Turbine Aeroplane Aerodynamics, Structures & Systems (B1) - EASA (Jul 24 Update)
The Turbine Aeroplane Aerodynamics, Structures, and Systems (M11A) Module for B1.1, compliant with PCAA ANO-066 standards, offers comprehensive training on ...
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Instructor
Omar Hayat Khan
- Description
- Curriculum
- Reviews
Introduction:
The Turbine Aeroplane Aerodynamics, Structures, and Systems (M11A) Module for B1.1, aligned with PCAA ANO-066 standards, is designed to provide aircraft maintenance engineers with the knowledge and skills necessary to maintain and troubleshoot turbine-powered aircraft. Covering aerodynamics, structural integrity, and aircraft systems, the course ensures that participants gain a deep understanding of how turbine-powered aircraft function and how to ensure their safe operation. By the end of the course, participants will be fully equipped to meet the requirements for B1.1 certification and work effectively in PCAA Part-145 approved organizations.
Course Features:
- Comprehensive Aerodynamics for Turbine Aircraft: Understand the principles of aerodynamics as they apply to turbine aeroplanes, including lift, drag, thrust, and control surface operation.
- Aircraft Structural Integrity: Learn about the structural components of turbine aircraft, including fuselage, wings, empennage, and landing gear, with a focus on maintaining structural safety and airworthiness.
- Turbine Aircraft Systems: Gain in-depth knowledge of aircraft systems such as hydraulic, pneumatic, pressurization, fuel, and landing gear systems, critical for maintaining turbine aircraft functionality.
- Troubleshooting and Maintenance Practices: Develop practical skills in diagnosing and resolving issues in aircraft structures and systems, preparing you for real-world maintenance tasks.
- PCAA ANO-066 Compliance: The course is fully compliant with PCAA ANO-066 standards, ensuring that participants are ready for B1.1 certification and capable of meeting the regulatory requirements for maintaining turbine-powered aircraft.
Target Audience:
This course is designed for aircraft maintenance engineers, technicians, and aviation professionals seeking PCAA ANO-066 B1.1 certification. It is especially beneficial for those working or aspiring to work within PCAA Part-145 approved maintenance organizations, focusing on the maintenance, repair, and troubleshooting of turbine-powered aircraft systems and structures. Whether you are preparing for certification or looking to enhance your expertise in turbine aeroplane maintenance, this course offers the essential skills and knowledge required for success in B1.1-certified maintenance roles.
11A.1.1 Aeroplane Aerodynamics and Flight Controls (Theory of Flight)
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11.1.1.1 Operation and Effect of Roll Control: Ailerons (L2) -
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11.1.1.2 Operation and Effect of Spoilers. (L2)
Operation and Effect of Spoiler
A spoiler is a device found on the upper surface of many heavy and high -performance aircraft. It is stowed flush to the wing’s upper surface. When deployed, it raises up into the air stream and disrupts the laminar airflow of the wing, thus reducing lift. Spoilers are made with similar construction materials and techniques as the other flight control surfaces on the aircraft. Often, they are honeycomb-core flat panels.
At low speeds, spoilers are rigged to operate when the ailerons operate to assist with the lateral movement and stability of the aircraft. On the wing where the aileron is moved up, the spoilers also raise thus amplifying the reduction of lift on that wing. Figure 11.1.1.2-1 On the wing with downward aileron deflection, the spoilers remain stowed. As the speed of the aircraft increases, the ailerons become more effective and the spoiler interconnect disengages.Note that spoilers are also used in as drag inducing devices.
Figure 11.1.1.2-1 Operation and effect of spoiler
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11.1.1.3 Operation and Effect of Pitch Control Devices , Elevator (L2)
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11.1.1.4 Stabilators and Variable Incidence Stabilisers (L2)
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11.1.1.5 Canards (L2)
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11.1.1.6 Operation and Effect of Yaw Control (L2)
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11.1.1.7 Rudder Limiters (L2)
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11.1.1.8 Control using Elevons (L2)
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11.1.1.9 Ruddervators (L2)
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11.1.1.10 High Lift Devices, Slots, Slats, Flaps, Flaperons (L2)
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11.1.1.11 Drag Inducing Devices, Spoilers, Lift Dumpers (L2)
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11.1.1.12 Speed Brakes (L2)
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11.1.1.13 Effects of Wing Fences and Saw Tooth Leading Edges (L2)
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11.1.1.14 Boundary Layer Control (L2)
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11.1.1.15 Vortex Generators and Stall Wedges or Leading Edge Devices (L2)
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11.1.1.16 Operation and Effect of Trim Tabs, Balance Tabs and Antibalance (leading) Tabs(L2)
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11.1.1.17 Servo Tabs, Spring Tabs and Mass Balance(L2)
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11.1.1.18 Control Surface Bias and Aerodynamic Balance Panels (L2)
11A.1.2 High Speed Flight
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11.1.2.1 Speed of Sound (L2)
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11.1.2.2 Subsonic Flight, Transonic Flight, Supersonic Flight(L2)
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11.1.2.3 Mach Number, Critical Mach number (L2)
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11.1.2.4 Compressibility Buffet (L2)
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11.1.2.5 Shock Wave and Aerodynamics Heating (L2)
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11.1.2.6 Area Rule (L2)
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11.1.2.7 Factors Affecting Airflow in Engine Intakes of High Speed Aircraft (L2)
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11.1.2.8 Effects of Sweepback on Critical Mach Number (L2)
11A.2 General Concepts (Airframe Structures)
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11.2a.1 Airworthiness Requirements for Structural Strength (L2)
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11.2a.2 Structural Classification, Primary, Secondary and Tertiary (L2)
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11.2a.3 Fail Safe,Safe Life, Damage Tolerance Concept (L2)
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11.2a.4 Zonal and Station Identification System (L2)
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11.2a.5 Structural Stresses (Stress, Strain) (L2)
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11.2a.6 Fatigue (L2)
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11.2a.7 Bending, Compression, Shear, Torsion and Tension (L2)
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11.2a.8 Hoop Stress (L2)
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11.2a.9 Drains and Ventilation Provisions (L2)
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11.2a.10 System Installation Provisions (L2)
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11.2a.11 Lightening Strike Protection And Bonding (L2)
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11.2a.12 Aircraft Bonding (L2)
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11.2b.1 Construction Methods of Stressed Skin Fuselage, Formers (L2)
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11.2b.2 Construction Methods of Stringers, Longerons, Bulkheads, Frames (L2)
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11.2b.3 Construction Methods of Doubler, Struts, Ties, Beam Floor Structures (L 2)
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11.2b.4 Construction Methods of Reinforcement(L2)
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11.2b.5 Method of Skinning, Anti-Corrosive Protection (L2)
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11.2b.6 Construction Methods of Wing , Empannage (L 2)
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11.2b.7 Construction Methods of Engine Attachments (L 2)
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11.2b.8 Structure Assembly Techniques: Riveting, Bolting, Bonding (L2)
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11.2b.9 Method of Surface Protection, Such as Chromating, Anodising and Painting (L2)
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11.2b.10 Surface Cleaning (L2)
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11.2b.11 Airframe Symmetry, Mehtods of Alignment and Symmetry Checks (L2)
11A.3.1 Fuselage (ATA 52/53/56) (Airframe structure- Aeroplanes)
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11.3.1.1 Fuselage-Construction and Pressurization Sealing (L2)
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11.3.1.2 Wing, Stabilizer, Undercarriage Attachments (L2)
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11.3.1.3 Pylons, Seat Installation and Cargo Loading System (L2)
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11.3.1.4 Doors and Emergency Exits: Construction, Mechanisms (L2)
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11.3.1.5 Operation and Safety Devices ( L 2 )
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11.3.1.6 Windows and Windscreen Construction and Mechanisms. ( L 2 )
11A.3.2 Wings (ATA 57) (Airframe structure-Aeroplanes)
11A.3.3 Stabilisers (ATA 55) (Airframe structure-Aeroplanes)
11A.3.4 Flight Control Surfaces (ATA 55/57) (Airframe structure-Aeroplanes)
11A.3.5 Nacelles/Pylons (ATA 54) (Airframe structure-Aeroplanes)
11A.4.1 Air supply (Air Conditioning and Cabin Pressurisation)
11A.4.2 Air Conditioning (Air Conditioning and Cabin Pressurisation)
11A.4.3 Pressurisation (Air Conditioning and Cabin Pressurisation)
11A.4.4 Safety and warning devices (Air Conditioning and Cabin Pressurisation)
11A.5.1 Instrument Systems (ATA 31) (Instruments/Avionic Systems)
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11.5.1.1 Pitot Static System (L2)
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11.5.1.2 Altimeters, Air Speed Indicator and Vertical Speed Indicator (L2)
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11.5.1.3 Artificial Horizon, Attitude Director (L2)
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11.5.1.5 Direction Indicator,Horizontal Situation Indicator and Turn and Slip Indicator (L2)
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11.5.1.6 Turn Coordinator (L2)
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11.5.1.7 Compasses Direct Reading and Remote Reading (L2)
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11.5.1.8 Angle of Attack Indication Stall Warning Systems Amp and Other Aircraft System Indication (L2)
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11.5.1.9 Glass Cockpit (L2)
11A.5.2 Avionic Systems (Instruments/Avionic Systems)
11A.6 Electrical Power (ATA 24)
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11.6.1 Batteries Installation and Operation (L3)
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11.6.2 DC Power Generation (L3)
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11.6.3 AC Power Generation (L3)
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11.6.4 Emergency Power Generation (L3)
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11.6.5 Voltage Regulation (L3)
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11.6.6 Power Distribution (L3)
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11.6.7 Inverters, Transformers and Rectifiers (L3)
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11.6.8 Circuit Protection(L3)
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11.6.9 External/Ground Power (L3)
11A.7a Emergency equipment requirements (Equipment and Furnishings )
11A.7b Cabin lay-out (Equipment and Furnishings )
11A.8a Fire and smoke detection and warning systems (Fire Protection -ATA 26)
11A.9 Flight Controls (ATA 27)
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11.9.1 Primary controls: Aileron, Elevator, Rudder and Spoiler (L3)
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11.9.2 Trim Controls (L3)
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11.9.3 Active Load Control (L3)
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11.9.4 High Lift Devices (L3)
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11.9.5 Lift Dump (L3)
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11.9.6 Speed Brakes (L3)
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11.9.7 Flight Control System Operation: Manual, Hydraulic, Electrical and Fly By Wire (L3)
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114
11.9.8 Pneumatic Flight Control Operation (L3)
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11.9.9 Artificial Feel and Mach Trim (L3)
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11.9.10 Yaw Damper and Rudder Limiter (L3)
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11.9.11 Gust Locks Systems
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11.9.12 Balancing and Rigging (L3)
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11.9.13 Stall Protection and Warning system (L3)
11A.10 Fuel Systems (ATA 28)
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11.10.1 Aircraft Fuel System Lay-out; Fuel Tanks (L3)
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11.10.2 Supply Systems; Dumping, Venting and Draining; (L3)
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11.10.3 Cross Feed and Transfer System (L3)
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11.10.4 Indications and Warnings (L3)
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11.10.5 Refuelling and Defuelling (L3)
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11.10.6 Longitudinal Balance Fuel System (L3)
11A.11 Hydraulic Power (ATA 29)
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11.11.1 Hydraulic Power System Lay-Out (L3)
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11.11.2 Hydraulic Fluids (L3)
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11.11.3 Hydraulic Reservoirs and Accumulators (L3)
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11.11.4 Pressure Generation: Filter, Electric, Mechanical and Pneumatic (L3)
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11.11.5 Emergency Pressure Generation (L3)
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11.11.6 Filters (L3)
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11.11.7 Pressure Control (L3)
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11.11.8 Power Distribution (L3)
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11.11.9 Indication and Warning Systems (L3)
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11.11.10 Interface with other Systems (L3)
11A.12 Ice and Rain Protection (ATA 30)
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11.12.1 Ice and Rain Protection; Ice Formation, Classification and Detection (L3)
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11.12.2 Anti-Icing Systems: Electrical, Hot Air and Chemical (L3)
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11.12.3 De-Icing Systems: Electrical, Hot Air, Pneumatic and Chemical (L3)
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139
11.12.4 Rain Repellant (L3)
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140
11.12.5 Probe and Drain Heating (L3)
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141
11.12.6 Wiper Systems (L3)
11A.13 Landing Gear (ATA 32)
11A.14 Lights (ATA 33)
11A.15 Oxygen (ATA 35)
11A.16 Pneumatic/Vacuum (ATA 36)
11A.17 Water/Waste (ATA 38)
11A.18 On Board Maintenance Systems (ATA 45)
11A.19 Integrated Modular Avionics (ATA42)
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168
11a.19.1 Functions that may be typically integrated in the Integrated Modular Avionic (IMA) Modules are, among others: Bleed Management, Air Pressure Control, Air Ventilation and Control, Avionics and Cockpit Ventilation Control, Temperature Control, Air Traffic Communication, Avionics Communication Router, Electrical Load Management, Circuit Breaker Monitoring, Electrical System BITE, Fuel Management, Braking Control, Steering Control, Landing Gear Extension and Retraction, Tyre Pressure Indication, Oleo Pressure Indication, Brake Temperature Monitoring, etc.; (L2)
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11.19.2 Core System (L2)
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11.19.3 Network Components (L2)
11A.20 Cabin Systems (ATA44)
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11.20.1 The units and Components which Furnish a Means of Entertaining the Passengers and Providing Communication within the Aircraft (CIDS) (L2)
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11.20.2 The Units and Components Which Communicates Between the Aircraft Cabin and Ground Stations (Cabin Network Service) Includes Voice, Data, Music and Video Transmissions. (L2)
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11.20.3 The Cabin Intercommunication Data System and Flight Attendant Panel (L2)
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11.20.4 Data/Radio Communication, In-Flight Entertainment System (L2)
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175
11.20.5 Access to Pre-Departure/Departure Reports (L2)
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11.20.6 E-mail / Intranet / Internet access (L2)
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177
11.20.7 Passenger Database (L2)
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178
11.20.8 In-flight Entertainment System (L2)
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179
11.20.9 External Communication System (L2)
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180
11.20.10 Cabin Mass Memory System (L2)
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11.20.11 Cabin Monitoring System (L2)
11A.21 Information Systems (ATA46)
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11.21.1 Information Storage and Retrieval (L2)
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11.21.2 Aircraft General Information System (L2)
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11.21.3 Flight Deck Information System (L2)
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11.21.4 Maintenance Information System (L2)
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186
11.21.5 Passenger Cabin Information System (L2)
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187
11.21.6 Miscellaneous Information System (L2)
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Course details
Lectures
187
Level
Beginner
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