
11 - Cabin Ready Signaling
11.1 System Purpose and Function
11.2 Control Interface (FAP)
11.3 Signal Flow and Indications
11.4 Activation Logic
12 - Maintenance
12.1 System Monitoring and Fault Storage
12.2 Ground Maintenance Access
12.3 Maintenance Bus (MPB)
13 - CIDS Programming
13.1 Overview of CIDS Programming
13.2 Director Memory Synchronization
13.3 CIDS Programming via FAP
13.4 Layout Change
14 - Emergency Locator Transmitter (ELT)
14.1 General Description
14.2 System Components
14.3 Operating Modes
14.4 Remote Control Panel
14.5 ELT Programming
15 - In-Flight Entertainment System
15.1 Overview
15.2 Main Components
15.3 Network Structure
15.4 Passenger Interface
15.5 Audio & Video Services
15.6 Power Supply & Safety
15.7 CIDS Integration
15.8 PATS (Passenger Air-to-ground Telephone System)
15.9 Panasonic IFE - System
15.10 Thales IFE - System
16 - Cockpit Voice Recorder (CVR) System
16.1 System Overview
16.2 Recording Principle
16.3 Main Components
16.4 Recording Channels
16.5 Time Synchronization
16.6 Certification Options
16.7 Power Supply Modes
16.8 Test and Monitoring
16.9 Erase Function
17 - Cockpit Door Surveillance System (CDSS)
17.1 General Description
17.2 System Configuration Options
17.3 Cameras
17.4 Display & Control
17.5 Built-in Test Equipment (BITE)
1 - Line Maintenance Briefing
1.1 System Overview
1.2 Environmental Precautions
1.3 A/C Electrostatic Balancing for Maintenance
1.4 Grounding
1.5 Grounding - A330-200F
1.6 Bonding
1.7 IDG Oil Servicing - General Warnings and Cautions
1.8 Visual Inspection of the Oil Level
1.9 Check of IDG Oil-Filter Differential Pressure Indicator (DPI)
1.10 IDG Servicing - Filling / Oil Addition after Level Check
1.11 Depressurize the IDG Case
1.12 Filling of the IDG with Oil
1.13 Removal of the Hoses
1.14 IDG Oil Level Inspection
1.15 Operational Test - IDG Disconnect and Reconnect
1.16 Cold Weather Maintenance - General
1.17 Cold Weather Maintenance - Battery Practices
2 - Electrical System - General Description
2.1 Electrical Generation Overview
2.2 AC Main Generation
2.3 AC Transfer
2.4 Emergency AC Generation
2.5 AC Essential Supply
2.6 AC Generation Properties (Voltage, Frequency, Phase)
2.7 DC Main Generation Architecture
2.8 DC Essential Supply Logic
2.9 Battery Description: BAT 1, BAT 2, APU BAT
2.10 Service Buses and MAINT BUS
2.11 Normal Configuration
2.12 NBPT (No Break Power Transfer)
2.13 Power Supply Priority Logic
2.14 Emergency Electrical Configuration
2.15 Battery-Only Supply (In-Flight and On-Ground Scenarios)
2.16 Summary Overview / Diagrams
2.17 Overview of Control & Management Architecture
2.18 Generator Control Unit (GCU)
2.19 Ground & Auxiliary Power Control Unit (GAPCU)
2.20 Electrical Contactor Management Unit (ECMU)
2.21 CSM/G Generator Control Unit
2.22 Battery Charge Limiters (BCLs)
2.23 Circuit Breaker Monitoring Unit (CBMU)
3 - Main AC Generation
3.1 Electrical Panel and AC ECAM Page
3.2 Integrated Drive Generator (IDG) Construction
3.3 Generator Control Unit (GCU) Functions
3.4 Generator Line Contactor (GLC) Operation
3.5 Feeder Lines and Current Transformers (CT)
3.6 ECMU Contactors & NBPT Logic
3.7 IDG Control P/B
3.8 GEN Control P/B
3.9 Generator Speed Regulation (CSD Function - 4900 to 9120 RPM input -> 24000 RPM output)
3.10 IDG Oil System
3.11 IDG Oil Temperature Sensors
3.12 IDG Low Oil Pressure Switch
3.13 IDG Differential Pressure Indicator (DPI)
3.14 IDG Remote Oil Level Sensor (ROLS)
4 - Auxiliary AC Generation
4.1 APU Generator Architecture and Regulation
4.2 GAPCU Interface
4.3 APU GEN Contactors and NBPT Priority
4.4 APU GEN Fault Monitoring and ECAM Logic
5 - Emergency AC Generation
5.1 CSM/G Hydraulic Drive Overview
5.2 EMER GEN Startup Logic and Timing
5.3 Electrical Contactor Management During Emergency
5.4 Static Inverter Supply Path
5.5 Transfer to AC ESS BUS and DC ESS BUS
5.6 ECAM and BITE Messages for EMER GEN
6 - Contactor Management
6.1 Overview of GLC, APU GLC, EPC, SIC, BTC
6.2 ECMU Switching Logic
6.3 Galley Shedding Control
6.4 NBPT Sequence and Protection Logic
7 - Main DC Generation
7.1 Transformer Rectifiers - TR1 and TR2
7.2 DC Busbar Architecture
7.3 DC BAT BUS Logic and Failover
7.4 ESS TR -> DC ESS BUS
7.5 Emergency DC Generation and Battery-only Supply
7.6 BCL Logic and Protection
7.7 General Monitoring Interfaces Overview
7.8 IDG - Oil Temperature Sensors
7.9 IDG - Low Oil Pressure Switch (LOP < 140 psi / 9.65 bar)
7.10 IDG - Differential Pressure Indicator (DPI)
7.11 IDG - Remote Oil Level Sensor (ROLS)
7.12 GCU to ECAM Interface (Advisories, Failures)
7.13 GCU to CMC and GAPCU (Maintenance Messaging)
7.14 ECMU Data Link (Contactor Commands, Fault Logic)
8 - Emergency DC Generation
8.1 ESS TR Backup Logic
8.2 DC ESS BUS Supply via Batteries
8.3 Failure Cascade Path and ECAM Alerts
9 - Load Distribution
9.1 Load Management Principles
9.2 Galley Load Shedding Logic
9.3 Normal vs Emergency Load Shedding
9.4 Service Bus Load and Activation
9.5 Refuel on Battery D/O
9.6 Refueling Electrical Configuration
9.7 Battery Power Supply Role
9.8 Available Loads During Refueling
9.9 APU/EXT Power Override Logic
9.10 Ground Safety Considerations
1 - Equipment/Furnishings Line MAINT Briefing
1.1 System Overview
1.2 Cabin Panel Layout
1.3 Cabin Escape Facilities
1.4 Lower Deck Cargo Compartments
1.5 Cargo Loading System (CLS)
1.6 MEL/Deactivation
1.7 Maintenance Tips
1.8 'A' Check Items
2 - Cockpit
2.1 Pilot Seats
2.2 Third Occupant Seat
2.3 Fourth Occupant Seat
3 - Passenger Compartment
3.1 General
3.2 Lining and Furnishing Panels
3.3 Lining and Furnishing Layout
3.4 Passenger Service Channel
3.5 Passenger Seats
3.6 Cabin Attendant Seats
3.7 Galley
3.8 Lavatories
3.9 Electrical Plug Supply
4 - Crew Rest Compartment
4.1 Description and Equipment
4.2 Interfaces
4.3 Safety Equipment
5 - Galley Cooling
5.1 Galley Trolley Compartment Cooling System
6 - Emergency Equipment
6.1 Cockpit Emergency Equipment
6.2 Cabin Emergency Equipment
7 - Lower Deck Area
7.1 Decompression Safety System
8 - Cargo Loading
8.1 Lower Deck Cargo Loading System
9 - Maintenance Practice
9.1 Equipment/Furnishings System Base Maintenance
9.2 Linings & Furnishings Removal/Installation
1 - System Overview
1.1 Fire Protection - General Overview
1.2 Components Location - Summary Overview
1.3 System Description - Global Architecture
1.4 Daily Checks
1.5 MEL / Deactivation
1.6 Maintenance Tips
2 - Avionics Smoke Detection
2.1 Avionics Smoke Detection
3 - Lavatory Smoke Detection
3.1 Description
3.2 System Architecture
3.3 Components Location
3.4 Detection Principle
3.5 Detection and Warning
3.6 Fire Test
3.7 System Interfaces
3.8 Maintenance
4 - Cargo Compartment Fire Protection
4.1 Description
4.2 System Architecture
4.3 Components Location
4.4 Detection Principle
4.5 Detection and Warning
4.6 Extinguishing
4.7 Maintenance Interface
4.8 Control and Monitoring
4.9 Fire Test
4.10 System Interfaces
4.11 Maintenance
5 - Engine Fire Protection
5.1 Description
5.2 Components Location
5.3 Detection Principle
5.4 Detection and Warning
5.5 Fire Test
5.6 Extinguishing
5.7 Test
5.8 System Interfaces
5.9 Maintenance
6 - APU Fire Protection
6.1 Description
6.2 Components Location
6.3 Detection Principle
6.4 Detection and Warning
6.5 Fire Test
6.6 Extinguishing
6.7 Test
6.8 System Interfaces
6.9 Maintenance
1 - System Overview
1.1 General Description
1.2 Control Surfaces and Functions
1.3 Control Laws
1.4 System Architecture
2 - Primary Flight Controls
2.1 Elevator - Description & Operation
2.2 Aileron - Description & Operation
2.3 Rudder - Description & Operation
2.4 Spoilers - Functions & Modes
3 - Secondary Flight Controls
3.1 THS (Trimmable Horizontal Stabilizer) - Architecture & Control
3.2 Rudder Trim - Manual and Automatic Inputs
3.3 Slats and Flaps - Normal Operation
3.4 Slats and Flaps - Alternate Operation
3.5 Flap & Slat Fault Modes
4 - Control Devices & Input Channels
4.1 Side Stick - Mechanical Interface & Signal Flow
4.2 Pedals - Rudder Trim Coupling
4.3 THS Trim Wheel - Manual Override
4.4 Flap/Slat Lever - Gate Logic and Step Zones
4.5 Auto-Trim and Autopilot Interaction
5 - Computers & Logic
5.1 FCPC - Flight Control Primary Computers
5.2 FCSC - Flight Control Secondary Computers
5.3 Control Surface Command Distribution & Redundancy
5.4 Monitoring & System Logic Overview
5.5 Signal Distribution, Voting Logic, & Redundancy
6 - Control Laws & System Modes
6.1 Control Laws - Overview
6.2 Normal Law
6.3 Alternate Law
6.4 Direct Law
6.5 Manual Control (Following Electrical Failure)
7 - System Integration & Behavior Summary
7.1 Flight Control Computer Roles
7.2 Speed-Based Control Surface Behavior
7.3 Actuator Feedback & Fault Handling
7.4 Control Law Reconfiguration Triggers
7.5 Fault Monitoring & Built-In Tests
8 - Tests & Maintenance
8.1 Flight Control BITE Tests
8.2 Ground Test Functions (Flight Control Test - FCT)
8.3 THS Mechanical Backup Operation & Inspection
1 - Fuel System Overview
1.1 General Architecture and Main Functions
1.2 Fuel Capacity Summary (with metric + imperial units)
1.3 Fuel Transfer & CG Management Logic
1.4 Automation and FCMC Roles
1.5 Temperature Monitoring and Protections
2 - Fuel Line Maintenance Briefing
2.1 System Overview and General Considerations
2.2 Safety Notes and Precautions
3 - Tank, Venting, Scavenge and Indicating
3.1 Tank Structure and Layout
3.2 Venting System and Surge Tanks
3.3 Scavenge and Trim Transfer Logic
3.4 Quantity and Indication Probes
4 - Fuel Feed
4.1 Engine Feed (A330-200)
4.2 Engine Feed (A330-300)
4.3 APU Feed (A330-200)
4.4 APU Feed (A330-300)
5 - Fuel Transfers
5.1 Main Transfer (A330-200)
5.2 Main Transfer (A330-300)
5.3 Trim Transfer (A330-200)
5.4 Trim Transfer (A330-300)
6 - Refuel / Defuel
6.1 Automatic Refuel Sequence
6.2 Refuel/Defuel (A330-200)
6.3 Refuel/Defuel (A330-300)
7 - Jettison
7.1 Jettison (A330-200)
7.2 Jettison (A330-300)
8 - Maintenance Practice
8.1 Ground Test Interfaces
8.2 BITE Test Access
8.3 MEL and Dispatch Considerations
9 - System Differences - A330-200 vs A330-300
9.1 Fuel Tank Capacities & Layout
9.2 Transfer Logic Variants
9.3 Refuel/Defuel Differences
9.4 Trim Tank Role and CG Strategies
1 - Hydraulic System Line Maintenance Briefing
1.1 System Overview
1.2 Users
1.3 Reservoirs
1.4 Engine Pumps
1.5 Electrical Pumps
1.6 Ram Air Turbine
1.7 Servicing Panels
1.8 Hydraulic System Monitoring Unit (HSMU)
1.9 Maintenance/Test Facilities
1.10 Safety Precautions
2 - Servicing
2.1 Check of Reservoir Fluid Level
2.2 Bleeding Upstream of the ENG Pump
2.3 Bleeding Upstream of the Electric Pump
2.4 Bleeding Downstream of the Engine Pump
2.5 Air System Check
3 - Maintenance Tips
3.1 Tightening Torques
3.2 External Leak Test of Components
4 - Circuit Identification and Routing
4.1 Pipe Routing
4.2 Pipe Identification
4.3 Component Identification
4.4 Connections
5 - Filling Presentation
5.1 General
5.2 System Presentation
5.3 Indicating
5.4 Reservoir Filling Procedure Summary
5.5 Environmental Precautions
6 - Pressurization Presentation
6.1 General
6.2 Sources
6.3 Manual Depressurization Valve
6.4 Depressurization and Pressurization Procedure Summary
7 - Green Hydraulic System
7.1 System Description
7.2 Accumulator
7.3 HP Filter Manifold
7.4 Brake Manifold
7.5 HP Manifold
7.6 FSOV Logic Operation
7.7 EDP Logic Operation
7.8 Electric Pump Logic
7.9 RAT Logic Operation
7.10 Current Unbalance Detector Units
7.11 Distribution Indications
8 - Blue Hydraulic System
8.1 System Description
8.2 Accumulator
8.3 HP Manifold
8.4 FSOV & EDP Logic
8.5 Electric Pump Logic
8.6 Current Unbalance Detector Units
8.7 Distribution Indications
9 - Yellow Hydraulic System
9.1 System Description
9.2 Accumulator
9.3 HP Manifold
9.4 Cargo Door Electro Selector Valve & Hand Pump
9.5 FSOV & EDP Logic
9.6 Electric Pump Auto Start
9.7 Current Unbalance Detector Units
9.8 Distribution Indications
10 - Seal Drain
10.1 General
10.2 Recovery Tanks
11 - Leak Test
11.1 General
11.2 Measurement Method
11.3 Predefined Measurement Points
11.4 Operational Modes
11.5 Full System Check
11.6 Full System without Primary Flight Controls
11.7 Component Checks
12 - RAM Air Turbine Manual Deployment System Line Maintenance
12.1 Introduction
12.2 Operational Test - Extension/Retraction
12.3 Inspection and ACMS Test
12.4 Spin-Up and Pump Test
1 - Ice & Rain Protection Line Maintenance Briefing
1.1 System Overview
1.2 Wing Ice Protection
1.3 Engine Air Intake Ice Protection
1.4 Probe Ice Detection
1.5 Windshield Anti-Icing
1.6 Rain Protection
1.7 Potable and Waste Water Ice Protection
1.8 Escape Slide Locking Mechanism Ice Protection
1.9 Ice Detection
2 - Servicing
2.1 Check of Rain-Repellent Fluid Can Assembly
2.2 Fluid Can Replacement Procedure
3 - MEL / Deactivation
3.1 Deactivation of Wing Anti-Ice Control Valve
3.2 Deactivation of Engine Air-Intake A-Ice Control Valve
4 - Maintenance Tips
4.1 Probe Heat System
5 - Wing Ice Protection
5.1 General
5.2 Wing Anti-Ice Air Ducting
5.3 Wing Anti-Ice Valve
5.4 Pressure Regulating Valve Internal Operation
5.5 Operation
- Normal Operation
- Abnormal Operation
- Monitoring
6 - Engine Air Intake Ice Protection
6.1 General
6.2 Engine Anti-Ice Air Ducting
6.3 Engine Anti-Ice Valve
6.4 Engine Anti-Ice Internal Operation
6.5 Engine Anti-Ice Valve Operation
- Normal Operation
- Abnormal Operation
- Monitoring
7 - Probe Ice Protection
7.1 General
7.2 Control and Operation
- EIVMU 1 Failure
- LGCIU 1 and 2 Failure
8 - Windshield Anti-Ice / Defogging & Rain Protection
8.1 General
8.2 Anti-Ice and Defogging Control and Monitoring
8.3 Windshield Spare Temperature Sensor Connection
8.4 Wiper System
8.5 Rain Repellent System
9 - Potable & Waste Water Ice Protection
9.1 General
9.2 Electrical Heating Elements
9.3 Control
10 - Escape Slide Locking Mechanism Ice Protection
10.1 General
10.2 Description
- Slide Attachment Fittings
- IPCU Location
- IPCU Functions
10.3 Normal Operation
10.4 Monitoring
11 - Ice Detection
11.1 General
11.2 Operation
11.3 Indication and Monitoring
11.4 Visual Light Indicator
12 - Maintenance Practice
12.1 Ice and Rain Protection System Base Maintenance
12.2 Adjustment of WIPDU Coding Switches and Enable Micro Switches
1 - Recording System Line Maintenance Briefing
1.1 Recording System Overview
1.2 ACMS Parameter Label Call-Up via MCDU
1.3 ACMS Parameter Alpha Call-Up via MCDU
1.4 ACMS Maintenance Tips
2 - DFDRS - Digital Flight Data Recording System
2.1 DFDRS General Description
2.2 DFDRS
2.3 DFDRS Sources
3 - ACMS - Aircraft Condition Monitoring System
3.1 ACMS General Description
3.2 ACMS
3.3 ACMS Reports
3.4 ACMS Sources
4 - Maintenance Practice
4.1 Recording Systems Base Maintenance
4.2 Auto/Manual Dump Procedure to Download ACMS Data
4.3 Operational Test of DFDR Playback via MCDU
1 - Landing Gear System Line Maintenance Briefing
1.1 System Overview
1.2 Main Landing Gear (MLG)
1.3 MLG Side Stay Assembly
1.4 MLG Bogie Alignment Pitch Trimmer
1.5 MLG Shortening Mechanism
1.6 MLG Doors
1.7 Nose Landing Gear (NLG)
1.8 NLG Lock Stay Assembly
1.9 NLG Doors
1.10 Normal Braking Manual Mode
1.11 Alternate Braking
1.12 Parking / Ultimate Emergency Braking
1.13 Safety Precautions
2 - Maintenance
2.1 Installation of Safety Devices on the L/G
2.2 Installation of Safety Devices on the L/G Doors
2.3 L/G Doors Ground Opening
2.4 L/G Doors Ground Closing
2.5 Tyre Pressure Check
2.6 Check Brake Pack Wear Indicators
2.7 MLG Wheel Brake Deactivation Procedure
2.8 Activating the MLG Seal Changeover Valve
2.9 Activating the NLG Seal Changeover Valve
3 - Landing Gear and Doors
3.1 Landing Gear Special Features
3.2 Normal Extension and Retraction
3.3 Free Fall Extension
3.4 Door Ground Opening
4 - Wheels and Brakes
4.1 Normal Braking
4.2 Alternate Braking
4.3 Park / Ultimate Braking
4.4 Brake Temperature and Cooling System
5 - Tire Pressure
5.1 TPIC
6 - Nose Wheel Steering
6.1 Nose Wheel Steering
7 - Maintenance Practice
7.1 Landing Gear MCDU Pages
7.2 Push Back and Towing
7.3 Landing Gear System Base Maintenance
1 - Landing Gear System Line Maintenance Briefing
1.1 System Overview
1.2 Main Landing Gear (MLG)
1.3 MLG Side Stay Assembly
1.4 MLG Bogie Alignment Pitch Trimmer
1.5 MLG Shortening Mechanism
1.6 MLG Doors
1.7 Nose Landing Gear (NLG)
1.8 NLG Lock Stay Assembly
1.9 NLG Doors
1.10 Normal Braking Manual Mode
1.11 Alternate Braking
1.12 Parking / Ultimate Emergency Braking
1.13 Safety Precautions
2 - Maintenance
2.1 Installation of Safety Devices on the L/G
2.2 Installation of Safety Devices on the L/G Doors
2.3 L/G Doors Ground Opening
2.4 L/G Doors Ground Closing
2.5 Tyre Pressure Check
2.6 Check Brake Pack Wear Indicators
2.7 MLG Wheel Brake Deactivation Procedure
2.8 Activating the MLG Seal Changeover Valve
2.9 Activating the NLG Seal Changeover Valve
3 - Landing Gear and Doors
3.1 Landing Gear Special Features
3.2 Normal Extension and Retraction
3.3 Free Fall Extension
3.4 Door Ground Opening
4 - Wheels and Brakes
4.1 Normal Braking
4.2 Alternate Braking
4.3 Park / Ultimate Braking
4.4 Brake Temperature and Cooling System
5 - Tire Pressure
5.1 TPIC
6 - Nose Wheel Steering
6.1 Nose Wheel Steering
7 - Maintenance Practice
7.1 Landing Gear MCDU Pages
7.2 Push Back and Towing
7.3 Landing Gear System Base Maintenance
1 - Navigation Line Maintenance Briefing
1.1 ADIRS Alignment
1.2 Battery Test
1.3 Alignment of the IRS
1.4 Automatic Alignment by GPS (Option)
1.5 Fast Realignment
1.6 Interruption During Alignment
1.7 Maintenance Tips
1.8 ADM Pneumatic Connection
2 - General
2.1 ADIRS & Standby Instruments General Description
3 - Radio Navigation Tuning
3.1 General
3.2 Automatic Tuning
3.3 Manual Tuning
3.4 MCDU Switching
3.5 FM Switching
3.6 Backup Tuning
4 - ADIRS
4.1 ADIRS Description/Operation
4.2 Air Data Module
4.3 ADR Computation
4.4 IR Computation
5 - ADIRS Switching
5.1 Principle
5.2 Switching
6 - Standby Instruments
6.1 Standby Compass
6.2 ISIS Description
6.3 ISIS Power Supply
6.4 ISIS Operation
6.5 ISIS Optional Displays
6.6 ISIS Abnormal Operation
6.7 ISIS Maintenance Operation
7 - Satellite Navigation
7.1 GPS Function
7.2 GPS Sensor and ADIRU Interface
7.3 FMGEC Integration
7.4 ATT/HDG Switching
7.5 Monitoring and Indicating
7.6 CMC Interface
8 - Multi Mode Receiver (MMR)
8.1 General Description
8.2 ILS Function
8.3 GPS Function
8.4 Maintenance Operation
9 - VOR / MKR / DME / ADF / DDRMI
9.1 General
9.2 ADF Principle
9.3 DME Principle
9.4 VOR Principle
9.5 MKR Principle
9.6 DDRMI
9.7 System Operation and Tuning
9.8 Antennas and Indicators
9.9 LGCIU / FMGEC / CMC Interfaces
10 - TAWS / EGPWS / T2CAS
10.1 General
10.2 Data Inputs (Digital / Discrete)
10.3 Visual and Aural Warnings
10.4 Control Interface
10.5 Runway Awareness & Advisory System (RAAS)
10.6 Warning Modes (1-5, Terrain Awareness, TCF)
10.7 T2CAS Overview and Logic
10.8 Differences between EGPWS and T2CAS
11 - Radio Altimeter
11.1 Antennae
11.2 Indication
11.3 Users and Interfaces
11.4 Cooling
11.5 CMC
12 - Weather Radar
13 - ATC / TCAS
1 - Oxygen System Line Maintenance Briefing
1.1 System Overview
1.2 Servicing
1.3 Daily Check
1.4 Weekly Check
1.5 MEL / Deactivation
1.6 Maintenance Tips
2 - Oxygen Safety in Aircraft Maintenance Environment
2.1 Oxygen Properties
2.2 Aircraft Oxygen Systems
2.3 The Fire Triangle
2.4 Leak in Confined Area
2.5 Safety Precautions
3 - Crew Oxygen Systems (Flight Deck Gaseous Supply)
3.1 Flight Crew Gaseous Oxygen Supply
3.2 Regulation and Distribution Architecture
3.3 Crew Oxygen Masks and Deployment
3.4 Indication and Control (ECAM / MCDU / Mechanical Gauge)
3.5 Cylinder Servicing and Safety Features
4 - Cabin and Passenger Oxygen Systems
4.1 Passenger Chemical Oxygen System
4.2 Cabin Crew Portable Gaseous Oxygen System
4.3 Passenger Portable Oxygen System (First Aid Bottles - Gaseous)
4.4 Optional Passenger Gaseous Backup System
1 - Pneumatic System Line Maintenance Briefing
1.1 System Overview
1.2 Sources and Users
1.3 Engine Bleed
1.4 APU Bleed and External Supply
1.5 Leak Detection
1.6 MEL / Deactivation
1.7 Maintenance Tips
2 - Bleed Air Distribution and Supply
2.1 General
2.2 HP Air Ground Supply
2.3 APU Bleed Air Supply
2.4 APU Bleed and Check Valves
2.5 APU Bleed Valve Control
2.6 Crossbleed System
2.7 Automatic Control
2.8 Manual Control
2.9 Incorrect Operation
3 - Engine Bleed Air Management
3.1 General
3.2 Bleed Air Transfer
3.3 Pressure Limitation
3.4 Temperature Limitation
3.5 Monitoring
4 - Engine Bleed Air Transfer System
4.1 Description
4.2 High Pressure Bleed Valve
4.3 Intermediate Pressure (IP) Check Valve
4.4 Bleed Transferred Pressure Transducer
4.5 Pressure Transfer System
4.6 Normal Operation
4.7 Abnormal HPV Closure
4.8 Valve Position Disagreement
4.9 Monitoring
5 - Engine Bleed Pressure Regulation System
5.1 System Description
5.2 Pressure Regulating Valve
5.3 Overpressure Valve
5.4 Bleed Regulated Pressure Transducer
5.5 Pressure Regulation
5.6 Isolation Functions
5.7 Manual Isolation
5.8 Fire Isolation
5.9 Automatic Isolation
5.10 Overpressure Protection
5.11 Monitoring
6 - Engine Bleed Temperature Regulation System
6.1 General
6.2 Description
6.3 Fan Air Valve (FAV)
6.4 Precooler
6.5 Outlet Bleed Temperature Sensor
6.6 Temperature Regulation
6.7 Overheat Detection
6.8 Low Temperature Detection
6.9 Monitoring
7 - Leak Detection System
7.1 General
7.2 Sensing Elements
7.3 BMC Loop Monitoring
7.4 Leak Detection Operation
8 - Maintenance Practice
8.1 Introduction
8.2 Functional Test - Bleed Transferred Pressure Transducer
8.3 Job Setup
8.4 Test Procedure
8.5 Close-Up
1 - Water and Waste Line Maintenance Briefing
1.1 System Overview
1.2 Potable and Waste Servicing Principles
1.3 Cold Weather Operations and Precautions
1.4 Maintenance Tips
2 - Potable Water System
2.1 System Description and Functional Logic
2.2 Tanks, Filling, and Overflow Control
2.3 Distribution Lines and Water Valves
2.4 Pressurization via Pneumatics, Compressor, or Ground Source
2.5 Indication System and FAP/Service Panel Interfaces
2.6 Optional Configuration: 3-Tank Potable Water Setup
3 - Air Supply System (Potable Water Pressurization)
3.1 Dedicated Compressor Description
3.2 Pressurization Control Logic
3.3 Ground Supply Interface and Regulation
4 - Toilet System
4.1 System Description and Flush Logic
4.2 Toilet Bowl Components and Solenoid Valve Function
4.3 Electrical Supply and Flush Interlocks
5 - Waste Water System
5.1 Waste Tank Layout and Optional Configurations
5.2 Vacuum Generation System
5.3 Line Heating, Drain Masts, and Overboard Discharge
5.4 Ventilation, Anti-Backflow, and Safety Features
6 - Maintenance Practice
6.1 Water and Waste MCDU Interface Pages
6.2 Potable Water Servicing with and without Electrical Power
6.3 Waste Tank Drain and Flush Procedures
6.4 Disinfection Quantities and Procedures
6.5 Cold Weather Draining and Pre-Charge Handling
6.6 Component Reset and In-Service Fault Isolation
1 - Onboard Maintenance System Line Maintenance Briefing
1.1 System Overview
1.2 OMS Architecture and Centralized Maintenance System (CMS)
1.3 Interfaces: MCDU, ECAM, CMC
1.4 Data Acquisition and Storage
1.5 OMS Configuration and Customization
1.6 Fault Reporting and ECAM/CMC Integration
1.7 Maintenance Messages and Post-Flight Reports
1.8 CMS Function Decentralization and Reconfiguration
1.9 Troubleshooting Support
1.10 OMS Memory Structure
2 - CMC Operation
2.1 Accessing the CMC
2.2 Menu Navigation
2.3 System Report and Flight Leg Selection
2.4 Status Report and Fault History
2.5 Post-Flight Report (PFR)
2.6 Maintenance Report (MCDU Format)
2.7 Class 3 Faults and ATA Correlation
2.8 Printer, Display, and Save Options
2.9 Maintenance Status Reset
3 - OMS Interfaces and Reporting Functions
3.1 CMC Functional Interfaces
3.2 System Report and Fault History Management
3.3 Report Menu Structure and Output Options
3.4 System Servicing Report and Ground Operations
3.5 BITE Test Access via CMC
3.6 Post-Flight Report Contents and Format
3.7 CMS Reconfiguration via Software Download
4 - OMS Maintenance Practice
4.1 CMS Fault Reset Function
4.2 Software Part Number and Standard Identification
4.3 System Configuration and Pin Programming
4.4 Maintenance Data Review and Report Printing
4.5 Data Download via Printer or Recorder
4.6 OMS Power Supply and CB Reset Conditions
4.7 CMC Limitations and Reset Logic
1 - Information Systems Line Maintenance Briefing
1.1 System Overview
1.2 Information System Functions
1.3 Information System Architecture
1.4 Overview of Server Client Relationship
1.5 Maintenance Support Functions
1.6 Line Replaceable Units (LRUs) and Interfaces
1.7 Maintenance Recommendations
2 - ATIMS
2.1 ATSU Interfaces
2.2 ATSU Description
2.3 ATSU Operation
3 - ATIMS Menu
3.1 ATSU Main Tree
3.2 COMM Menu
3.3 ATC Menu
3.4 AOC Menu
3.5 Step-by-Step Procedures
4 - Information Systems AINS
4.1 System Architecture
4.2 The ANSU
4.3 The SIU
4.4 The TWLU
4.5 Power Supply
4.6 Interfaces
5 - Information Systems CINS
5.1 System Architecture
5.2 The CNSU
5.3 The ESU
5.4 The CWLU
5.5 Power Supply
5.6 Interfaces
6 - Maintenance Practice
6.1 Information Systems MCDU Pages
6.2 Information Systems Base Maintenance
1 - Information Systems Line Maintenance Briefing
1.1 System Overview
1.2 Information System Functions
1.3 Information System Architecture
1.4 Overview of Server Client Relationship
1.5 Maintenance Support Functions
1.6 Line Replaceable Units (LRUs) and Interfaces
1.7 Maintenance Recommendations
2 - ATIMS
2.1 ATSU Interfaces
2.2 ATSU Description
2.3 ATSU Operation
3 - ATIMS Menu
3.1 ATSU Main Tree
3.2 COMM Menu
3.3 ATC Menu
3.4 AOC Menu
3.5 Step-by-Step Procedures
4 - Information Systems AINS
4.1 System Architecture
4.2 The ANSU
4.3 The SIU
4.4 The TWLU
4.5 Power Supply
4.6 Interfaces
5 - Information Systems CINS
5.1 System Architecture
5.2 The CNSU
5.3 The ESU
5.4 The CWLU
5.5 Power Supply
5.6 Interfaces
6 - Maintenance Practice
6.1 Information Systems MCDU Pages
6.2 Information Systems Base Maintenance
1 - APU Line Maintenance Briefing
1.1 System Overview
1.2 Servicing
1.3 MEL / Deactivation
1.4 Maintenance Tips
1.5 Environmental Precautions
2 - APU General
2.1 General
2.2 Engine Power Section
2.3 Load Compressor
2.4 Accessory Drive Gearbox
2.5 APU Mounts System
2.6 Air Intake System
2.7 Drain System
2.8 Exhaust
3 - APU Fuel
3.1 General
3.2 Fuel Control Unit
3.3 Flow Divider
3.4 Fuel Distribution
3.5 Control and Monitoring
4 - APU Air
4.1 General
4.2 Bleed and Surge Subsystem Description
4.3 Bleed and Surge Air Operation
4.4 Accessory Cooling
5 - APU Oil
5.1 Lube Module Description
5.2 Gearbox Description
5.3 Oil Cooler and Thermal Bypass Valve
5.4 Normal Operation
5.5 Abnormal Operation
5.6 Monitoring
6 - APU Operation, Ignition and Starting
6.1 Description
6.2 APU Start Operation
6.3 APU Available
6.4 Normal APU Shutdown
6.5 Protective Shutdowns
7 - Maintenance Practice
7.1 APU MCDU Pages
1 - Doors
1.1 General
1.2 Passenger Doors
1.3 Cargo Compartment Doors
1.4 Access & Service Doors
1.5 Landing Gear Doors
2 - Fuselage
2.1 General Description
2.2 Upper and Lower Shell Construction
2.3 Frame and Stringer Integration
2.4 Center Fuselage and Belly Fairing
2.5 Pressure Bulkheads
3 - Pylons and Nacelles
3.1 Pylon General Structure
3.2 Nacelle Structure
3.3 Fire Protection Interfaces
3.4 Materials and Attachment Zones
4 - Stabilizers
4.1 Horizontal Stabilizer
4.2 Vertical Stabilizer
4.3 Leading Edge and Tip Structure
4.4 Attachment and Load Transfer
5 - Windows
5.1 Cockpit Windows
5.2 Cabin Windows
5.3 Window Frames and Seals
5.4 Materials and Lightning Protection
6 - Wings
6.1 General
6.2 Center Wing Box
6.3 Outer Wing Box
6.4 Outer Wing Box
6.5 Slats
6.6 Fixed Trailing Edge
6.7 Trailing Edge Devices
7 - Structure Repair Manual (SRM)
7.1 SRM Organization and Use
7.2 Zoning, Access Panels, and Coordinates
7.3 Damage Limits and Categories
7.4 Temporary vs Permanent Repair Logic
1 - Doors Line Maintenance
1.1 System Overview
1.2 Servicing
1.3 Maintenance Tips
1.4 MEL / Deactivation
2 - Emergency Exits
2.1 Passenger Door Control Mechanism
2.2 Escape Facility Release Mechanism
3 - Cargo Doors
3.1 Forward and AFT Cargo Doors
3.2 Bulk Cargo Door Operation
3.3 Cargo Door Locking Mechanism
3.4 Cargo Doors FWD and AFT Hydraulic System
4 - Cockpit Door
4.1 Cockpit Doors
5 - Door and Slide Control System
5.1 DSCS Passenger/Crew Doors
5.2 DSCS Forward and AFT Cargo Doors
5.3 DSCS Bulk Cargo and Avionics Compartment Doors
6 - Maintenance Practice
6.1 Doors System Base Maintenance
1 - Engine Line Maintenance
1.1 System Overview
1.2 Servicing
1.3 MEL / Deactivation
1.4 Maintenance Tips
1.5 Engine Change Procedure
2 - Engine Description (Expanded with full technical detail)
2.1 General
2.2 Low Pressure Compressor and Turbine
2.3 Intermediate Pressure Compressor and Turbine
2.4 High Pressure Compressor and Turbine
2.5 Combustion Chamber
2.6 Engine Bearings
2.7 Accessory Drive Section
2.8 External Gearbox Module
2.9 Drains System
2.10 Aerodynamic Stations
2.11 Borescope Access Ports
3 - Fuel System
3.1 Fuel Pump Assembly
3.2 Low Pressure Fuel Circuit
3.3 High Pressure Fuel Circuit
3.4 Metered Fuel Flow
3.5 Fuel Control and Monitoring
4 - Full Authority Digital Engine Control (FADEC)
4.1 FADEC Architecture
4.2 EEC Interfaces
4.3 Power Supply and Backup
4.4 Control Logic and Monitoring
5 - Ignition and Starting
5.1 Ignition System Components
5.2 Starter System
5.3 Automatic and Manual Start Logic
5.4 APU Boost and Alternate Start
6 - Air System
6.1 Airflow Control
6.2 IP and HP Bleed Systems
7 - Cooling
7.1 Oil Cooling and Air/Oil Heat Exchanger
7.2 Nacelle Ventilation
8 - Engine Controls
8.1 Thrust Control
8.2 Engine Master Control
8.3 TLA and MRA Logic
10 - Thrust Reverser
10.1 Description and Operation
10.2 Actuation and Locking System
10.3 Control and Indications
11 - Oil System
11.1 Description and Layout
11.2 Pumping and Scavenging
11.3 Oil Indications and Chip Detection
12 - Maintenance Practice
12.1 Power Plant Base Maintenance
12.2 Engine Preservation and Depreservation
1 - 72-00 General
1.1 Abbreviations and Acronyms
1.2 Engine Specifications
1.3 Power Setting Curves (Take Off)
1.4 Engine Station Designations
1.5 Engine Control PB's and Switches
2 - ATA 71 - Power Plant
2.1 Engine Cowlings - Description
2.2 Thrust Reverser Cowl Doors
2.3 T/R Interlock Valve
2.4 Engine Air Intake Cowl
2.5 Engine Fire Barriers
2.6 Engine Mounts (ATA 71-20)
3 - 72-00 Engine Modules
3.1 Module Description
3.2 Fan and LPC Description
3.3 Fan Rotor Blades Removal / Installation
3.4 One Blade Installation
3.5 Borescope Plugs and Access
3.6 N2 Manual Crank (Borescope Rotation Adapter)
3.7 Compressor Rear Frame (CRF) and Combustor
3.8 HPT Nozzle Guide Vanes (NGV) and Rotor Cooling
3.9 Eleventh Stage Cooling (ESC) and CCCV Notes
3.10 LPT Stator Case and Turbine Rear Frame (TRF)
4 - ATA 73 - FADEC System (73-21)
4.1 FADEC Description
4.2 ECU Interfaces
5 - ATA 74 - Ignition System (74-00)
5.1 General
5.2 Ignition Exciters
5.3 Ignition Leads
5.4 Engine Ignitors
6 - ATA 75 - Air System / Cooling & Variable Geometry
6.1 Bore Cooling Valve (BCV)
6.2 Core Compartment Cooling Valve (CCCV)
6.3 HPT Active Clearance Control (HPTACC)
6.4 LPT Active Clearance Control (LPTACC)
6.5 VBV Schedule (Variable Bleed Valves)
7 - ATA 76 - Engine Control (76-10 Power Control)
7.1 Cockpit Engine Controls - General
7.2 Thrust Levers
7.3 Engine Master
7.4 Engine Start
7.5 Engine Manual Start
7.6 FADEC Ground Power
7.7 Engine Fire
7.8 Engine Anti-Ice
8 - ATA 77 - EIVMU (77-00)
8.1 MCDU Pages & Reports
8.2 Specific Data / Fan Unbalance / Max Flight Vibration Display
8.3 Sensors & Conditioning - CRF Accelerometer, Remote Charge Converter (RCC)
9 - ATA 78 - Exhaust / Thrust Reverser (78-30)
9.1 Thrust Reverser Description
9.2 Thrust Reverser Deactivation
9.3 Directional Pilot Valve Deactivation
9.4 Thrust Reverser - Deployed / Stowed
9.5 Thrust Reverser Indication
9.6 Thrust Reverser CMS Test
10 - ATA 79 - Engine Oil
10.1 General - Introduction
10.2 Oil Components - Oil tank, master chip detector, lube supply filter, scavenge filter, fuel-oil heat exchanger
10.3 Oil Indicating - Low oil pressure switch, oil temperature sensor, oil quantity indication, scavenge oil filter bypass warning
11 - ATA 80 - Starting System (80-00)
11.1 Starter Shut Off Valve (SOV)
11.2 Starter
11.3 Starter Duct
12 - ATA 30-21 - Ice & Rain Protection (Interface)
12.1 General
13 - 71-00 Power Plant General (Operational & Procedures)
13.1 Safety Precautions
13.2 Engine Danger Zones
13.3 Speed RPM
13.4 Oil System
13.5 Starting and Ignition Systems
13.6 Ground Operation in Icing Conditions
13.7 Throttle Movement
13.8 Fuel System
13.9 High Nacelle Temperature Indication
13.10 Abnormal Operation and Emergency Procedures
13.11 Procedure in Case of Engine Fire
13.12 Abnormal Operations
13.13 Dry Motoring Check
13.14 Wet Motoring Check
13.15 Engine Automatic Start
13.16 Engine Manual Start
13.17 Engine Tests
1 - 72-00 General
1.1 Abbreviations and Acronyms
1.2 Engine Overview & Specifications
1.3 Power Setting & Flat-Rating Concept
1.4 Engine Station Designations / Access Views
1.5 Engine Control Interfaces
2 - ATA 71 Power Plant
2.1 Engine Cowlings - Description / Access
2.2 Engine Mounts - Forward/Aft
2.3 Nacelle/Strut Basics for Ground Ops & Limits
3 - 72-00 Engine Modules
3.1 Module Description / Arrangement
3.2 Main Bearings
3.3 Cold Section
3.4 Hot Section
3.5 Gearbox & Accessories
3.6 Airflow
4 - ATA 73 - FADEC / Fuel & Control (73-21)
4.1 EEC/FADEC Description
4.2 Engine Control Interfaces & Sensors
4.3 Maintenance/Pages Reference
5 - ATA 74 - Ignition System (74-00)
5.1 General
5.2 Ignition Exciters
5.3 Ignition Leads
5.4 Igniters
5.5 Engine Relay Unit (ERU)
6 - ATA 75 - Air System / Cooling & Variable Geometry
6.1 Compressor Bleed Control - General
6.2 2.5 Bleed Subsystem
6.3 2.9 Bleed Subsystem
6.4 Variable Stator Vanes / Actuation (SVA)
6.5 Turbine Case Cooling (TCC)
6.6 Turbine Vane & Blade Cooling (TVBC)
7 - ATA 76 - Engine Control
7.1 Thrust Levers, Autothrottle, TRA/TLA basics
7.2 EEC Functions & Interfaces
8 - ATA 77 - Engine Indicating & Vibration
8.1 EPCS / Maintenance Page Access & Parameters
8.2 Performance Maintenance Page
9 - ATA 78 - Exhaust / Thrust Reverser
9.1 Thrust Reverser Description
9.2 Interlocks / Indications
10 - ATA 79 - Engine Oil
10.1 System Overview & Component Locations
10.2 Lube & Scavenge Pump / Main Filter / Chip Detectors
10.3 Fuel/Oil Cooler & Bypass Valve
10.4 Oil Indicating
10.5 Breather Path Items
10.6 Engine air/oil heat exchanger
10.7 FCOC outlet manifold
10.8 No. 3 bearing breather restrictor valve
10.9 Low oil PR SW and oil PR sensor
11 - ATA 80 - Starting System
11.1 Starter & Start Valve
11.2 Autostart Logic (SCU basics)
11.3 Handling/Servicing & Limits
12 - ATA 30-21 - Ice & Rain Protection
12.1 Engine Lip Anti-Ice Interface
13 - 71-00 Power Plant General
13.1 Safety Precautions / Danger Zones
13.2 Ground Operation in Icing / Continuous Ignition Use
13.3 Start Limits & Abnormals

Available for organizations and individuals

Organizations

  • Licensing for teams and classrooms.
  • Windows/macOS deployment with internet access.
  • Instructor-led or self-paced options.
Email us for a quote

Individuals

  • Purchase via our website store (like your current products).
  • Note: this Level 3 CBT alone does not issue a certificate.

If you need a certificate, choose A330 General Familiarization or Refresher, or email us for Type Rating (B1/B2).

A330 Gen Fam A330 Refresher Email us about Type Rating

Type rating programs (B1/B2)

We deliver theory and practical type rating training for aircraft engineers (B1/B2) under EASA license.

If you require approval or documentation for another national CAA, contact us.

Email us about Type Rating

FAQ

Who can buy this course?

Both organizations and individuals. Individuals purchase through our website store. Organizations should email us to set up licensing and deployment.

Will I receive a certificate from this CBT?

No. This Level 3 CBT by itself does not issue a certificate. For certificates, choose A330 General Familiarization or Refresher (store pages coming soon), or email us for Type Rating (B1/B2).

How do organizations deploy it?

Windows and macOS installers with internet connection. Tablet/iPad build available on request. Supports instructor-led and self-paced use.

Do you provide B1/B2 type rating?

Yes. We deliver theory and practical type rating programs for B1/B2 under EASA license. If you need approval or paperwork for another national CAA, contact us.

Shopping cart0
There are no products in the cart!
Continue shopping
0