Appendix C to AMC 20-22 - Curriculum and Lessons Plan

• ED Decision 2008/007/R found in: AMC-20 Amdt 21 - Airworthiness of Products, Parts and Appliances (Apr 2021)

Appendix C to AMC 20-22 – Curriculum and Lessons Plan ED Decision 2008/007/R Electrical Wiring Interconnection System Curriculum 1          OVERVIEW This training is targeted at each person who performs aeroplane maintenance, inspections, alterations or repairs on EWIS and/or structure. After training, the person is able to properly evaluate the EWIS and effectively use the manufacturers Chapter 20 Wiring System overhaul manual for that aeroplane. The training programme must include: wiring system condition, applicable repair schemes, wiring modifications and ancillary repairs to wiring systems and components. All of the training components are integrated to maintain wiring system quality and airworthiness of the aeroplane. 2          OBJECTIVES Depending on the modules taught, the person shows competency in the following skills: a.         Know or demonstrate the safe handling of aeroplane electrical systems, Line Replaceable Units (LRU), tooling, troubleshooting procedures, and electrical measurement. b.         Know or demonstrate the construction and navigation of the applicable aeroplane wiring system overhaul or wiring practices manual. c.         Know the different types of inspections, human factors in inspections, zonal areas and typical damages. d.         Know the contamination sources, materials, cleaning and protection procedures. e.         Know or demonstrate the correct identification of different wire types, their inspection criteria, and damage tolerance, repair and preventative maintenance procedures. f.          Know or demonstrate the procedures to identify, inspect and find the correct repair for typical types of connective devices found on the applicable aeroplane. g.         Demonstrate the procedures for replacement of all parts of typical types of connective devices found on the applicable aeroplane. 3          SCOPE The course is to be used by training providers for all maintenance persons at any stage in their careers. The person can be trained to the appropriate level using the applicable modules, depending on the person’s experience, work assignment and operator’s policy. MODULE A – GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICES: (1)       Safety practices (2)       ESDS device handling and protection (3)       Tools, special tools and equipment (4)       Verify calibration/certification of instruments, tools, and equipment (5)       Required wiring checks using the Troubleshooting Procedures and charts (6)       Measurement and troubleshooting using meters (7)       LRU replacement general practices MODULE B – WIRING PRACTICES DOCUMENTATION: (1)       Chapter 20 structure/overview (2)       Chapter 20 cross-reference index (3)       Chapter 20 important data and tables (4)       Wiring Diagram Manual (5)       Other documentation (as applicable) MODULE C – INSPECTION: (1)       Special inspections (2)       Criteria and standards (3)       Human factors in inspection (4)       Zonal areas of inspection (5)       Wiring system damage MODULE D – HOUSEKEEPING: (1)       Aeroplane external contamination sources (2)       Aeroplane internal contamination sources (3)       Other contamination sources (4)       Contamination protection planning (5)       Protection during aeroplane maintenance and repair (6)       Cleaning processes MODULE E – WIRE: (1)       Identification, type and construction (2)       Insulation qualities (3)       Inspection criteria and standards of wire and wire bundles (4)       Wire bundle installation practices (5)       Typical damage and areas found (aeroplane specific) (6)       Maintenance and repair procedures (7)       Sleeving (8)       Unused wires - termination and storage (9)       Electrical bonding and grounds MODULE F – CONNECTIVE DEVICES: (1)       General types and identification (2)       Cautions and protections (3)       Visual inspection procedures (4)       Typical damage found (5)       Repair procedures MODULE G – CONNECTIVE DEVICE REPAIR: (1)       Circular connectors (2)       Rectangular connectors (3)       Terminal blocks - modular (4)       Terminal blocks - non-modular (5)       Grounding modules (6)       Pressure seals MODULE A: GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICE 1          OVERVIEW Through Module A, the instructor lays the groundwork of safe, effective maintenance and repair of the aeroplane EWIS and LRU removal and replacement, including BITE test, without damage to the aeroplane or injury to the student. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the student is able to demonstrate the following skills: a.         Know the safety procedures of normal and non-normal maintenance procedures so that the person can protect himself/herself and the aeroplane. b.         Recognise ESDS equipment and demonstrate standard anti-static procedures so that no damage occurs to that equipment. c.         Demonstrate the correct use of hand tools including specialised and automated tools and equipment. d.         Verify the calibration of electrical measuring instruments, tools and equipment so that correct maintenance procedures may be carried out. e.         Demonstrate the process and procedures to successfully use the troubleshooting procedures and charts of current aeroplane faults and know re-occurring problems causing “No Fault Found” on removed LRU. f.          Demonstrate the correct use of electrical meters for measuring voltage, current, resistance, continuity, insulation and short to ground. g.         Know the removal and replacement techniques so that no damage will occur to the LRU or aeroplane connector. 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. The following strategies can be used to expedite learning and are recommended to the instructor: <table border="1" cellpadding="0" cellspacing="0" width="566"> <tr> <td valign="top" width="379"> <p>ESDS handling and protection</p> </td> <td valign="top" width="188"> <p>Multimedia/training aids</p> </td> </tr> <tr> <td valign="top" width="379"> <p>Calibration/certification of instruments, tools, and equipment</p> </td> <td valign="top" width="188"> <p>Company policy</p> </td> </tr> <tr> <td valign="top" width="379"> <p>Wiring checks using the Troubleshooting Procedures and charts</p> </td> <td valign="top" width="188"> <p>Aeroplane manuals</p> </td> </tr> <tr> <td valign="top" width="379"> <p>Measurement and troubleshooting using meters</p> </td> <td valign="top" width="188"> <p>Meters and circuits</p> </td> </tr> <tr> <td valign="top" width="379"> <p>LRU removal and replacement</p> </td> <td valign="top" width="188"> <p>Aeroplane manuals</p> </td> </tr> </table> MODULE A – GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICES: 1          Safety Practices a.         Current is lethal - First aid b.         Applying power to the aeroplane c.         Isolating the circuit d.         Aeroplane warnings e.         Human factors 2          ESDS Device Handling and Protection a.         Sources of electrostatic discharge b.         Soft and hard failures c.         ESDS safety procedures d.         ESDS handling/packing procedures 3          Tools, Special Tools and Equipment a.         General hand tools b.         Specialised tools c.         Automated tools and equipment 4          Verify Calibration/Certification of Instruments, Tools and Equipment a.         Tools requiring certification b.         Determining certification requirements c.         Typical problems 5          Required Wiring Checks Using the Troubleshooting Procedures and charts a.         Troubleshooting procedures manual (all chapters) b.         Aeroplane Maintenance Manual/Illustrated Parts Catalogue c.         Wiring schematics/troubleshooting graphics d.         Wiring diagrams e.         The process of troubleshooting f.          Testing of LRU connectors g.         Troubleshooting exercises h.         Company “No Fault Found” policy and data 6          Measurement and Troubleshooting Using Meters a.         Voltage, current and resistance b.         Continuity c.         Insulation d.         Short to ground e.         Loop impedance 7          LRU Replacement - General Practices a.         Different retention devices b.         Certification considerations (e.g. CAT 2/CAT3 Landing) c.         LRU re-racking procedures d.         “No Fault Found” data (aeroplane specific) e.         Built-in test equipment (BITE) MODULE B: WIRING PRACTICES DOCUMENTATION 1          OVERVIEW Through Module B, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane EWIS. The intent of this module is to teach the person how to locate desired information in the Chapter 20 Wiring System overhaul manual, Wiring Diagram Manual and other applicable documentation. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Know the applicable Sub-Chapters and Section to follow during normal and non-normal electrical maintenance procedures. b.         Demonstrate the use of the Cross-Reference Index, Chapter Table of Contents, and Subject Tables of Contents so as to find specific material within each Sub-Chapter and Section. c.         Demonstrate the use of the associated tables for replacement of wire, connective devices and contacts, and associated components, including approved replacements. d.         Demonstrate the use of the Wiring Diagram Manual. e.         Demonstrate the use of other documentation (as applicable). 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. The Chapter 20 Wiring Practices Manual, Wiring Diagram Manual, and other applicable documentation should be made available to the class so that hands-on exploration of the material can be achieved. MODULE B – WIRING PRACTICES DOCUMENTATION: 1          Chapter 20 Structure/Overview a.         Table of contents b.         Sub-chapter titles c.         Section structure d.         General procedures 2          Chapter 20 Cross-Reference Index a.         Cross-reference index – Alphanumeric b.         Cross-reference index – Standard Part number c.         Cross-reference index – Suppliers e.         Equivalence tables – Std Part Numbers EN-ASN-NSA 3          Chapter 20 Important Data and Tables a.         Contact crimp tools, insertion/extraction tools b.         Wire Insulation removal tools c.         Electrical cable binding d.         Wire type codes and part numbers identification e.         Connective devices types and contacts f.          Terminal blocks and terminations g.         Terminal blocks modules, grounding modules and contacts h.         Cleaning procedures i.          Repair procedures 4          Wiring Diagram Manual (WDM) a.         Front matter b.         Diagrams c.         Charts d.         Lists 5          Other documentation (as applicable) MODULE C: INSPECTION 1          OVERVIEW Through Module C, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane wiring systems, by teaching the skills of inspection so as to identify wiring system damage. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Know the different types of inspections: General Visual Inspection (GVI), Detailed Inspection (DET), Zonal Inspection and Enhanced Zonal Analysis Procedure (EZAP). b.         Know the criteria and standards of inspection so that the person knows which tools are used to ensure inspection procedures and standards are achieved, which leads to all defects being found. c.         Know the effects of fatigue and complacency during inspection and how to combat these effects (Human Factors). d.         Know the specific zonal inspection requirements related to system affiliation and environmental conditions. e.         Recognise typical wiring system damage, such as hot gas, fluid contamination, external mechanically induced damage, chafing, corrosion, signs of overheating of wire, wire bundles, connective and control device assemblies. 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. ATA 117 video and colour photos of actual wiring system damage could be used to show typical problems found on the aeroplane. Examples of discrepancies should be made available to the student. [AMC 20-21](#_DxCrossRefBm421436843), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE C – INSPECTION 1.         Special Inspections a.         General Visual Inspection (GVI) b.         Detailed Inspection (DET) c.         Zonal Inspection d.         Enhanced Zonal Analysis Procedure (EZAP) 2.         Criteria and Standards a.         Tools b.         Criteria/standards c.         Procedures of inspection 3.         Human Factors in Inspection a.         Fatigue b.         Complacency 4.         Zonal Areas of Inspection a.         Zonal areas of inspection b.         Zonal inspection procedures and standards 5.         Wiring System Damage a.         Swarf/FOD/metal shavings b.         External mechanically induced damage c.         Hot gas d.         Fluid contamination e.         Vibration/chafing f.          Corrosion g.         Signs of overheating MODULE D: HOUSEKEEPING 1          OVERVIEW Through Module D, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane EWIS, by teaching housekeeping strategies, so as to keep the EWIS free of contamination. The Instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Recognise external contamination and other damage due to external environmental conditions. b.         Know the aeroplane internal contamination sources so that inspection processes can be effectively carried out and contamination damage easily recognised. c.         Recognise other possible contamination sources. d.         Know the planning procedures to be followed, on EWIS areas in different parts of the aeroplane. e.         Know the protection procedures and processes to protect the EWIS during maintenance and repair. f.          Know the process of cleaning wiring systems during maintenance and repair. 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. ATA 117 video and colour photos of actual EWIS contamination could be used to show typical problems found on the aeroplane. Relevant Aeroplane Maintenance Manual and/or Chapter 20 Wiring Practices procedures should be used. The ATSRAC Task Group 1, Non-Intrusive Inspection Final Report could be used to identify typical housekeeping issues. [AMC 20-21](#_DxCrossRefBm421436843), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE D – HOUSEKEEPING 1          Aeroplane External Contamination Sources a.         De-ice fluids b.         Water and rain c.         Snow and ice d.         Miscellaneous (e.g. cargo/beverage spillage) e.         Air erosion 2          Aeroplane Internal Contamination Sources a.         Hydraulic oils b.         Engine and APU oils c.         Fuel d.         Greases e.         Galleys and toilets f.          Lint/Dust g.         Bleed air and hot areas h.         Hazardous materials 3          Other Contamination Sources a.         Paint b.         Corrosion inhibitor c.         Drill shavings/Swarf d.         Foreign objects (screws, washers, rivets, tools, etc.) e.         Animal waste 4          Contamination Protection Planning a.         Have a plan/types of plan/area mapping b.         Protection and Caution Recommendations c.         Procedures d.         Keep cleaning 5          Protection during Aeroplane Maintenance and Repair a.         Recommended general maintenance protection procedures b.         Recommended airframe repair protection procedures c.         Recommended powerplant repair protection procedures 6          Cleaning Processes a.         Fluid contamination (1)       Snow and ice (2)       De-ice fluid (3)       Cargo spillage (4)       Water and rain (5)       Galleys (6)       Toilets water waste (7)       Oils and greases (8)       Pressure washing b.         Solid contamination (1)       Drill shavings/Swarf (2)       Foreign objects (screws, washers, rivets, tools, etc.) c.         Environmental contamination (1)       Lint and dust (2)       Paint (3)       Corrosion inhibitor (4)       Animal waste MODULE E: WIRE 1          OVERVIEW Through Module E, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS by teaching wire selection and inspection strategies. The Instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Demonstrate the procedure used to identify specific wire types using the aeroplane manuals. b.         Know from approved data different insulation types and their relative qualities. c.         Know the inspection criteria for wire and wire bundles. d.         Know the standard installation practices for wire and wire bundles (aeroplane specific). e.         Know typical damage that can be found (aeroplane specific). f.          Demonstrate the repair procedures for typical damage found on the student’s type of aeroplane. g.         Demonstrate the procedures to fitting differing types of sleeving (aeroplane specific). h.         Know the procedures for termination and storage of unused wires. i.          Know the correct installation practices for electrical bonds and grounds (aeroplane specific). 3          STRATEGIES Normal classroom lecture can be used for the majority of the training with hands-on practice for Section 6. Chapter 20 Wiring Practices, Wiring Diagram Manual and WDM Lists should be made available to the class to ensure hands-on use of the manual so that wire identification, inspection, installation and repair procedures can be fully explored. Examples of wire discrepancies should be made available to the student. The ATSRAC Task Group 1, Intrusive Inspection Final Report could be used to identify typical wire issues. [AMC 20-21](#_DxCrossRefBm421436843), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE E – WIRE 1          Identification, Type and Construction a.         Wire type codes – alphanumeric b.         Wire type codes – specification and standard part number c.         Wire type codes – specified wire and alternate d.         Manufacturer identification 2          Insulation Qualities a.         Types of insulation b.         Typical insulation damage and limitations c.         Carbon arcing 3          Inspection Criteria and Standards of Wire and Wire Bundles a.         Inspection of individual wiring b.         Inspection of wire bundles 4          Wire Bundle Installation Practices a.         Routing b.         Segregation rules c.         Clearance d.         Clamp inspection e.         Clamp removal and fitting f.          Conduit types and fitting g.         Raceways h.         Heat shields and drip shields 5          Typical Damage and Areas Found (aeroplane specific) a.         Vibration b.         Heat c.         Corrosion d.         Contamination e.         Personnel traffic passage 6          Maintenance and Repair Procedures a.         Wire damage assessment and classification b.         Approved repairs - improper repairs c.         Shielded wire repair d.         Repair techniques e.         Terminals and splices f.          Preventative maintenance procedures 7          Sleeving a.         Identification sleeves b.         Shrink sleeves c.         Screen braid grounding crimp sleeves d.         Screen braid grounding solder sleeves 8          Unused Wires - Termination and Storage a.         Termination – end caps b.         Storage and attachment 9          Electrical Bonding and Grounds a.         Inspection standards b.         Primary Bonding (HIRF protection) c.         Secondary Bonding (System grounding) d.         Lightning strikes MODULE F: CONNECTIVE DEVICES 1          OVERVIEW Through Module F, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS by teaching the identification, inspection and repair of connective devices found on the aeroplane. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Know the general types and positive identification of connective devices (aeroplane specific). b.         Know the various safety procedures, cautions and warnings prior to inspection. c.         Know the relevant visual inspection procedures for each type of connector so that any internal or external damage can be found. d.         Recognise typical external and internal damage to the connector. e.         Demonstrate where to find the relevant repair schemes from Chapter 20 for connector repair. 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. The Chapter 20 Wiring Practices manual should be made available to the class so that hands-on use of the manual can be ensured. Connector identification, inspection and repair procedures should be fully explored. Colour photographs of typical external damage and internal damage could be used to show problems on the aeroplane. The ATSRAC Task Group 1, Non-Intrusive Inspection and Intrusive Inspection Final Report, Chapter 7, could be used to identify typical connector issues. [AMC 20-21](#_DxCrossRefBm421436843), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE F – CONNECTIVE DEVICES 1          General Types and Identification a.         Part number identification b.         Reference tables c.         Specific connective devices chapters 2          Cautions and Protections a.         Safety precautions b.         Maintenance precautions 3          Visual Inspection Procedures a.         Installed inspection criteria b.         Removed inspection criteria 4          Typical Damage Found a.         Exterior damage b.         Internal damage 5          Repair Procedures a.         Finding the correct section b.         Finding the correct part c.         Finding the correct tooling d.         Confirming the correct repair MODULE G: CONNECTIVE DEVICES REPAIR 1          OVERVIEW Through Module G, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS. This module is primarily a hands-on class, emphasising the repair and replacement of connective devices found on the aeroplane. This list can be used to cover typical connectors for aeroplanes and can be adjusted to suit training requirements. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVE After this module is complete, the person will have the following skills: a.         Demonstrate the replacement of components for circular connectors. b.         Demonstrate the replacement of components for rectangular connectors. c.         Demonstrate the replacement of components for terminal blocks - modular. d.         Demonstrate the replacement of components for terminal blocks - non-modular. e.         Demonstrate the replacement of components for grounding modules. f.          Demonstrate the replacement of pressure seals. 3          STRATEGIES This class is primarily a hands-on class to give the student motor skills in the repair of connective devices from their aeroplane. The Chapter 20 Wiring Practices Manual and the appropriate connective devices should be made available to the class so that repair procedures can be fully explored. Photographs of typical internal conditions and external damage could be made available. It is recommended that MODULE F: CONNECTORS should precede this module. [AMC 20-21](#_DxCrossRefBm421436843), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE G – CONNECTIVE DEVICES REPAIR 1          Circular Connectors a.         Disassembly b.         Back-shell maintenance c.         Contact extraction and insertion d.         Contact crimping e.         Assembly and strain relief 2          Rectangular Connectors a.         Disassembly b.         Back-shell maintenance c.         Contact extraction and insertion d.         Contact Crimping e.         Assembly and strain relief 3          Terminal Blocks - Modular a.         Disassembly b.         Contact extraction and insertion c.         Contact Crimping d.         Assembly and strain relief 4          Terminal Block – Non-modular a.         Disassembly b.         Terminal Lug Crimping c.         Terminal Lug Stacking d.         Assembly, torque and strain relief 5          Grounding Modules a.         Disassembly b.         Contact extraction and insertion c.         Contact Crimping d.         Assembly and strain relief 6          Pressure Seals a.         Disassembly b.         Maintenance c.         Assembly and strain relief [Amdt 20/4] Appendix C to AMC 20-22 – Curriculum and Lessons Plan ED Decision 2008/007/R Electrical Wiring Interconnection System Curriculum 1 OVERVIEW This training is targeted at each person who performs aeroplane maintenance, inspections, alterations or repairs on EWIS and/or structure. After training, the person is able to properly evaluate the EWIS and effectively use the manufacturers Chapter 20 Wiring System overhaul manual for that aeroplane. The training programme must include: wiring system condition, applicable repair schemes, wiring modifications and ancillary repairs to wiring systems and components. All of the training components are integrated to maintain wiring system quality and airworthiness of the aeroplane. 2 OBJECTIVES Depending on the modules taught, the person shows competency in the following skills: a. Know or demonstrate the safe handling of aeroplane electrical systems, Line Replaceable Units (LRU), tooling, troubleshooting procedures, and electrical measurement. b. Know or demonstrate the construction and navigation of the applicable aeroplane wiring system overhaul or wiring practices manual. c. Know the different types of inspections, human factors in inspections, zonal areas and typical damages. d. Know the contamination sources, materials, cleaning and protection procedures. e. Know or demonstrate the correct identification of different wire types, their inspection criteria, and damage tolerance, repair and preventative maintenance procedures. f. Know or demonstrate the procedures to identify, inspect and find the correct repair for typical types of connective devices found on the applicable aeroplane. g. Demonstrate the procedures for replacement of all parts of typical types of connective devices found on the applicable aeroplane. 3 SCOPE The course is to be used by training providers for all maintenance persons at any stage in their careers. The person can be trained to the appropriate level using the applicable modules, depending on the person’s experience, work assignment and operator’s policy. MODULE A – GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICES: (1) Safety practices (2) ESDS device handling and protection (3) Tools, special tools and equipment (4) Verify calibration/certification of instruments, tools, and equipment (5) Required wiring checks using the Troubleshooting Procedures and charts (6) Measurement and troubleshooting using meters (7) LRU replacement general practices MODULE B – WIRING PRACTICES DOCUMENTATION: (1) Chapter 20 structure/overview (2) Chapter 20 cross-reference index (3) Chapter 20 important data and tables (4) Wiring Diagram Manual (5) Other documentation (as applicable) MODULE C – INSPECTION: (1) Special inspections (2) Criteria and standards (3) Human factors in inspection (4) Zonal areas of inspection (5) Wiring system damage MODULE D – HOUSEKEEPING: (1) Aeroplane external contamination sources (2) Aeroplane internal contamination sources (3) Other contamination sources (4) Contamination protection planning (5) Protection during aeroplane maintenance and repair (6) Cleaning processes MODULE E – WIRE: (1) Identification, type and construction (2) Insulation qualities (3) Inspection criteria and standards of wire and wire bundles (4) Wire bundle installation practices (5) Typical damage and areas found (aeroplane specific) (6) Maintenance and repair procedures (7) Sleeving (8) Unused wires - termination and storage (9) Electrical bonding and grounds MODULE F – CONNECTIVE DEVICES: (1) General types and identification (2) Cautions and protections (3) Visual inspection procedures (4) Typical damage found (5) Repair procedures MODULE G – CONNECTIVE DEVICE REPAIR: (1) Circular connectors (2) Rectangular connectors (3) Terminal blocks - modular (4) Terminal blocks - non-modular (5) Grounding modules (6) Pressure seals MODULE A: GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICE 1 OVERVIEW Through Module A, the instructor lays the groundwork of safe, effective maintenance and repair of the aeroplane EWIS and LRU removal and replacement, including BITE test, without damage to the aeroplane or injury to the student. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2 OBJECTIVES After this module is complete, the student is able to demonstrate the following skills: a. Know the safety procedures of normal and non-normal maintenance procedures so that the person can protect himself/herself and the aeroplane. b. Recognise ESDS equipment and demonstrate standard anti-static procedures so that no damage occurs to that equipment. c. Demonstrate the correct use of hand tools including specialised and automated tools and equipment. d. Verify the calibration of electrical measuring instruments, tools and equipment so that correct maintenance procedures may be carried out. e. Demonstrate the process and procedures to successfully use the troubleshooting procedures and charts of current aeroplane faults and know re-occurring problems causing “No Fault Found” on removed LRU. f. Demonstrate the correct use of electrical meters for measuring voltage, current, resistance, continuity, insulation and short to ground. g. Know the removal and replacement techniques so that no damage will occur to the LRU or aeroplane connector. 3 STRATEGIES Normal classroom lecture can be used for the majority of the training. The following strategies can be used to expedite learning and are recommended to the instructor: <table border="1" cellpadding="0" cellspacing="0" width="566"><tr><td valign="top" width="379"><p>ESDS handling and protection</p></td><td valign="top" width="188"><p>Multimedia/training aids</p></td></tr><tr><td valign="top" width="379"><p>Calibration/certification of instruments, tools, and equipment</p></td><td valign="top" width="188"><p>Company policy</p></td></tr><tr><td valign="top" width="379"><p>Wiring checks using the Troubleshooting Procedures and charts</p></td><td valign="top" width="188"><p>Aeroplane manuals</p></td></tr><tr><td valign="top" width="379"><p>Measurement and troubleshooting using meters</p></td><td valign="top" width="188"><p>Meters and circuits</p></td></tr><tr><td valign="top" width="379"><p>LRU removal and replacement</p></td><td valign="top" width="188"><p>Aeroplane manuals</p></td></tr></table> MODULE A – GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICES: 1 Safety Practices a. Current is lethal - First aid b. Applying power to the aeroplane c. Isolating the circuit d. Aeroplane warnings e. Human factors 2 ESDS Device Handling and Protection a. Sources of electrostatic discharge b. Soft and hard failures c. ESDS safety procedures d. ESDS handling/packing procedures 3 Tools, Special Tools and Equipment a. General hand tools b. Specialised tools c. Automated tools and equipment 4 Verify Calibration/Certification of Instruments, Tools and Equipment a. Tools requiring certification b. Determining certification requirements c. Typical problems 5 Required Wiring Checks Using the Troubleshooting Procedures and charts a. Troubleshooting procedures manual (all chapters) b. Aeroplane Maintenance Manual/Illustrated Parts Catalogue c. Wiring schematics/troubleshooting graphics d. Wiring diagrams e. The process of troubleshooting f. Testing of LRU connectors g. Troubleshooting exercises h. Company “No Fault Found” policy and data 6 Measurement and Troubleshooting Using Meters a. Voltage, current and resistance b. Continuity c. Insulation d. Short to ground e. Loop impedance 7 LRU Replacement - General Practices a. Different retention devices b. Certification considerations (e.g. CAT 2/CAT3 Landing) c. LRU re-racking procedures d. “No Fault Found” data (aeroplane specific) e. Built-in test equipment (BITE) MODULE B: WIRING PRACTICES DOCUMENTATION 1 OVERVIEW Through Module B, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane EWIS. The intent of this module is to teach the person how to locate desired information in the Chapter 20 Wiring System overhaul manual, Wiring Diagram Manual and other applicable documentation. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2 OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a. Know the applicable Sub-Chapters and Section to follow during normal and non-normal electrical maintenance procedures. b. Demonstrate the use of the Cross-Reference Index, Chapter Table of Contents, and Subject Tables of Contents so as to find specific material within each Sub-Chapter and Section. c. Demonstrate the use of the associated tables for replacement of wire, connective devices and contacts, and associated components, including approved replacements. d. Demonstrate the use of the Wiring Diagram Manual. e. Demonstrate the use of other documentation (as applicable). 3 STRATEGIES Normal classroom lecture can be used for the majority of the training. The Chapter 20 Wiring Practices Manual, Wiring Diagram Manual, and other applicable documentation should be made available to the class so that hands-on exploration of the material can be achieved. MODULE B – WIRING PRACTICES DOCUMENTATION: 1 Chapter 20 Structure/Overview a. Table of contents b. Sub-chapter titles c. Section structure d. General procedures 2 Chapter 20 Cross-Reference Index a. Cross-reference index – Alphanumeric b. Cross-reference index – Standard Part number c. Cross-reference index – Suppliers e. Equivalence tables – Std Part Numbers EN-ASN-NSA 3 Chapter 20 Important Data and Tables a. Contact crimp tools, insertion/extraction tools b. Wire Insulation removal tools c. Electrical cable binding d. Wire type codes and part numbers identification e. Connective devices types and contacts f. Terminal blocks and terminations g. Terminal blocks modules, grounding modules and contacts h. Cleaning procedures i. Repair procedures 4 Wiring Diagram Manual (WDM) a. Front matter b. Diagrams c. Charts d. Lists 5 Other documentation (as applicable) MODULE C: INSPECTION 1 OVERVIEW Through Module C, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane wiring systems, by teaching the skills of inspection so as to identify wiring system damage. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2 OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a. Know the different types of inspections: General Visual Inspection (GVI), Detailed Inspection (DET), Zonal Inspection and Enhanced Zonal Analysis Procedure (EZAP). b. Know the criteria and standards of inspection so that the person knows which tools are used to ensure inspection procedures and standards are achieved, which leads to all defects being found. c. Know the effects of fatigue and complacency during inspection and how to combat these effects (Human Factors). d. Know the specific zonal inspection requirements related to system affiliation and environmental conditions. e. Recognise typical wiring system damage, such as hot gas, fluid contamination, external mechanically induced damage, chafing, corrosion, signs of overheating of wire, wire bundles, connective and control device assemblies. 3 STRATEGIES Normal classroom lecture can be used for the majority of the training. ATA 117 video and colour photos of actual wiring system damage could be used to show typical problems found on the aeroplane. Examples of discrepancies should be made available to the student. [AMC 20-21](#_DxCrossRefBm1701658037), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE C – INSPECTION 1. Special Inspections a. General Visual Inspection (GVI) b. Detailed Inspection (DET) c. Zonal Inspection d. Enhanced Zonal Analysis Procedure (EZAP) 2. Criteria and Standards a. Tools b. Criteria/standards c. Procedures of inspection 3. Human Factors in Inspection a. Fatigue b. Complacency 4. Zonal Areas of Inspection a. Zonal areas of inspection b. Zonal inspection procedures and standards 5. Wiring System Damage a. Swarf/FOD/metal shavings b. External mechanically induced damage c. Hot gas d. Fluid contamination e. Vibration/chafing f. Corrosion g. Signs of overheating MODULE D: HOUSEKEEPING 1 OVERVIEW Through Module D, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane EWIS, by teaching housekeeping strategies, so as to keep the EWIS free of contamination. The Instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2 OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a. Recognise external contamination and other damage due to external environmental conditions. b. Know the aeroplane internal contamination sources so that inspection processes can be effectively carried out and contamination damage easily recognised. c. Recognise other possible contamination sources. d. Know the planning procedures to be followed, on EWIS areas in different parts of the aeroplane. e. Know the protection procedures and processes to protect the EWIS during maintenance and repair. f. Know the process of cleaning wiring systems during maintenance and repair. 3 STRATEGIES Normal classroom lecture can be used for the majority of the training. ATA 117 video and colour photos of actual EWIS contamination could be used to show typical problems found on the aeroplane. Relevant Aeroplane Maintenance Manual and/or Chapter 20 Wiring Practices procedures should be used. The ATSRAC Task Group 1, Non-Intrusive Inspection Final Report could be used to identify typical housekeeping issues. [AMC 20-21](#_DxCrossRefBm1701658037), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE D – HOUSEKEEPING 1 Aeroplane External Contamination Sources a. De-ice fluids b. Water and rain c. Snow and ice d. Miscellaneous (e.g. cargo/beverage spillage) e. Air erosion 2 Aeroplane Internal Contamination Sources a. Hydraulic oils b. Engine and APU oils c. Fuel d. Greases e. Galleys and toilets f. Lint/Dust g. Bleed air and hot areas h. Hazardous materials 3 Other Contamination Sources a. Paint b. Corrosion inhibitor c. Drill shavings/Swarf d. Foreign objects (screws, washers, rivets, tools, etc.) e. Animal waste 4 Contamination Protection Planning a. Have a plan/types of plan/area mapping b. Protection and Caution Recommendations c. Procedures d. Keep cleaning 5 Protection during Aeroplane Maintenance and Repair a. Recommended general maintenance protection procedures b. Recommended airframe repair protection procedures c. Recommended powerplant repair protection procedures 6 Cleaning Processes a. Fluid contamination (1) Snow and ice (2) De-ice fluid (3) Cargo spillage (4) Water and rain (5) Galleys (6) Toilets water waste (7) Oils and greases (8) Pressure washing b. Solid contamination (1) Drill shavings/Swarf (2) Foreign objects (screws, washers, rivets, tools, etc.) c. Environmental contamination (1) Lint and dust (2) Paint (3) Corrosion inhibitor (4) Animal waste MODULE E: WIRE 1 OVERVIEW Through Module E, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS by teaching wire selection and inspection strategies. The Instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2 OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a. Demonstrate the procedure used to identify specific wire types using the aeroplane manuals. b. Know from approved data different insulation types and their relative qualities. c. Know the inspection criteria for wire and wire bundles. d. Know the standard installation practices for wire and wire bundles (aeroplane specific). e. Know typical damage that can be found (aeroplane specific). f. Demonstrate the repair procedures for typical damage found on the student’s type of aeroplane. g. Demonstrate the procedures to fitting differing types of sleeving (aeroplane specific). h. Know the procedures for termination and storage of unused wires. i. Know the correct installation practices for electrical bonds and grounds (aeroplane specific). 3 STRATEGIES Normal classroom lecture can be used for the majority of the training with hands-on practice for Section 6. Chapter 20 Wiring Practices, Wiring Diagram Manual and WDM Lists should be made available to the class to ensure hands-on use of the manual so that wire identification, inspection, installation and repair procedures can be fully explored. Examples of wire discrepancies should be made available to the student. The ATSRAC Task Group 1, Intrusive Inspection Final Report could be used to identify typical wire issues. [AMC 20-21](#_DxCrossRefBm1701658037), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE E – WIRE 1 Identification, Type and Construction a. Wire type codes – alphanumeric b. Wire type codes – specification and standard part number c. Wire type codes – specified wire and alternate d. Manufacturer identification 2 Insulation Qualities a. Types of insulation b. Typical insulation damage and limitations c. Carbon arcing 3 Inspection Criteria and Standards of Wire and Wire Bundles a. Inspection of individual wiring b. Inspection of wire bundles 4 Wire Bundle Installation Practices a. Routing b. Segregation rules c. Clearance d. Clamp inspection e. Clamp removal and fitting f. Conduit types and fitting g. Raceways h. Heat shields and drip shields 5 Typical Damage and Areas Found (aeroplane specific) a. Vibration b. Heat c. Corrosion d. Contamination e. Personnel traffic passage 6 Maintenance and Repair Procedures a. Wire damage assessment and classification b. Approved repairs - improper repairs c. Shielded wire repair d. Repair techniques e. Terminals and splices f. Preventative maintenance procedures 7 Sleeving a. Identification sleeves b. Shrink sleeves c. Screen braid grounding crimp sleeves d. Screen braid grounding solder sleeves 8 Unused Wires - Termination and Storage a. Termination – end caps b. Storage and attachment 9 Electrical Bonding and Grounds a. Inspection standards b. Primary Bonding (HIRF protection) c. Secondary Bonding (System grounding) d. Lightning strikes MODULE F: CONNECTIVE DEVICES 1 OVERVIEW Through Module F, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS by teaching the identification, inspection and repair of connective devices found on the aeroplane. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2 OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a. Know the general types and positive identification of connective devices (aeroplane specific). b. Know the various safety procedures, cautions and warnings prior to inspection. c. Know the relevant visual inspection procedures for each type of connector so that any internal or external damage can be found. d. Recognise typical external and internal damage to the connector. e. Demonstrate where to find the relevant repair schemes from Chapter 20 for connector repair. 3 STRATEGIES Normal classroom lecture can be used for the majority of the training. The Chapter 20 Wiring Practices manual should be made available to the class so that hands-on use of the manual can be ensured. Connector identification, inspection and repair procedures should be fully explored. Colour photographs of typical external damage and internal damage could be used to show problems on the aeroplane. The ATSRAC Task Group 1, Non-Intrusive Inspection and Intrusive Inspection Final Report, Chapter 7, could be used to identify typical connector issues. [AMC 20-21](#_DxCrossRefBm1701658037), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE F – CONNECTIVE DEVICES 1 General Types and Identification a. Part number identification b. Reference tables c. Specific connective devices chapters 2 Cautions and Protections a. Safety precautions b. Maintenance precautions 3 Visual Inspection Procedures a. Installed inspection criteria b. Removed inspection criteria 4 Typical Damage Found a. Exterior damage b. Internal damage 5 Repair Procedures a. Finding the correct section b. Finding the correct part c. Finding the correct tooling d. Confirming the correct repair MODULE G: CONNECTIVE DEVICES REPAIR 1 OVERVIEW Through Module G, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS. This module is primarily a hands-on class, emphasising the repair and replacement of connective devices found on the aeroplane. This list can be used to cover typical connectors for aeroplanes and can be adjusted to suit training requirements. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2 OBJECTIVE After this module is complete, the person will have the following skills: a. Demonstrate the replacement of components for circular connectors. b. Demonstrate the replacement of components for rectangular connectors. c. Demonstrate the replacement of components for terminal blocks - modular. d. Demonstrate the replacement of components for terminal blocks - non-modular. e. Demonstrate the replacement of components for grounding modules. f. Demonstrate the replacement of pressure seals. 3 STRATEGIES This class is primarily a hands-on class to give the student motor skills in the repair of connective devices from their aeroplane. The Chapter 20 Wiring Practices Manual and the appropriate connective devices should be made available to the class so that repair procedures can be fully explored. Photographs of typical internal conditions and external damage could be made available. It is recommended that MODULE F: CONNECTORS should precede this module. [AMC 20-21](#_DxCrossRefBm1701658037), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE G – CONNECTIVE DEVICES REPAIR 1 Circular Connectors a. Disassembly b. Back-shell maintenance c. Contact extraction and insertion d. Contact crimping e. Assembly and strain relief 2 Rectangular Connectors a. Disassembly b. Back-shell maintenance c. Contact extraction and insertion d. Contact Crimping e. Assembly and strain relief 3 Terminal Blocks - Modular a. Disassembly b. Contact extraction and insertion c. Contact Crimping d. Assembly and strain relief 4 Terminal Block – Non-modular a. Disassembly b. Terminal Lug Crimping c. Terminal Lug Stacking d. Assembly, torque and strain relief 5 Grounding Modules a. Disassembly b. Contact extraction and insertion c. Contact Crimping d. Assembly and strain relief 6 Pressure Seals a. Disassembly b. Maintenance c. Assembly and strain relief [Amdt 20/4] Appendix C to AMC 20-22 – Curriculum and Lessons Plan ED Decision 2008/007/R Electrical Wiring Interconnection System Curriculum 1          OVERVIEW This training is targeted at each person who performs aeroplane maintenance, inspections, alterations or repairs on EWIS and/or structure. After training, the person is able to properly evaluate the EWIS and effectively use the manufacturers Chapter 20 Wiring System overhaul manual for that aeroplane. The training programme must include: wiring system condition, applicable repair schemes, wiring modifications and ancillary repairs to wiring systems and components. All of the training components are integrated to maintain wiring system quality and airworthiness of the aeroplane. 2          OBJECTIVES Depending on the modules taught, the person shows competency in the following skills: a.         Know or demonstrate the safe handling of aeroplane electrical systems, Line Replaceable Units (LRU), tooling, troubleshooting procedures, and electrical measurement. b.         Know or demonstrate the construction and navigation of the applicable aeroplane wiring system overhaul or wiring practices manual. c.         Know the different types of inspections, human factors in inspections, zonal areas and typical damages. d.         Know the contamination sources, materials, cleaning and protection procedures. e.         Know or demonstrate the correct identification of different wire types, their inspection criteria, and damage tolerance, repair and preventative maintenance procedures. f.          Know or demonstrate the procedures to identify, inspect and find the correct repair for typical types of connective devices found on the applicable aeroplane. g.         Demonstrate the procedures for replacement of all parts of typical types of connective devices found on the applicable aeroplane. 3          SCOPE The course is to be used by training providers for all maintenance persons at any stage in their careers. The person can be trained to the appropriate level using the applicable modules, depending on the person’s experience, work assignment and operator’s policy. MODULE A – GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICES: (1)       Safety practices (2)       ESDS device handling and protection (3)       Tools, special tools and equipment (4)       Verify calibration/certification of instruments, tools, and equipment (5)       Required wiring checks using the Troubleshooting Procedures and charts (6)       Measurement and troubleshooting using meters (7)       LRU replacement general practices MODULE B – WIRING PRACTICES DOCUMENTATION: (1)       Chapter 20 structure/overview (2)       Chapter 20 cross-reference index (3)       Chapter 20 important data and tables (4)       Wiring Diagram Manual (5)       Other documentation (as applicable) MODULE C – INSPECTION: (1)       Special inspections (2)       Criteria and standards (3)       Human factors in inspection (4)       Zonal areas of inspection (5)       Wiring system damage MODULE D – HOUSEKEEPING: (1)       Aeroplane external contamination sources (2)       Aeroplane internal contamination sources (3)       Other contamination sources (4)       Contamination protection planning (5)       Protection during aeroplane maintenance and repair (6)       Cleaning processes MODULE E – WIRE: (1)       Identification, type and construction (2)       Insulation qualities (3)       Inspection criteria and standards of wire and wire bundles (4)       Wire bundle installation practices (5)       Typical damage and areas found (aeroplane specific) (6)       Maintenance and repair procedures (7)       Sleeving (8)       Unused wires - termination and storage (9)       Electrical bonding and grounds MODULE F – CONNECTIVE DEVICES: (1)       General types and identification (2)       Cautions and protections (3)       Visual inspection procedures (4)       Typical damage found (5)       Repair procedures MODULE G – CONNECTIVE DEVICE REPAIR: (1)       Circular connectors (2)       Rectangular connectors (3)       Terminal blocks - modular (4)       Terminal blocks - non-modular (5)       Grounding modules (6)       Pressure seals MODULE A: GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICE 1          OVERVIEW Through Module A, the instructor lays the groundwork of safe, effective maintenance and repair of the aeroplane EWIS and LRU removal and replacement, including BITE test, without damage to the aeroplane or injury to the student. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the student is able to demonstrate the following skills: a.         Know the safety procedures of normal and non-normal maintenance procedures so that the person can protect himself/herself and the aeroplane. b.         Recognise ESDS equipment and demonstrate standard anti-static procedures so that no damage occurs to that equipment. c.         Demonstrate the correct use of hand tools including specialised and automated tools and equipment. d.         Verify the calibration of electrical measuring instruments, tools and equipment so that correct maintenance procedures may be carried out. e.         Demonstrate the process and procedures to successfully use the troubleshooting procedures and charts of current aeroplane faults and know re-occurring problems causing “No Fault Found” on removed LRU. f.          Demonstrate the correct use of electrical meters for measuring voltage, current, resistance, continuity, insulation and short to ground. g.         Know the removal and replacement techniques so that no damage will occur to the LRU or aeroplane connector. 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. The following strategies can be used to expedite learning and are recommended to the instructor: <table border="1" cellpadding="0" cellspacing="0" width="566"> <tr> <td valign="top" width="379"> <p>ESDS handling and protection</p> </td> <td valign="top" width="188"> <p>Multimedia/training aids</p> </td> </tr> <tr> <td valign="top" width="379"> <p>Calibration/certification of instruments, tools, and equipment</p> </td> <td valign="top" width="188"> <p>Company policy</p> </td> </tr> <tr> <td valign="top" width="379"> <p>Wiring checks using the Troubleshooting Procedures and charts</p> </td> <td valign="top" width="188"> <p>Aeroplane manuals</p> </td> </tr> <tr> <td valign="top" width="379"> <p>Measurement and troubleshooting using meters</p> </td> <td valign="top" width="188"> <p>Meters and circuits</p> </td> </tr> <tr> <td valign="top" width="379"> <p>LRU removal and replacement</p> </td> <td valign="top" width="188"> <p>Aeroplane manuals</p> </td> </tr> </table> MODULE A – GENERAL ELECTRICAL WIRING INTERCONNECTION SYSTEM PRACTICES: 1          Safety Practices a.         Current is lethal - First aid b.         Applying power to the aeroplane c.         Isolating the circuit d.         Aeroplane warnings e.         Human factors 2          ESDS Device Handling and Protection a.         Sources of electrostatic discharge b.         Soft and hard failures c.         ESDS safety procedures d.         ESDS handling/packing procedures 3          Tools, Special Tools and Equipment a.         General hand tools b.         Specialised tools c.         Automated tools and equipment 4          Verify Calibration/Certification of Instruments, Tools and Equipment a.         Tools requiring certification b.         Determining certification requirements c.         Typical problems 5          Required Wiring Checks Using the Troubleshooting Procedures and charts a.         Troubleshooting procedures manual (all chapters) b.         Aeroplane Maintenance Manual/Illustrated Parts Catalogue c.         Wiring schematics/troubleshooting graphics d.         Wiring diagrams e.         The process of troubleshooting f.          Testing of LRU connectors g.         Troubleshooting exercises h.         Company “No Fault Found” policy and data 6          Measurement and Troubleshooting Using Meters a.         Voltage, current and resistance b.         Continuity c.         Insulation d.         Short to ground e.         Loop impedance 7          LRU Replacement - General Practices a.         Different retention devices b.         Certification considerations (e.g. CAT 2/CAT3 Landing) c.         LRU re-racking procedures d.         “No Fault Found” data (aeroplane specific) e.         Built-in test equipment (BITE) MODULE B: WIRING PRACTICES DOCUMENTATION 1          OVERVIEW Through Module B, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane EWIS. The intent of this module is to teach the person how to locate desired information in the Chapter 20 Wiring System overhaul manual, Wiring Diagram Manual and other applicable documentation. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Know the applicable Sub-Chapters and Section to follow during normal and non-normal electrical maintenance procedures. b.         Demonstrate the use of the Cross-Reference Index, Chapter Table of Contents, and Subject Tables of Contents so as to find specific material within each Sub-Chapter and Section. c.         Demonstrate the use of the associated tables for replacement of wire, connective devices and contacts, and associated components, including approved replacements. d.         Demonstrate the use of the Wiring Diagram Manual. e.         Demonstrate the use of other documentation (as applicable). 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. The Chapter 20 Wiring Practices Manual, Wiring Diagram Manual, and other applicable documentation should be made available to the class so that hands-on exploration of the material can be achieved. MODULE B – WIRING PRACTICES DOCUMENTATION: 1          Chapter 20 Structure/Overview a.         Table of contents b.         Sub-chapter titles c.         Section structure d.         General procedures 2          Chapter 20 Cross-Reference Index a.         Cross-reference index – Alphanumeric b.         Cross-reference index – Standard Part number c.         Cross-reference index – Suppliers e.         Equivalence tables – Std Part Numbers EN-ASN-NSA 3          Chapter 20 Important Data and Tables a.         Contact crimp tools, insertion/extraction tools b.         Wire Insulation removal tools c.         Electrical cable binding d.         Wire type codes and part numbers identification e.         Connective devices types and contacts f.          Terminal blocks and terminations g.         Terminal blocks modules, grounding modules and contacts h.         Cleaning procedures i.          Repair procedures 4          Wiring Diagram Manual (WDM) a.         Front matter b.         Diagrams c.         Charts d.         Lists 5          Other documentation (as applicable) MODULE C: INSPECTION 1          OVERVIEW Through Module C, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane wiring systems, by teaching the skills of inspection so as to identify wiring system damage. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Know the different types of inspections: General Visual Inspection (GVI), Detailed Inspection (DET), Zonal Inspection and Enhanced Zonal Analysis Procedure (EZAP). b.         Know the criteria and standards of inspection so that the person knows which tools are used to ensure inspection procedures and standards are achieved, which leads to all defects being found. c.         Know the effects of fatigue and complacency during inspection and how to combat these effects (Human Factors). d.         Know the specific zonal inspection requirements related to system affiliation and environmental conditions. e.         Recognise typical wiring system damage, such as hot gas, fluid contamination, external mechanically induced damage, chafing, corrosion, signs of overheating of wire, wire bundles, connective and control device assemblies. 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. ATA 117 video and colour photos of actual wiring system damage could be used to show typical problems found on the aeroplane. Examples of discrepancies should be made available to the student. [AMC 20-21](#_DxCrossRefBm1926189281), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE C – INSPECTION 1.         Special Inspections a.         General Visual Inspection (GVI) b.         Detailed Inspection (DET) c.         Zonal Inspection d.         Enhanced Zonal Analysis Procedure (EZAP) 2.         Criteria and Standards a.         Tools b.         Criteria/standards c.         Procedures of inspection 3.         Human Factors in Inspection a.         Fatigue b.         Complacency 4.         Zonal Areas of Inspection a.         Zonal areas of inspection b.         Zonal inspection procedures and standards 5.         Wiring System Damage a.         Swarf/FOD/metal shavings b.         External mechanically induced damage c.         Hot gas d.         Fluid contamination e.         Vibration/chafing f.          Corrosion g.         Signs of overheating MODULE D: HOUSEKEEPING 1          OVERVIEW Through Module D, the instructor lays the groundwork for safe, effective maintenance and repair of aeroplane EWIS, by teaching housekeeping strategies, so as to keep the EWIS free of contamination. The Instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Recognise external contamination and other damage due to external environmental conditions. b.         Know the aeroplane internal contamination sources so that inspection processes can be effectively carried out and contamination damage easily recognised. c.         Recognise other possible contamination sources. d.         Know the planning procedures to be followed, on EWIS areas in different parts of the aeroplane. e.         Know the protection procedures and processes to protect the EWIS during maintenance and repair. f.          Know the process of cleaning wiring systems during maintenance and repair. 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. ATA 117 video and colour photos of actual EWIS contamination could be used to show typical problems found on the aeroplane. Relevant Aeroplane Maintenance Manual and/or Chapter 20 Wiring Practices procedures should be used. The ATSRAC Task Group 1, Non-Intrusive Inspection Final Report could be used to identify typical housekeeping issues. [AMC 20-21](#_DxCrossRefBm1926189281), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE D – HOUSEKEEPING 1          Aeroplane External Contamination Sources a.         De-ice fluids b.         Water and rain c.         Snow and ice d.         Miscellaneous (e.g. cargo/beverage spillage) e.         Air erosion 2          Aeroplane Internal Contamination Sources a.         Hydraulic oils b.         Engine and APU oils c.         Fuel d.         Greases e.         Galleys and toilets f.          Lint/Dust g.         Bleed air and hot areas h.         Hazardous materials 3          Other Contamination Sources a.         Paint b.         Corrosion inhibitor c.         Drill shavings/Swarf d.         Foreign objects (screws, washers, rivets, tools, etc.) e.         Animal waste 4          Contamination Protection Planning a.         Have a plan/types of plan/area mapping b.         Protection and Caution Recommendations c.         Procedures d.         Keep cleaning 5          Protection during Aeroplane Maintenance and Repair a.         Recommended general maintenance protection procedures b.         Recommended airframe repair protection procedures c.         Recommended powerplant repair protection procedures 6          Cleaning Processes a.         Fluid contamination (1)       Snow and ice (2)       De-ice fluid (3)       Cargo spillage (4)       Water and rain (5)       Galleys (6)       Toilets water waste (7)       Oils and greases (8)       Pressure washing b.         Solid contamination (1)       Drill shavings/Swarf (2)       Foreign objects (screws, washers, rivets, tools, etc.) c.         Environmental contamination (1)       Lint and dust (2)       Paint (3)       Corrosion inhibitor (4)       Animal waste MODULE E: WIRE 1          OVERVIEW Through Module E, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS by teaching wire selection and inspection strategies. The Instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Demonstrate the procedure used to identify specific wire types using the aeroplane manuals. b.         Know from approved data different insulation types and their relative qualities. c.         Know the inspection criteria for wire and wire bundles. d.         Know the standard installation practices for wire and wire bundles (aeroplane specific). e.         Know typical damage that can be found (aeroplane specific). f.          Demonstrate the repair procedures for typical damage found on the student’s type of aeroplane. g.         Demonstrate the procedures to fitting differing types of sleeving (aeroplane specific). h.         Know the procedures for termination and storage of unused wires. i.          Know the correct installation practices for electrical bonds and grounds (aeroplane specific). 3          STRATEGIES Normal classroom lecture can be used for the majority of the training with hands-on practice for Section 6. Chapter 20 Wiring Practices, Wiring Diagram Manual and WDM Lists should be made available to the class to ensure hands-on use of the manual so that wire identification, inspection, installation and repair procedures can be fully explored. Examples of wire discrepancies should be made available to the student. The ATSRAC Task Group 1, Intrusive Inspection Final Report could be used to identify typical wire issues. [AMC 20-21](#_DxCrossRefBm1926189281), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE E – WIRE 1          Identification, Type and Construction a.         Wire type codes – alphanumeric b.         Wire type codes – specification and standard part number c.         Wire type codes – specified wire and alternate d.         Manufacturer identification 2          Insulation Qualities a.         Types of insulation b.         Typical insulation damage and limitations c.         Carbon arcing 3          Inspection Criteria and Standards of Wire and Wire Bundles a.         Inspection of individual wiring b.         Inspection of wire bundles 4          Wire Bundle Installation Practices a.         Routing b.         Segregation rules c.         Clearance d.         Clamp inspection e.         Clamp removal and fitting f.          Conduit types and fitting g.         Raceways h.         Heat shields and drip shields 5          Typical Damage and Areas Found (aeroplane specific) a.         Vibration b.         Heat c.         Corrosion d.         Contamination e.         Personnel traffic passage 6          Maintenance and Repair Procedures a.         Wire damage assessment and classification b.         Approved repairs - improper repairs c.         Shielded wire repair d.         Repair techniques e.         Terminals and splices f.          Preventative maintenance procedures 7          Sleeving a.         Identification sleeves b.         Shrink sleeves c.         Screen braid grounding crimp sleeves d.         Screen braid grounding solder sleeves 8          Unused Wires - Termination and Storage a.         Termination – end caps b.         Storage and attachment 9          Electrical Bonding and Grounds a.         Inspection standards b.         Primary Bonding (HIRF protection) c.         Secondary Bonding (System grounding) d.         Lightning strikes MODULE F: CONNECTIVE DEVICES 1          OVERVIEW Through Module F, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS by teaching the identification, inspection and repair of connective devices found on the aeroplane. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVES After this module is complete, the person is able to demonstrate the following skills: a.         Know the general types and positive identification of connective devices (aeroplane specific). b.         Know the various safety procedures, cautions and warnings prior to inspection. c.         Know the relevant visual inspection procedures for each type of connector so that any internal or external damage can be found. d.         Recognise typical external and internal damage to the connector. e.         Demonstrate where to find the relevant repair schemes from Chapter 20 for connector repair. 3          STRATEGIES Normal classroom lecture can be used for the majority of the training. The Chapter 20 Wiring Practices manual should be made available to the class so that hands-on use of the manual can be ensured. Connector identification, inspection and repair procedures should be fully explored. Colour photographs of typical external damage and internal damage could be used to show problems on the aeroplane. The ATSRAC Task Group 1, Non-Intrusive Inspection and Intrusive Inspection Final Report, Chapter 7, could be used to identify typical connector issues. [AMC 20-21](#_DxCrossRefBm1926189281), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE F – CONNECTIVE DEVICES 1          General Types and Identification a.         Part number identification b.         Reference tables c.         Specific connective devices chapters 2          Cautions and Protections a.         Safety precautions b.         Maintenance precautions 3          Visual Inspection Procedures a.         Installed inspection criteria b.         Removed inspection criteria 4          Typical Damage Found a.         Exterior damage b.         Internal damage 5          Repair Procedures a.         Finding the correct section b.         Finding the correct part c.         Finding the correct tooling d.         Confirming the correct repair MODULE G: CONNECTIVE DEVICES REPAIR 1          OVERVIEW Through Module G, the instructor lays the groundwork for safe, effective maintenance, alteration and repair of aeroplane EWIS. This module is primarily a hands-on class, emphasising the repair and replacement of connective devices found on the aeroplane. This list can be used to cover typical connectors for aeroplanes and can be adjusted to suit training requirements. The instructor may vary the depth and scope of the topics to be covered, depending on the type of aeroplane to be maintained and skills of the persons. 2          OBJECTIVE After this module is complete, the person will have the following skills: a.         Demonstrate the replacement of components for circular connectors. b.         Demonstrate the replacement of components for rectangular connectors. c.         Demonstrate the replacement of components for terminal blocks - modular. d.         Demonstrate the replacement of components for terminal blocks - non-modular. e.         Demonstrate the replacement of components for grounding modules. f.          Demonstrate the replacement of pressure seals. 3          STRATEGIES This class is primarily a hands-on class to give the student motor skills in the repair of connective devices from their aeroplane. The Chapter 20 Wiring Practices Manual and the appropriate connective devices should be made available to the class so that repair procedures can be fully explored. Photographs of typical internal conditions and external damage could be made available. It is recommended that MODULE F: CONNECTORS should precede this module. [AMC 20-21](#_DxCrossRefBm1926189281), Programme to Enhance Aeroplane EWIS Maintenance is recommended as a source of typical aeroplane wiring installations and areas of concern. MODULE G – CONNECTIVE DEVICES REPAIR 1          Circular Connectors a.         Disassembly b.         Back-shell maintenance c.         Contact extraction and insertion d.         Contact crimping e.         Assembly and strain relief 2          Rectangular Connectors a.         Disassembly b.         Back-shell maintenance c.         Contact extraction and insertion d.         Contact Crimping e.         Assembly and strain relief 3          Terminal Blocks - Modular a.         Disassembly b.         Contact extraction and insertion c.         Contact Crimping d.         Assembly and strain relief 4          Terminal Block – Non-modular a.         Disassembly b.         Terminal Lug Crimping c.         Terminal Lug Stacking d.         Assembly, torque and strain relief 5          Grounding Modules a.         Disassembly b.         Contact extraction and insertion c.         Contact Crimping d.         Assembly and strain relief 6          Pressure Seals a.         Disassembly b.         Maintenance c.         Assembly and strain relief [Amdt 20/4]