Module 17A

MODULE 17A. PROPELLER

Note: This module does not apply to category B3. Relevant subject matters for category B3 are defined in module 17B.

17.1 Fundamentals:-
        Blade element theory;
        High/low blade angle, reverse angle, angle of attack, rotational speed;
        Propeller slip;
        Aerodynamic, centrifugal, and thrust forces;
        Torque;
        Relative airflow on blade angle of attack;
        Vibration and resonance.

17.2 Propeller Construction
       Construction methods and materials used in wooden, composite and metal propellers;
       Blade station, blade face, blade shank, blade back and hub assembly;
       Fixed pitch, controllable pitch, constant speeding propeller;
       Propeller/spinner installation.

17.3 Propeller Pitch Control
       Speed control and pitch change methods, mechanical and electrical/electronic;
       Feathering and reverse pitch;
       Overspeed protection.

17.4 Propeller Synchronising
       Synchronising and synchrophasing equipment.

17.5 Propeller Ice Protection
        Fluid and electrical de-icing equipment.

17.6 Propeller Maintenance
        Static and dynamic balancing;
        Blade tracking;
        Assessment of blade damage, erosion, corrosion, impact damage, delamination;
        Propeller treatment/repair schemes;
        Propeller engine running.

17.7 Propeller Storage and Preservation
        Propeller preservation and depreservation

Module 13

MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

13.1 Theory of Flight
        (a) Aeroplane Aerodynamics and Flight Controls Operation and effect of:
             — roll control: ailerons and spoilers,
             — pitch control: elevators, stabilators, variable incidence stabilisers and canards,
             — yaw control, rudder limiters; Control using elevons, ruddervators;
            High lift devices: slots, slats, flaps;
            Drag inducing devices: spoilers, lift dumpers, speed brakes;
            Operation and effect of trim tabs, servo tabs, control surface bias;
           (b) High Speed Flight
           Speed of sound, subsonic flight, transonic flight, supersonic flight;
           Mach number, critical Mach number;
           (c) Rotary Wing Aerodynamics Terminology;
           Operation and effect of cyclic, collective and anti-torque controls.

13.2 Structures — General Concepts
        (a) Fundamentals of structural systems;
        (b) Zonal and station identification systems;
             Electrical bonding;
             Lightning strike protection provision.

13.3 Autoflight (ATA 22)
        Fundamentals of automatic flight control including working principles and current
          terminology;
        Command signal processing;
        Modes of operation: roll, pitch and yaw channels;
        Yaw dampers;
        Stability Augmentation System in helicopters;
        Automatic trim control;
        Autopilot navigation aids interface;
        Autothrottle systems;
        Automatic Landing Systems: principles and categories, modes of operation,
          approach, glideslope, land,
          go-around, system monitors and failure conditions.

13.4 Communication/Navigation (ATA 23/34)
         Fundamentals of radio wave propagation, antennas, transmission lines,
          communication, receiver and transmitter;
        Working principles of following systems:
        — Very High Frequency (VHF) communication,
        — High Frequency (HF) communication,
        — Audio,
        — Emergency Locator Transmitters,
        — Cockpit Voice Recorder,
        — Very High Frequency omnidirectional range (VOR),
        — Automatic Direction Finding (ADF),
        — Instrument Landing System (ILS),
        — Microwave Landing System (MLS),
        — Flight Director systems, Distance Measuring Equipment (DME),
       — Very Low Frequency and hyperbolic navigation (VLF/Omega), 
       — Doppler navigation,
       — Area navigation, RNAV systems,
       — Flight Management Systems,
       — Global Positioning System (GPS), Global Navigation Satellite Systems (GNSS),
       — Inertial Navigation System,
      — Air Traffic Control transponder, secondary surveillance radar,
      — Traffic Alert and Collision Avoidance System (TCAS),
      — Weather avoidance radar,
      — Radio altimeter,
      — ARINC communication and reporting.

13.5 Electrical Power (ATA 24)
        Batteries Installation and Operation;
        DC power generation;
        AC power generation;
       Emergency power generation;
       Voltage regulation;
       Power distribution;
       Inverters, transformers, rectifiers;
       Circuit protection;
       External/Ground power.

13.6 Equipment and Furnishings (ATA 25)

        Electronic emergency equipment requirements;
        Cabin entertainment equipment.

13.7 Flight Controls (ATA 27)
        (a) Primary controls: aileron, elevator, rudder, spoiler;
             Trim control;
             Active load control;
            High lift devices;
            Lift dump, speed brakes;
            System operation: manual, hydraulic, pneumatic;
            Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks.
            Stall protection systems;
      (b) System operation: electrical, fly-by-wire.

13.8 Instruments (ATA 31)
        Classification;
        Atmosphere;
        Terminology;
        Pressure measuring devices and systems;
        Pitot static systems;
        Altimeters;
        Vertical speed indicators;
        Airspeed indicators;
       Machmeters;
       Altitude reporting/alerting systems;
      Air data computers;
      Instrument pneumatic systems;
      Direct reading pressure and temperature gauges;
      Temperature indicating systems;
      Fuel quantity indicating systems;
      Gyroscopic principles;
      Artificial horizons;
      Slip indicators;
      Directional gyros;
      Ground Proximity Warning Systems;
      Compass systems;
      Flight Data Recording systems;
      Electronic Flight Instrument Systems;
      Instrument warning systems including master warning systems and centralised
       warning panels;
     Stall warning systems and angle of attack indicating systems;
     Vibration measurement and indication;
     Glass cockpit

13.9 Lights (ATA 33)
        External: navigation, landing, taxiing, ice;
        Internal: cabin, cockpit, cargo;
        Emergency.

13.10 On Board Maintenance Systems (ATA 45)
         Central maintenance computers;
         Data loading system;
         Electronic library system;
         Printing;
         Structure monitoring (damage tolerance monitoring).

13.11 Air Conditioning and Cabin Pressurisation (ATA21)
         1) Air supply
             Sources of air supply including engine bleed, APU and ground cart;
         2) Air Conditioning
             Air conditioning systems;
             Air cycle and vapour cycle machines;
             Distribution systems;
             Flow, temperature and humidity control system.
         3) Pressurisation
             Pressurisation systems;
             Control and indication including control and safety valves;
             Cabin pressure controllers.
         4) Safety and warning devices
             Protection and warning devices.

13.12 Fire Protection (ATA 26)
         (a) Fire and smoke detection and warning systems;
              Fire extinguishing systems;
              System tests;
        (b) Portable fire extinguisher

13.13 Fuel Systems (ATA 28)
         System lay-out;
         Fuel tanks;
         Supply systems;
         Dumping, venting and draining;
         Cross-feed and transfer;
         Indications and warnings;
         Refuelling and defuelling;
         Longitudinal balance fuel systems.

13.14 Hydraulic Power (ATA 29)
         System lay-out;
         Hydraulic fluids;
         Hydraulic reservoirs and accumulators;
         Pressure generation: electrical, mechanical, pneumatic;
         Emergency pressure generation;
         Filters;
         Pressure control;
         Power distribution;
         Indication and warning systems;
         Interface with other systems.

13.15 Ice and Rain Protection (ATA 30)
          Ice formation, classification and detection;
          Anti-icing systems: electrical, hot air and chemical;
          De-icing systems: electrical, hot air, pneumatic, chemical; Rain repellent;
          Probe and drain heating; Wiper Systems.

13.16 Landing Gear (ATA 32)
          Construction, shock absorbing;
          Extension and retraction systems: normal and emergency;
          Indications and warnings;
         Wheels, brakes, antiskid and autobraking;
          Tyres;
          Steering;
          Air-ground sensing.

13.17 Oxygen (ATA 35)
          System lay-out: cockpit, cabin;
          Sources, storage, charging and distribution;
          Supply regulation;
          Indications and warnings.

13.18 Pneumatic/Vacuum (ATA 36)
          System lay-out;
          Sources: engine/APU, compressors, reservoirs, ground supply;
          Pressure control;
          Distribution;
          Indications and warnings;
          Interfaces with other systems.

13.19 Water/Waste (ATA 38)
          Water system lay-out, supply, distribution, servicing and draining;
          Toilet system lay-out, flushing and servicing.

13.20 Integrated Modular Avionics (ATA42)
          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.;
        Core System;
        Network Components.

13.21 Cabin Systems (ATA44)
           The units and components which furnish a means of entertaining the passengers and
             providing communication within the aircraft (Cabin Intercommunication Data
             System) and between the aircraft cabin and ground stations (Cabin Network Service).
           Includes voice, data, music and video transmissions.
           The Cabin Intercommunication Data System provides an interface between
             cockpit/cabin crew and cabin systems. These systems support data exchange of the
             different related LRU's and they are typically operated via Flight Attendant Panels.
          The Cabin Network Service typically consists on a server, typically interfacing with,
            among others, the following systems:
     —  Data/Radio Communication, In-Flight Entertainment System
           The Cabin Network Service may host functions such as:
     — Access to pre-departure/departure reports,
     — E-mail/intranet/Internet access,
     — Passenger database; Cabin Core System;
          In-flight Entertainment System; External Communication System; Cabin Mass Memory                      System; Cabin Monitoring System; Miscellaneous Cabin System.

13.22 Information Systems (ATA46)
          The units and components which furnish a means of storing, updating and retrieving digital                    information traditionally provided on paper, microfilm or microfiche. Includes units that are                dedicated to the information storage and retrieval function such as the electronic library mass              storage and controller. Does not include units or components installed for other uses and                      shared with other systems, such as flight deck printer or general use display.

         Typical examples include Air Traffic and Information Management Systems and Network                   Server Systems.

        Aircraft General Information System; Flight Deck Information System; Maintenance                            Information System; Passenger Cabin Information System; Miscellaneous Information System.



Module 12

MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

12.1 Theory of Flight — Rotary Wing Aerodynamics
Terminology;
Effects of gyroscopic precession;
Torque reaction and directional control;
Dissymmetry of lift, Blade tip stall;
Translating tendency and its correction;
Coriolis effect and compensation;
Vortex ring state, power settling, overpitching;
Auto-rotation;
Ground effect.

12.2 Flight Control Systems
Cyclic control;
Collective control;
Swashplate;
Yaw control: Anti-Torque Control, Tail rotor, bleed air;
Main Rotor Head: Design and Operation features;
Blade Dampers: Function and construction;
Rotor Blades: Main and tail rotor blade construction and attachment;
Trim control, fixed and adjustable stabilisers;
System operation: manual, hydraulic, electrical and flyby-wire;
Artificial feel;
Balancing and Rigging.

12.3 Blade Tracking and Vibration Analysis
Rotor alignment;
Main and tail rotor tracking;
Static and dynamic balancing;
Vibration types, vibration reduction methods;
Ground resonance.

12.4 Transmissions
Gear boxes, main and tail rotors;
Clutches, free wheel units and rotor brake.
Tail rotor drive shafts, flexible couplings, bearings,
vibration dampers and bearing hangers

12.5 Airframe Structures
(a) Airworthiness requirements for structural strength;
Structural classification, primary, secondary and tertiary;
Fail safe, safe life, damage tolerance concepts;
Zonal and station identification systems;
Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;
Drains and ventilation provisions;
System installation provisions;
Lightning strike protection provision.
(b) Construction methods of: stressed skin fuselage, formers, stringers, longerons,
bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement,
methods of skinning and anti-corrosive protection.
Pylon, stabiliser and undercarriage attachments;
Seat installation;
Doors: construction, mechanisms, operation and safety devices;
Windows and windscreen construction;
Fuel storage;
Firewalls;
Engine mounts;
Structure assembly techniques: riveting, bolting, bonding;
Methods of surface protection, such as chromating, anodising, painting;
Surface cleaning.
Airframe symmetry: methods of alignment and symmetry checks.

12.6 Air Conditioning (ATA 21)
12.6.1 Air supply
Sources of air supply including engine bleed and ground cart;
12.6.2 Air Conditioning
Air conditioning systems;
Distribution systems;
Flow and temperature control systems;
Protection and warning devices.

12.7 Instruments/Avionic Systems
12.7.1 Instrument Systems (ATA 31)
Pitot static:altimeter, air speed indicator, vertical speed indicator;
Gyroscopic:artificial horizon, attitude director, direction indicator, horizontal
situation indicator, turn and slip indicator, turn coordinator;
Compasses: direct reading, remote reading;
Vibration indicating systems — HUMS;
Glass Cockpit
Other aircraft system indication.
12.7.2 Avionic Systems
Fundamentals of system layouts and operation of:
Auto Flight (ATA 22);
Communications (ATA 23);
Navigation Systems (ATA 34).

12.8 Electrical Power (ATA 24)
Batteries Installation and Operation;
DC power generation, AC power generation;
Emergency power generation;
Voltage regulation, Circuit protection.
Power distribution;
Inverters, transformers, rectifiers;
External/Ground power.

12.9 Equipment and Furnishings (ATA 25)
(a) Emergency equipment requirements;
Seats, harnesses and belts;
Lifting systems.
(b) Emergency flotation systems;
Cabin lay-out, cargo retention;
Equipment lay-out;
Cabin Furnishing Installation.

12.10 Fire Protection (ATA 26)
Fire and smoke detection and warning systems;
Fire extinguishing systems;
System tests.

12.11 Fuel Systems (ATA 28)
System lay-out;
Fuel tanks;
Supply systems;
Dumping, venting and draining;
Cross-feed and transfer;
Indications and warnings;
Refuelling and defuelling.

12.12 Hydraulic Power (ATA 29)
System lay-out;
Hydraulic fluids;
Hydraulic reservoirs and accumulators;
Pressure generation: electric, mechanical, pneumatic;
Emergency pressure generation;
Filters
Pressure Control;
Power distribution;
Indication and warning systems;
Interface with other systems.

12.13 Ice and Rain Protection (ATA 30)
Ice formation, classification and detection;
Anti-icing and de-icing systems: electrical, hot air and chemical;
Rain repellant and removal;
Probe and drain heating.
Wiper system

12.14 Landing Gear (ATA 32)
Construction, shock absorbing;
Extension and retraction systems: normal and emergency;
Indications and warning;
Wheels, tyres, brakes;
Steering;
Air-ground sensing
Skids, floats.

12.15 Lights (ATA 33)
External: navigation, landing, taxiing, ice;
Internal: cabin, cockpit, cargo;
Emergency.

12.16 Pneumatic/Vacuum (ATA 36)
System lay-out;
Sources: engine, compressors, reservoirs, ground supply.;
Pressure control;
Distribution;
Indications and warnings;
Interfaces with other systems.

12.17 Integrated Modular Avionics (ATA42)
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.
Core System;
Network Components.

12.18 On Board Maintenance Systems (ATA45)
Central maintenance computers; Data loading system;
Electronic library system; Printing;
Structure monitoring (damage tolerance monitoring).

12.19 Information Systems (ATA46)
The units and components which furnish a means of storing, updating and retrieving digital information traditionally provided on paper, microfilm or microfiche. Includes units that are dedicated to the information storage and retrieval function such as the electronic library mass storage and controller. Does not include units or components installed for other uses and shared with other systems, such as flight deck printer or general use display.
Typical examples include Air Traffic and Information Management Systems and Network Server Systems.
Aircraft General Information System; Flight Deck Information System; Maintenance Information System; Passenger Cabin Information System; Miscellaneous Information System.



Module 11C

MODULE 11C. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
Note: The scope of this module shall reflect the technology of aeroplanes pertinent to the B3 category.

11.1 Theory of Flight
11.1.1 Aeroplane Aerodynamics and Flight Controls
Operation and effect of:
— roll control: ailerons and spoilers;
pitch control: elevators, stabilators, variable incidence stabilisers and canards;
yaw control, rudder limiters; Control using elevons, ruddervators;
High lift devices, slots, slats, flaps, flaperons;
Drag inducing devices, spoilers, lift dumpers, speed brakes; Effects of wing fences, saw tooth leading edges;
Boundary layer control using, vortex generators, stall wedges or leading edge devices;
Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamic balance panels;

11.2 Airframe Structures — General Concepts
(a) Airworthiness requirements for structural strength;
Structural classification, primary, secondary and tertiary;
Fail safe, safe life, damage tolerance concepts;
Zonal and station identification systems;
Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;
Drains and ventilation provisions;
System installation provisions;
Lightning strike protection provision.
Aircraft bonding
(b) Construction methods of: stressed skin fuselage, formers, stringers, longerons,
bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement,
methods of skinning, anti-corrosive protection, wing, empennage and engine
attachments;
Structure assembly techniques: riveting, bolting, bonding;
Methods of surface protection, such as chromating,
anodising, painting;
Surface cleaning;
Airframe symmetry: methods of alignment and symmetry checks.

11.3 Airframe Structures — Aeroplanes
11.3.1 Fuselage (ATA 52/53/56)
Construction and pressurisation sealing;
Wing, tail-plane pylon and undercarriage attachments;
Seat installation;
Doors and emergency exits: construction and operation;
Window and windscreen attachment.
11.3.2 Wings (ATA 57)
Construction;
Fuel storage;
Landing gear, pylon, control surface and high lift/drag attachments.
11.3.3 Stabilisers (ATA 55)
Construction;
Control surface attachment.
11.3.4 Flight Control Surfaces (ATA 55/57)
Construction and attachment;
Balancing — mass and aerodynamic.
11.3.5 Nacelles/Pylons (ATA 54)
Nacelles/Pylons:
— Construction;
— Firewalls;
— Engine mounts.

11.4 Air Conditioning (ATA 21)
Heating and ventilation Systems

11.5 Instruments/Avionic Systems
11.5.1 Instrument Systems (ATA 31)
Pitot static: altimeter, air speed indicator, vertical speed indicator;
Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal
situation indicator, turn and slip indicator, turn coordinator;
Compasses: direct reading, remote reading;
Angle of attack indication, stall warning systems.
Glass cockpit;
Other aircraft system indication.
11.5.2 Avionic Systems
Fundamentals of system lay-outs and operation of:
— Auto Flight (ATA 22);
— Communications (ATA 23);
— Navigation Systems (ATA 34).

11.6 Electrical Power (ATA 24)
Batteries Installation and Operation;
DC power generation;
Voltage regulation;
Power distribution;
Circuit protection;
Inverters, transformers.

11.7 Equipment and Furnishings (ATA 25)
Emergency equipment requirements;
Seats, harnesses and belts.

11.8 Fire Protection (ATA 26)
Portable fire extinguisher.

11.9 Flight Controls (ATA 27)
Primary controls: aileron, elevator, rudder;
Trim tabs;
High lift devices;
System operation: manual;
Gust locks;
Balancing and rigging;
Stall warning system.

11.10 Fuel Systems (ATA 28)
System lay-out;
Fuel tanks;
Supply systems;
Cross-feed and transfer;
Indications and warnings;
Refuelling and defuelling.

11.11 Hydraulic Power (ATA 29)
System lay-out;
Hydraulic fluids;
Hydraulic reservoirs and accumulators;
Pressure generation: electric, mechanical;
Filters
Pressure Control;
Power distribution;
Indication and warning systems.

11.12 Ice and Rain Protection (ATA 30)
Ice formation, classification and detection;
De-icing systems: electrical, hot air, pneumatic and chemical;
Probe and drain heating;
Wiper systems.

11.13 Landing Gear (ATA 32)
Construction, shock absorbing;
Extension and retraction systems: normal and emergency;
Indications and warning;
Wheels, brakes, antiskid and auto braking;
Tyres;
Steering.

11.14 Lights (ATA 33)
External: navigation, anti collision, landing, taxiing, ice;
Internal: cabin, cockpit, cargo;
Emergency.

11.15 Oxygen (ATA 35)
System lay-out: cockpit, cabin;
Sources, storage, charging and distribution;
Supply regulation;
Indications and warnings;

11.16 Pneumatic/Vacuum (ATA 36)
System lay-out;
Sources: engine/APU, compressors, reservoirs, ground supply; Pressure and vaccum pumps
Pressure control;
Distribution;
Indications and warnings; Interfaces with other systems.


Module 11B

MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
Note 1: This module does not apply to category B3. Relevant subject matters for category B3 are defined in module 11C.
Note 2: The scope of this Module should reflect the technology of aeroplanes pertinent to the A2 and B1.2 subcategory.

11.1 Theory of Flight
11.1.1 Aeroplane Aerodynamics and Flight Controls
Operation and effect of:
— roll control: ailerons and spoilers;
— pitch control: elevators, stabilators, variable incidence stabilisers and canards;
— yaw control, rudder limiters;
Control using elevons, ruddervators;
High lift devices, slots, slats, flaps, flaperons;
Drag inducing devices, spoilers, lift dumpers, speed brakes;
Effects of wing fences, saw tooth leading edges;
Boundary layer control using, vortex generators, stall wedges or leading edge
devices;
Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs,
spring tabs, mass balance, control surface bias, aerodynamic balance panels;

11.1.2 High Speed Flight — N/A —
11.2 Airframe Structures — General Concepts
(a) Airworthiness requirements for structural strength;
Structural classification, primary, secondary and tertiary;
Fail safe, safe life, damage tolerance concepts;
Zonal and station identification systems;
Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;
Drains and ventilation provisions;
System installation provisions;
Lightning strike protection provision.
Aircraft bonding
(b) Construction methods of: stressed skin fuselage, formers, stringers, longerons,
bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement,
methods of skinning, anti-corrosive protection, wing, empennage and engine
attachments;
Structure assembly techniques: riveting, bolting, bonding;
Methods of surface protection, such as chromating,
anodising, painting;
Surface cleaning;
Airframe symmetry: methods of alignment and symmetry checks.

11.3 Airframe Structures — Aeroplanes
11.3.1 Fuselage (ATA 52/53/56)
Construction and pressurisation sealing;
Wing, tail-plane pylon and undercarriage attachments;
Seat installation;
Doors and emergency exits: construction and operation;
Window and windscreen attachment.

11.3.2 Wings (ATA 57)
Construction;
Fuel storage;
Landing gear, pylon, control surface and high lift/drag attachments.

11.3.3 Stabilisers (ATA 55)
Construction;
Control surface attachment.

11.3.4 Flight Control Surfaces (ATA 55/57)
Construction and attachment;
Balancing — mass and aerodynamic.

11.3.5 Nacelles/Pylons (ATA 54)

Nacelles/Pylons:
— Construction;
— Firewalls;
— Engine mounts.

11.4 Air Conditioning and Cabin Pressurisation (ATA 21)
Pressurisation and air conditioning systems;
Cabin pressure controllers, protection and warning devices
Heating Systems

11.5 Instruments/Avionic Systems
11.5.1 Instrument Systems (ATA 31)
Pitot static: altimeter, air speed indicator, vertical speed indicator;
Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal
situation indicator, turn and slip indicator, turn coordinator;
Compasses: direct reading, remote reading;
Angle of attack indication, stall warning systems.
Glass cockpit;
Other aircraft system indication.
11.5.2 Avionic Systems
Fundamentals of system lay-outs and operation of:
— Auto Flight (ATA 22);
— Communications (ATA 23);
— Navigation Systems (ATA 34).

11.6 Electrical Power (ATA 24)
Batteries Installation and Operation;
DC power generation;
Voltage regulation;
Power distribution;
Circuit protection;
Inverters, transformers.

11.7 Equipment and Furnishings (ATA 25)
(a) Emergency equipment requirements;
Seats, harnesses and belts.
(b) Cabin lay-out;
Equipment lay-out;
Cabin Furnishing Installation (level 2);
Cabin entertainment equipment;
Galley installation;
Cargo handling and retention equipment;
Airstairs.

11.8 Fire Protection (ATA 26)
(a) Fire extinguishing systems;
Fire and smoke detection and warning systems;
System tests.
(b) Portable fire extinguisher.

11.9 Flight Controls (ATA 27)
Primary controls: aileron, elevator, rudder;
Trim tabs;
High lift devices;
System operation: manual;
Gust locks;
Balancing and rigging;
Stall warning system.

11.10 Fuel Systems (ATA 28)
System lay-out;
Fuel tanks;
Supply systems;
Cross-feed and transfer;
Indications and warnings;
Refuelling and defuelling.

11.11 Hydraulic Power (ATA 29)
System lay-out;
Hydraulic fluids;
Hydraulic reservoirs and accumulators;
Pressure generation: electric, mechanical;
Filters
Pressure Control;
Power distribution;
Indication and warning systems.

11.12 Ice and Rain Protection (ATA 30)
Ice formation, classification and detection;
De-icing systems: electrical, hot air, pneumatic and chemical;
Probe and drain heating;
Wiper systems.

11.13 Landing Gear (ATA 32)
Construction, shock absorbing;
Extension and retraction systems: normal and emergency;
Indications and warning;
Wheels, brakes, antiskid and auto braking;
Tyres;
Steering.
Air-ground sensing

11.14 Lights (ATA 33)
External: navigation, anti collision, landing, taxiing, ice;
Internal: cabin, cockpit, cargo;
Emergency.

11.15 Oxygen (ATA 35)
System lay-out: cockpit, cabin;
Sources, storage, charging and distribution; Supply regulation;
Indications and warnings;

11.16 Pneumatic/Vacuum (ATA 36)
System lay-out;
Sources: engine/APU, compressors, reservoirs, ground supply; Pressure control;
Distribution;
Indications and warnings; Interfaces with other systems.

11.17 Water/Waste (ATA 38)
Water system lay-out, supply, distribution, servicing and draining; Toilet system lay-out, flushing and servicing;
Corrosion aspects.



Module 11A

MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

11.1 Theory of Flight
11.1.1 Aeroplane Aerodynamics and Flight Controls
Operation and effect of:
— roll control: ailerons and spoilers;
— pitch control: elevators, stabilators, variable incidence stabilisers and canards;
— yaw control, rudder limiters;
Control using elevons, ruddervators;
High lift devices, slots, slats, flaps, flaperons;
Drag inducing devices, spoilers, lift dumpers, speed brakes;
Effects of wing fences, saw tooth leading edges;
Boundary layer control using, vortex generators, stall wedges or leading edge
devices;
Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs,
spring tabs, mass balance, control surface bias, aerodynamic balance panels;

11.1.2 High Speed Flight
Speed of sound, subsonic flight, transonic flight, supersonic flight,
Mach number, critical Mach number, compressibility buffet, shock wave,
aerodynamic heating, area rule;
Factors affecting airflow in engine intakes of high speed aircraft;
Effects of sweepback on critical Mach number.

11.2 Airframe Structures — General Concepts
(a) Airworthiness requirements for structural strength;
Structural classification, primary, secondary and tertiary;
Fail safe, safe life, damage tolerance concepts;
Zonal and station identification systems;
Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;
Drains and ventilation provisions;
System installation provisions;
Lightning strike protection provision.
Aircraft bonding
(b) Construction methods of: stressed skin fuselage, formers, stringers, longerons,
bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement,
methods of skinning, anti-corrosive protection, wing, empennage and engine
attachments;
Structure assembly techniques: riveting, bolting, bonding
Methods of surface protection, such as chromating, anodising, painting;
Surface cleaning.
Airframe symmetry: methods of alignment and symmetry checks.

11.3 Airframe Structures — Aeroplanes
11.3.1 Fuselage (ATA 52/53/56)
Construction and pressurisation sealing;
Wing, stabiliser, pylon and undercarriage attachments;
Seat installation and cargo loading system;
Doors and emergency exits: construction, mechanisms, operation and safety devices;
Windows and windscreen construction and mechanisms.
11.3.2 Wings (ATA 57)
Construction;
Fuel storage;
Landing gear, pylon, control surface and high lift/drag attachments.
11.3.3 Stabilisers (ATA 55)
Construction;
Control surface attachment.
11.3.4 Flight Control Surfaces (ATA 55/57)
Construction and attachment;
Balancing — mass and aerodynamic.
11.3.5 Nacelles/Pylons (ATA 54)
Construction;
Firewalls;
Engine mounts.

11.4 Air Conditioning and Cabin Pressurisation (ATA 21)
11.4.1 Air supply
Sources of air supply including engine bleed, APU and ground cart;
11.4.2 Air Conditioning
Air conditioning systems;
Air cycle and vapour cycle machines
Distribution systems;
Flow, temperature and humidity control system.
11.4.3 Pressurisation
Pressurisation systems;
Control and indication including control and safety valves;
Cabin pressure controllers.
11.4.4 Safety and warning devices
Protection and warning devices.

11.5 Instruments/Avionic Systems
11.5.1 Instrument Systems (ATA 31)
Pitot static: altimeter, air speed indicator, vertical speed indicator;
Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal
situation indicator, turn and slip indicator, turn coordinator;
Compasses: direct reading, remote reading;
Angle of attack indication, stall warning systems;
Glass Cockpit
Other aircraft system indication.
11.5.2 Avionic Systems
Fundamentals of system lay-outs and operation of;
Auto Flight (ATA 22);
Communications (ATA 23);
Navigation Systems (ATA 34).

11.6 Electrical Power (ATA 24)
Batteries Installation and Operation;
DC power generation;
AC power generation;
Emergency power generation;
Voltage regulation;
Power distribution;
Inverters, transformers, rectifiers;
Circuit protection.
External/Ground power;

11.7 Equipment and Furnishings (ATA 25)
(a) Emergency equipment requirements;
Seats, harnesses and belts.
(b) Cabin lay-out;
Equipment lay-out;
Cabin Furnishing Installation;
Cabin entertainment equipment;
Galley installation;
Cargo handling and retention equipment;
Airstairs.

11.8 Fire Protection (ATA 26)
(a) Fire and smoke detection and warning systems;
Fire extinguishing systems;
System tests.
(b) Portable fire extinguisher

11.9 Flight Controls (ATA 27)
Primary controls: aileron, elevator, rudder, spoiler;
Trim control;
Active load control;
High lift devices;
Lift dump, speed brakes;
System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire;
Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks systems;
Balancing and rigging;
Stall protection/warning system.

11.10 Fuel Systems (ATA 28)
System lay-out;
Fuel tanks;
Supply systems;
Dumping, venting and draining;
Cross-feed and transfer;
Indications and warnings;
Refuelling and defuelling;
Longitudinal balance fuel systems.

11.11 Hydraulic Power (ATA 29)
System lay-out;
Hydraulic fluids;
Hydraulic reservoirs and accumulators;
Pressure generation: electric, mechanical, pneumatic;
Emergency pressure generation;
Filters
Pressure Control;
Power distribution;
Indication and warning systems;
Interface with other systems.

11.12 Ice and Rain Protection (ATA 30)
Ice formation, classification and detection;
Anti-icing systems: electrical, hot air and chemical;
De-icing systems: electrical, hot air, pneumatic and chemical;
Rain repellant;
Probe and drain heating.
Wiper systems

11.13 Landing Gear (ATA 32)
Construction, shock absorbing;
Extension and retraction systems: normal and emergency;
Indications and warning;
Wheels, brakes, antiskid and autobraking;
Tyres;
Steering.
Air-ground sensing

11.14 Lights (ATA 33)
External: navigation, anti-collision, landing, taxiing, ice;
Internal: cabin, cockpit, cargo;
Emergency.

11.15 Oxygen (ATA 35)
System lay-out: cockpit, cabin;
Sources, storage, charging and distribution;
Supply regulation;
Indications and warnings;

11.16 Pneumatic/Vacuum (ATA 36)
System lay-out;
Sources: engine/APU, compressors, reservoirs, ground supply;
Pressure control;
Distribution;
Indications and warnings;
Interfaces with other systems.

11.17 Water/Waste (ATA 38)
Water system lay-out, supply, distribution, servicing and draining;
Toilet system lay-out, flushing and servicing;
Corrosion aspects.

11.18 On Board Maintenance Systems (ATA 45)
Central maintenance computers;
Data loading system;
Electronic library system;
Printing;
Structure monitoring (damage tolerance monitoring).

11.19 Integrated Modular Avionics (ATA42 )
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.

11.20 Cabin Systems (ATA44)
The units and components which furnish a means of entertaining the passengers and providing communication within the aircraft (Cabin Intercommunication Data System) and between the aircraft cabin and ground stations (Cabin Network Service). Includes voice, data, music and video transmissions.
The Cabin Intercommunication Data System provides an interface between cockpit/cabin crew and cabin systems. These systems support data exchange of the different related LRU's and they are typically operated via Flight Attendant Panels.
The Cabin Network Service typically consists on a server, typically interfacing with, among others, the following systems:
— Data/Radio Communication, In-Flight Entertainment System.
The Cabin Network Service may host functions such as:
Access to pre-departure/departure reports,
E-mail/intranet/Internet access, — Passenger database;
Cabin Core System;
In-flight Entertainment System; External Communication System; Cabin Mass Memory System; Cabin Monitoring System; Miscellaneous Cabin System.

11.21 Information Systems (ATA46)
The units and components which furnish a means of storing, updating and retrieving digital information traditionally provided on paper, microfilm or microfiche. Includes units that are dedicated to the information storage and retrieval function
such as the electronic library mass storage and controller. Does not include units or components installed for other uses and shared with other systems, such as flight deck printer or general use display.
Typical examples include Air Traffic and Information Management Systems and Network Server Systems
Aircraft General Information System; Flight Deck Information System; Maintenance Information System;
Passenger Cabin Information System;
Miscellaneous Information System.



Module 10

MODULE 10. AVIATION LEGISLATION (DGCA - INDIA)
10.1 Regulatory Framework
        Role of International Civil Aviation Organisation;
        The Aircraft Act and Rules made there under
        Role of the DGCA;
        Relationship between CAR-21, CAR-M, CAR-145, CAR-66, CAR 147
        The Aircraft Rules ( Applicable to Aircraft Maintenance and Release)
       Aeronautical Information Circulars ( Applicable to Aircraft Maintenance and Release)
       CAR Sections 1 and 2

10.2 CAR-66 Certifying Staff - Maintenance
        Detailed understanding of CAR-66.

10.3 CAR-145 — Approved Maintenance Organisations
        Detailed understanding of CAR-145 and CAR M Subpart F

10.4 Aircraft Operations
       Commercial Air Transport/Commercial Operations
       Air Operators Certificates;
       Operators Responsibilities, in particular regarding continuing airworthiness and maintenance;
       Documents to be carried on board;
       Aircraft Placarding (Markings);

10.5 Aircraft Certification
  (a) General
       Certification rules: such as FAA & EACS 23/25/27/29;
       Type Certification;
       Supplemental Type Certification;
       CAR-21 Design/Production Organisation Approvals.
       Aircraft Modifications and repairs approval and certification
       Permit to fly requirements
 (b) Documents
      Certificate of Airworthiness;
      Certificate of Registration;
      Noise Certificate;
      Weight Schedule;
      Radio Station Licence and Approval.

10.6 CAR-M
        Detail understanding of CAR M provisions related to Continuing Airworthiness
        Detailed understanding of CAR-M.

10.7 Applicable National and International Requirements
  (a) Maintenance Programme, Maintenance checks and inspections;
       Master Minimum Equipment Lists, Minimum Equipment
       List, Dispatch Deviation Lists;
       Airworthiness Directives;
       Service Bulletins, manufacturers service information;
       Modifications and repairs;
       Maintenance documentation: maintenance manuals, structural repair manual,
       illustrated parts catalogue, etc.;
 (b) Continuing airworthiness;
       Test flights;
       ETOPS /EDTO , maintenance and dispatch requirements;
       RVSM, maintenance and dispatch requirements
       RNP, MNPS Operations
       All Weather Operations,
      Category 2/3 operations and minimum equipment requirements.

10.8 Safety Management System
       State Safety Programme
       Basic Safety Concepts
       Hazards & Safety Risks
       SMS Operation
       SMS Safety performance
       Safety Assurance

10.9 Fuel Tank Safety
       Special Federal Aviation Regulations (SFARs) from 14 CFR SFAR 88 of the FAA
        and of JAA TGL 47
      Concept of CDCCL,
      Airworthiness Limitations Items (ALI)

Module 9B

MODULE 9B. HUMAN FACTORS
Note: The scope of this module shall reflect the less demanding environment of
maintenance for B3 licence holders.
9.1 General
      The need to take human factors into account;
      Incidents attributable to human factors/human error;
      ‘Murphy's’ law.
9.2 Human Performance and Limitations
      Vision;
      Hearing;
      Information processing;
      Attention and perception;
      Memory;
      Claustrophobia and physical access.
9.3 Social Psychology
      Responsibility: individual and group;
      Motivation and de-motivation;
      Peer pressure;
     ‘Culture’ issues;
      Team working;
      Management, supervision and leadership
9.4 Factors Affecting Performance
      Fitness/health;
      Stress: domestic and work related;
      Time pressure and deadlines;
      Workload: overload and underload;
      Sleep and fatigue, shiftwork;
      Alcohol, medication, drug abuse.
9.5 Physical Environment
      Noise and fumes;
      Illumination;
     Climate and temperature;
     Motion and vibration;
     Working environment.
9.6 Tasks
      Physical work;
      Repetitive tasks;
      Visual inspection;
      Complex systems.
9.7 Communication
     Within and between teams;
     Work logging and recording;
     Keeping up to date, currency; Dissemination of information.
9.8 Human Error
      Error models and theories;
      Types of error in maintenance tasks; Implications of errors (i.e accidents) Avoiding and 
       managing errors.
9.9 Hazards in the Workplace
      Recognising and avoiding hazards;
      Dealing with emergencies.

Module 9A

MODULE 9A. HUMAN FACTORS
Note: This module does not apply to category B3. Relevant subject matters for category
B3 are defined in module 9B.
9.1 General
      The need to take human factors into account; Incidents attributable to human factors/human error;
      ‘Murphy's’ law.
9.2 Human Performance and Limitations
      Vision;
      Hearing;
      Information processing; Attention and perception; Memory;
      Claustrophobia and physical access.
9.3 Social Psychology Responsibility: individual and group; Motivation and de-motivation;
      Peer pressure;
     ‘Culture’ issues;
      Team working;
      Management, supervision and leadership
9.4 Factors Affecting Performance
      Fitness/health;
      Stress: domestic and work related;
      Time pressure and deadlines;
      Workload: overload and underload;
      Sleep and fatigue, shiftwork;
      Alcohol, medication, drug abuse.
9.5 Physical Environment
      Noise and fumes;
      Illumination;
     Climate and temperature;
     Motion and vibration;
     Working environment.
9.6 Tasks
      Physical work;
      Repetitive tasks;
      Visual inspection;
      Complex systems.
9.7 Communication
      Within and between teams;
      Work logging and recording;
      Keeping up to date, currency;
      Dissemination of information.
9.8 Human Error
      Error models and theories;
      Types of error in maintenance tasks;
      Implications of errors (i.e accidents)
      Avoiding and managing errors.
9.9 Hazards in the Workplace
      Recognising and avoiding hazards;
      Dealing with emergencies.

Module 8

MODULE 8. BASIC AERODYNAMICS
8.1 Physics of the Atmosphere
      International Standard Atmosphere (ISA), application to aerodynamics.
8.2 Aerodynamics
      Airflow around a body;
      Boundary layer, laminar and turbulent flow, free stream flow, relative airflow, upwash and                    
      downwash, vortices, stagnation;
     The terms: camber, chord, mean aerodynamic chord, profile (parasite) drag, induced drag,
      centre of pressure, angle of attack, wash in and wash out, fineness ratio,
      wing shape and aspect ratio;
    Thrust, Weight, Aerodynamic Resultant;
    Generation of Lift and Drag: Angle of Attack, Lift coefficient,
    Drag coefficient, polar curve, stall;
    Aerofoil contamination including ice, snow, frost.
8.3 Theory of Flight
      Relationship between lift, weight, thrust and drag;
      Glide ratio;
      Steady state flights, performance;
      Theory of the turn;
      Influence of load factor: stall, flight envelope and structural limitations;
      Lift augmentation.
8.4 Flight Stability and Dynamics
      Longitudinal, lateral and directional stability (active and passive).

Module 7B

MODULE 7B. MAINTENANCE PRACTICES
Note: The scope of this module shall reflect the technology of aeroplanes relevant
to the B3 category.
7.1 Safety Precautions-Aircraft and Workshop
      Aspects of safe working practices including precautions to take when working
      with electricity, gases especially oxygen, oils and chemicals.
      Also, instruction in the remedial action to be taken in the event of a fire or
       another accident with one or more of these hazards including knowledge on extinguishing agents.
7.2 Workshop Practices
      Care of tools, control of tools, use of workshop materials;
      Dimensions, allowances and tolerances, standards of workmanship;
      Calibration of tools and equipment, calibration standards.
7.3 Tools
      Common hand tool types;
      Common power tool types;
      Operation and use of precision measuring tools;
      Lubrication equipment and methods.
     Operation, function and use of electrical general test equipment;
7.4 Avionic General Test Equipment
      Operation, function and use of avionic general test equipment.
7.5 Engineering Drawings, Diagrams and Standards
      Drawing types and diagrams, their symbols, dimensions, tolerances and projections;
      Identifying title block information
      Microfilm, microfiche and computerised presentations;
      Specification 100 of the Air Transport Association (ATA) of America;
      Aeronautical and other applicable standards including
      ISO, AN, MS, NAS and MIL;
     Wiring diagrams and schematic diagrams.
7.6 Fits and Clearances
      Drill sizes for bolt holes, classes of fits;
      Common system of fits and clearances;
      Schedule of fits and clearances for aircraft and engines;
      Limits for bow, twist and wear;
      Standard methods for checking shafts, bearings and other parts.
7.7 Electrical Wiring Interconnection System (EWIS)
     Continuity, insulation and bonding techniques and testing;
     Use of crimp tools: hand and hydraulic operated;
     Testing of crimp joints;
     Connector pin removal and insertion;
     Co-axial cables: testing and installation precautions;
     Identification of wire types, their inspection criteria and damage tolerance.
     Wiring protection techniques: Cable looming and loom support, cable clamps,
     protective sleeving techniques including heat shrink wrapping, shielding.
     EWIS installations, inspection, repair, maintenance and cleanliness standards.
7.8 Riveting
      Riveted joints, rivet spacing and pitch;
      Tools used for riveting and dimpling;
      Inspection of riveted joints.
7.9 Pipes and Hoses
      Bending and belling/flaring aircraft pipes;
      Inspection and testing of aircraft pipes and hoses;
      Installation and clamping of pipes.
7.10 Springs
        Inspection and testing of springs.
7.11 Bearings
       Testing, cleaning and inspection of bearings;
       Lubrication requirements of bearings;
       Defects in bearings and their causes.
7.12 Transmissions
        Inspection of gears, backlash;
        Inspection of belts and pulleys, chains and sprockets;
        Inspection of screw jacks, lever devices, push-pull rod systems.
7.13 Control Cables
       Swaging of end fittings;
       Inspection and testing of control cables;
       Bowden cables; aircraft flexible control systems.
7.14 Material handling
7.14.1 Sheet Metal
           Marking out and calculation of bend allowance;
           Sheet metal working, including bending and forming;
           Inspection of sheet metal work.
7.14.2 Composite and non-metallic
           Bonding practices;
           Environmental conditions
           Inspection methods
7.15 Welding, Brazing, Soldering and Bonding
   (a) Soldering methods; inspection of soldered joints.
   (b) Welding and brazing methods;
         Inspection of welded and brazed joints;
         Bonding methods and inspection of bonded joints.
7.16 Aircraft Weight and Balance
  (a) Centre of Gravity/Balance limits calculation: use of relevant documents;
  (b) Preparation of aircraft for weighing;
        Aircraft weighing;
7.17 Aircraft Handling and Storage
        Aircraft taxiing/towing and associated safety precautions;
        Aircraft jacking, chocking, securing and associated safety precautions;
        Aircraft storage methods;
        Refuelling/defuelling procedures;
        De-icing/anti-icing procedures;
        Electrical, hydraulic and pneumatic ground supplies.
        Effects of environmental conditions on aircraft handling and operation.
7.18 Disassembly, Inspection, Repair and Assembly Techniques
  (a) Types of defects and visual inspection techniques.
        Corrosion removal, assessment and reprotection.
  (b) General repair methods, Structural Repair Manual;
        Ageing, fatigue and corrosion control programmes;
  (c) Non destructive inspection techniques including, penetrant, radiographic,
        eddy current, ultrasonic and boroscope methods.
  (d) Disassembly and re-assembly techniques.
(e) Trouble shooting techniques
7.19 Abnormal Events
   (a) Inspections following lightning strikes and HIRF penetration.
   (b) Inspections following abnormal events such as heavy
         landings and flight through turbulence. 
7.20 Maintenance Procedures
        Maintenance planning;
        Modification procedures;
        Stores procedures;
        Certification/release procedures;
        Interface with aircraft operation;
        Maintenance Inspection/Quality Control/Quality Assurance;
        Additional maintenance procedures.
        Control of life limited components

Module 5

MODULE 5. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS
5.1 Electronic Instrument Systems 
     Typical systems arrangements and cockpit layout of electronic instrument systems.

5.2 Numbering Systems
      Numbering systems: binary, octal and hexadecimal;
      Demonstration of conversions between the decimal and binary, octal and hexadecimal
       systems and  vice versa.

5.3 Data Conversion
      Analogue Data, Digital Data;
      Operation and application of analogue to digital, and digital to
       analogue converters, inputs and outputs, limitations of various types.

5.4 Data Buses
      Operation of data buses in aircraft systems, including knowledge of ARINC and other
       specifications.

5.5 Logic Circuits
 (a) Identification of common logic gate symbols, tables and equivalent circuits;
      Applications used for aircraft systems, schematic diagrams.
 (b)Interpretation of logic diagrams.

5.6 Basic Computer Structure
(a) Computer terminology (including bit, byte, software, hardware, CPU,
      IC, and various memory devices such as RAM, ROM, PROM);
      Computer technology (as applied in aircraft systems).
(b) Computer related terminology;
      Operation, layout and interface of the major components in a micro
       computer including their associated bus systems;
     Information contained in single and multi address instruction words;
     Memory associated terms;
     Operation of typical memory devices;
     Operation, advantages and disadvantages of the various data storage systems.

5.7 Microprocessors
      Functions performed and overall operation of a microprocessor;
      Basic operation of each of the following microprocessor elements:
       control and processing unit, clock, register, arithmetic logic unit.

5.8 Integrated Circuits
     Operation and use of encoders and decoders
     Function of encoder types
     Uses of medium, large and very large scale integration.

5.9 Multiplexing
      Operation, application and identification in logic diagrams of multiplexers and 
       demultiplexers.

5.10 Fibre Optics
        Advantages and disadvantages of fibre optic data transmission over electrical wire
          propagation;
         Fibre optic data bus;
         Fibre optic related terms;
         Terminations;
         Couplers, control terminals, remote terminals;
         Application of fibre optics in aircraft systems.

5.11 Electronic Displays
        Principles of operation of common types of displays used in modern aircraft, including
        Cathode Ray Tubes, Light Emitting Diodes and Liquid
        Crystal Display.

5.12 Electrostatic Sensitive Devices
       Special handling of components sensitive to electrostatic discharges;
       Awareness of risks and possible damage, component and personnel
       anti-static protection devices.

5.13 Software Management Control
        Awareness of restrictions, airworthiness requirements and possible
        catastrophic effects of unapproved changes to software programmes.

5.14 Electromagnetic Environment
        Influence of the following phenomena on maintenance practices for electronic system:
        EMC-Electromagnetic Compatibility
        EMI-Electromagnetic Interference
        HIRF-High Intensity Radiated Field
        Lightning/lightning protection

5.15 Typical Electronic/Digital Aircraft Systems
       General arrangement of typical electronic/digital aircraft systems and associated BITE 
       (Built In Test Equipment) testing such as:
  (a) For B1 and B2 only:
       ACARS-ARINC Communication and Addressing and Reporting System
       EICAS-Engine Indication and Crew Alerting System
       FBW-Fly by Wire
       FMS-Flight Management System IRS-Inertial reference system
 (b) For B1, B2 and B3:
       ECAM-Electronic Centralised Aircraft Monitoring EFIS-Electronic Flight Instrument
        System
       GPS-Global Positioning System
       TCAS-Traffic Collission Avoidance system Integrated modular Avionica
       Cabin System Information system


Module 7A

MODULE 7A. MAINTENANCE PRACTICES
Note: This module does not apply to category B3. Relevant subject matters for category
B3 are defined in module 7B.

7.1 Safety Precautions-Aircraft and Workshop
      Aspects of safe working practices including precautions to take when working
      with electricity, gases especially oxygen, oils and chemicals.
      Also, instruction in the remedial action to be taken in the event of a fire or
      another accident with one or more of these hazards including knowledge on
      extinguishing agents.

7.2 Workshop Practices
      Care of tools, control of tools, use of workshop materials;
      Dimensions, allowances and tolerances, standards of workmanship;
      Calibration of tools and equipment, calibration standards.

7.3 Tools
      Common hand tool types;
      Common power tool types;
      Operation and use of precision measuring tools;
      Lubrication equipment and methods.
      Operation, function and use of electrical general test equipment;


7.4 Avionic General Test Equipment
      Operation, function and use of avionic general test equipment.

7.5 Engineering Drawings, Diagrams and Standards
      Drawing types and diagrams, their symbols, dimensions, tolerances and projections;
      Identifying title block information
      Microfilm, microfiche and computerised presentations;
      Specification 100 of the Air Transport Association (ATA) of America;
      Aeronautical and other applicable standards including
      ISO, AN, MS, NAS and MIL;
      Wiring diagrams and schematic diagrams.

7.6 Fits and Clearances
      Drill sizes for bolt holes, classes of fits;
      Common system of fits and clearances;
      Schedule of fits and clearances for aircraft and engines;
      Limits for bow, twist and wear;
      Standard methods for checking shafts, bearings and other parts.

7.7 Electrical Wiring Interconnection System (EWIS)
      Continuity, insulation and bonding techniques and testing;
      Use of crimp tools: hand and hydraulic operated;
      Testing of crimp joints;
      Connector pin removal and insertion;
      Co-axial cables: testing and installation precautions;
      Identification of wire types, their inspection criteria and damage tolerance.
      Wiring protection techniques: Cable looming and loom  support, cable clamps, protective                      sleeving techniques including heat shrink wrapping, shielding.
     EWIS installations, inspection, repair, maintenance and cleanliness standards.

7.8 Riveting
      Riveted joints, rivet spacing and pitch;
      Tools used for riveting and dimpling;
       Inspection of riveted joints.

7.9 Pipes and Hoses
      Bending and belling/flaring aircraft pipes;
      Inspection and testing of aircraft pipes and hoses;
      Installation and clamping of pipes.

7.10 Springs
        Inspection and testing of springs.

7.11 Bearings
        Testing, cleaning and inspection of bearings;
        Lubrication requirements of bearings;
        Defects in bearings and their causes.

7.12 Transmissions
        Inspection of gears, backlash;
        Inspection of belts and pulleys, chains and sprockets;
        Inspection of screw jacks, lever devices, push-pull rod systems.

7.13 Control Cables
        Swaging of end fittings;
        Inspection and testing of control cables;
        Bowden cables; aircraft flexible control systems.

7.14 Material handling
7.14.1 Sheet Metal
          Marking out and calculation of bend allowance;
          Sheet metal working, including bending and forming;
          Inspection of sheet metal work.
7.14.2 Composite and non-metallic
          Bonding practices;
          Environmental conditions
          Inspection methods

7.15 Welding, Brazing, Soldering and Bonding
   (a) Soldering methods; inspection of soldered joints.
   (b) Welding and brazing methods;
         Inspection of welded and brazed joints;
         Bonding methods and inspection of bonded joints.

7.16 Aircraft Weight and Balance
  (a) Centre of Gravity/Balance limits calculation: use of relevant documents;
  (b) Preparation of aircraft for weighing;
       Aircraft weighing;

7.17 Aircraft Handling and Storage
        Aircraft taxiing/towing and associated safety precautions;
        Aircraft jacking, chocking, securing and associated safety precautions;
        Aircraft storage methods;
         Refuelling/defuelling procedures;
         De-icing/anti-icing procedures;
         Electrical, hydraulic and pneumatic ground supplies.
         Effects of environmental conditions on aircraft handling and operation.

7.18 Disassembly, Inspection, Repair and Assembly Techniques
  (a) Types of defects and visual inspection techniques.
       Corrosion removal, assessment and reprotection.
   (b) General repair methods, Structural Repair Manual;
        Ageing, fatigue and corrosion control programmes;
   (c) Non destructive inspection techniques including, penetrant, radiographic,
        eddy current, ultrasonic and boroscope methods.
   (d) Disassembly and re-assembly techniques.
   (e) Trouble shooting techniques

7.19 Abnormal Events
   (a) Inspections following lightning strikes and HIRF penetration.
   (b) Inspections following abnormal events such as heavy landings and
         flight through turbulence.

7.20 Maintenance Procedures
        Maintenance planning;
        Modification procedures;
        Stores procedures;
        Certification/release procedures;
        Interface with aircraft operation;
        Maintenance Inspection/Quality Control/Quality Assurance;
        Additional maintenance procedures.
        Control of life limited components


Module 6

MODULE 6. MATERIALS AND HARDWARE
6.1 Aircraft Materials — Ferrous
(a) Characteristics, properties and identification of common alloy steels used in aircraft;
Heat treatment and application of alloy steels;
(b) Testing of ferrous materials for hardness, tensile strength, fatigue strength and impact resistance.

6.2 Aircraft Materials — Non-Ferrous
(a) Characteristics, properties and identification of common non-ferrous materials used in aircraft;
Heat treatment and application of non-ferrous materials;
(b) Testing of non-ferrous material for hardness, tensile strength, fatigue strength and impact resistance.

6.3 Aircraft Materials - Composite and Non- Metallic
6.3.1 Composite and non-metallic other than wood and fabric
    (a) Characteristics, properties and identification of common composite and non- metallic                              materials,  other than wood, used in aircraft;
          Sealant and bonding agents.
   (b) The detection of defects/deterioration in composite and non-metallic material.
         Repair of composite and non-metallic material.
6.3.2 Wooden structures
         Construction methods of wooden airframe structures;
         Characteristics, properties and types of wood and glue used in aeroplanes;
         Preservation and maintenance of wooden structure;
         Types of defects in wood material and wooden structures;
         The detection of defects in wooden structure;
         Repair of wooden structure.
6.3.3 Fabric covering
        Characteristics, properties and types of fabrics used in aeroplanes;
        Inspections methods for fabric;
        Types of defects in fabric;
        Repair of fabric covering.

6.4 Corrosion
(a) Chemical fundamentals;
      Formation by, galvanic action process, microbiological, stress;
(b) Types of corrosion and their identification;
     Causes of corrosion;
     Material types, susceptibility to corrosion.

6.5 Fasteners
6.5.1 Screw threads
         Screw nomenclature;
         Thread forms, dimensions and tolerances for standard threads used in aircraft;
         Measuring screw threads;
6.5.2 Bolts, studs and screws
         Bolt types: specification, identification and marking of aircraft bolts,
          international standards;
       Nuts: self locking, anchor, standard types;
       Machine screws: aircraft specifications;
       Studs: types and uses, insertion and removal;
       Self tapping screws, dowels.
6.5.3 Locking devices
        Tab and spring washers, locking plates, split pins, palnuts, wire locking, quick
         release fasteners, keys, circlips, cotter pins.
6.5.4 Aircraft rivets
         Types of solid and blind rivets: specifications and identification, heat treatment.

6.6 Pipes and Unions
(a) Identification of, and types of rigid and flexible pipes and their connectors used
      in aircraft;
(b) Standard unions for aircraft hydraulic, fuel, oil, pneumatic and air system pipes.

6.7 Springs
      Types of springs, materials, characteristics and applications.

6.8 Bearings
      Purpose of bearings, loads, material, construction;
      Types of bearings and their application.

6.9 Transmissions
      Gear types and their application;
      Gear ratios, reduction and multiplication gear systems, driven and driving
        gears, idler gears, mesh patterns;
      Belts and pulleys, chains and sprockets.

6.10 Control Cables
       Types of cables;
       End fittings, turnbuckles and compensation devices;
       Pulleys and cable system components;
       Bowden cables; Aircraft flexible control systems.

6.11 Electrical Cables and Connectors
       Cable types, construction and characteristics;
       High tension and co-axial cables;
       Crimping; Connector types, pins, plugs, sockets, insulators, current and voltage rating, coupling,           identification codes.

Module 3

MODULE 3. ELECTRICAL FUNDAMENTALS
3.1 Electron Theory
    Structure and distribution of electrical charges within: atoms, molecules,
    ions, compounds; Molecular structure of conductors, semiconductors and insulators.

3.2 Static Electricity and Conduction
    Static electricity and distribution of electrostatic charges;
    Electrostatic laws of attraction and repulsion;
    Units of charge, Coulomb's Law;
    Conduction of electricity in solids, liquids, gases and a vacuum.

3.3 Electrical Terminology
    The following terms, their units and factors affecting them: potential
    difference, electromotive force, voltage, current, resistance, conductance,
    charge, conventional current flow, electron flow.

3.4 Generation of Electricity
    Production of electricity by the following methods: light, heat, friction,
    pressure, chemical action, magnetism and motion.

3.5 DC Sources of Electricity
    Construction and basic chemical action of: primary cells, secondary cells, 
    lead acid cells, nickel cadmium cells, other alkaline cells;
    Cells connected in series and parallel; Internal resistance and its effect on a battery;
    Construction, materials and operation of thermocouples;
    Operation of photo-cells.

3.6 DC Circuits
    Ohms Law, Kirchoff's Voltage and Current Laws;
    Calculations using the above laws to find resistance, voltage and current;
    Significance of the internal resistance of a supply.

3.7 Resistance/Resistor
    (a) Resistance and affecting factors;
    Specific resistance;
    Resistor colour code, values and tolerances, preferred values, wattage
    ratings;
    Resistors in series and parallel;
    Calculation of total resistance using series, parallel and series parallel combinations;
    Operation and use of potentiometers and rheostats;
    Operation of Wheatstone Bridge.
    (b) Positive and negative temperature coefficient conductance;
    Fixed resistors, stability, tolerance and limitations, methods of construction;
    Variable resistors, thermistors, voltage dependent resistors;
    Construction of potentiometers and rheostats;
    Construction of Wheatstone Bridge;

3.8 Power
    Power, work and energy (kinetic and potential);
    Dissipation of power by a resistor;
    Power formula;
    Calculations involving power, work and energy.

3.9 Capacitance/Capacitor
    Operation and function of a capacitor;
    Factors affecting capacitance area of plates, distance between plates, number of plates, dielectric
    and dielectric constant, working voltage, voltage rating;
    Capacitor types, construction and function;
    Capacitor colour coding;
    Calculations of capacitance and voltage in series and parallel circuits;
    Exponential charge and discharge of a capacitor, time constants;
    Testing of capacitors.

3.10 Magnetism
   (a) Theory of magnetism;
         Properties of a magnet
         Action of a magnet suspended in the Earth's magnetic field;
         Magnetisation and demagnetisation;
         Magnetic shielding;
         Various types of magnetic material;
         Electromagnets construction and principles of operation;
         Hand clasp rules to determine: magnetic field around current carrying conductor.
   (b) Magnetomotive force, field strength, magnetic flux density, permeability,
         hysteresis loop, retentivity, coercive force reluctance, saturation point, eddy currents;
         Precautions for care and storage of magnets.

3.11 Inductance/Inductor
        Faraday's Law; Action of inducing a voltage in a conductor moving in a magnetic field;
        Induction principles;
        Effects of the following on the magnitude of an induced voltage: magnetic field strength, rate of 
         change of flux, number of conductor turns;
        Mutual induction;
        The effect the rate of change of primary current and mutual inductance has on induced voltage;
        Factors affecting mutual inductance: number of turns in coil, physical size of coil, permeability
         of coil, position of coils with respect to each other;
        Lenz's Law and polarity determining rules; Back emf, self induction;
        Saturation point;
        Principle uses of inductors;

3.12 DC Motor/Generator Theory
        Basic motor and generator theory;
        Construction and purpose of components in DC generator;
        Operation of, and factors affecting output and direction of current flow in DC generators;
        Operation of, and factors affecting output power, torque, speed and direction of rotation of DC
          motors;
        Series wound, shunt wound and compound motors; Starter Generator construction.

3.13 AC Theory
       Sinusoidal waveform: phase, period, frequency, cycle;
       Instantaneous, average, root mean square, peak, peak to peak current values and calculations of 
        these values, in relation to voltage, current and power Triangular/Square waves;
        Single/3 phase principles.

3.14 Resistive (R), Capacitive (C) and Inductive (L) Circuits
       Phase relationship of voltage and current in L, C and R circuits, parallel, series and series
        parallel;
      Power dissipation in L, C and R circuits;
      Impedance, phase angle, power factor and current calculations; True power, apparent power and
       reactive power calculations.

3.15 Transformers
        Transformer construction principles and operation; Transformer losses and methods for 
          overcoming them;
       Transformer action under load and no-load conditions; Power transfer, efficiency, polarity 
         markings;
       Calculation of line and phase voltages and currents;
       Calculation of power in a three phase system;
       Primary and Secondary current, voltage, turns ratio, power, efficiency;
       Auto transformers.

3.16 Filters
       Operation, application and uses of the following filters: low pass, high pass, band pass, band 
         stop.

3.17 AC Generators
        Rotation of loop in a magnetic field and waveform produced;
        Operation and construction of revolving armature and revolving field type AC generators;
        Single phase, two phase and three phase alternators;
         Three phase star and delta connections advantages and uses;
         Permanent Magnet Generators.

3.18 AC Motors
        Construction, principles of operation and characteristics of: AC synchronous and induction                    motors both single and polyphase;
        Methods of speed control and direction of rotation;
         Methods of producing a rotating field: capacitor, inductor, shaded or split pole.

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