Course IV: Aircraft Composite Repair
Course Outline
- 1.0 Introduction (3.0 hrs.)
- 1.1 Difference between Metals and Composites (repairs to metal parts vs. repairs to composite parts)
- 1.2 CRC Composite Structures Awareness Video
- 1.3 Definitions, typical defect and damage types, and sources of damage
- 1.4 Potential for defects and damage in composite parts (ply collation, curing, adhesive bonding, machining, assembly, disassembly, handling, environment, impact, erosion, lightning strike, and during repair !)
- 1.5 Assessment of need for repair (no repair action, cosmetic or sealing repair, structural repair, repair not being economical)
- 1.6 Manufacturing assessment process
- 1.6.1 Process specifications (acceptance and rework criteria for minor defects)
- 1.6.2 Engineering review (repair of damage and major defects)
- 1.7 In-Service assessment process
- 1.7.1 Structural Repair Manual (SRM) (allowable damage and repair of most in-service damage incidents)
- 1.7.2 Original Equip. Manufacturer (OEM) (damages beyond the SRM as needed e.g. infrequently damaged parts, damages at joints)
- 1.8 Repair environments (Manufacturing: Composite Shop, Final Assembly, Flight Line. In-Service: Line Maintenance (at the gate), Line Maintenance (overnight), Base Maintenance, Composite Shop)
- 1.9 Design for Repairability
- 2.0 Inspection Techniques (3.0 hrs.)
- 2.1 Non-instrumented or low-skill inspection methods
- 2.2 Instrumented nondestructive test methods
- 2.3 Emergent nondestructive test technologies
- 2.4 Applicability of NDT methods vs. flaw type
- 2.5 Probability of Detection (POD)
- 2.6 In-service inspection vs. production inspection -- differences
- 2.7 Damage detection – methods used and rationale
- 2.8 Repair assessment – methods used and rationale
- 2.9 Test cases and examples
- 3.0 Basic Types of Repair and design criteria (4.0 hrs.)
- 3.1 Nonstructural Repairs
- 3.1.1 Sealing
- 3.1.2 Potting
- 3.1.3 Resin Injection
- 3.2 Structural Repairs
- 3.2.1 Bolted, external patches
- 3.2.2 Bolted, flush patches
- 3.2.3 Adhesively bonded, external patches
- 3.2.4 Adhesively bonded, flush patches
- 3.2.5 Wet lay-up, flush patches
- 3.2.6 Overlay repairs
- 3.2.7 Bolted and Bonded patches
- 3.4 Drivers that determine the type of repair
- 3.5 Repair Design considerations Criteria and Requirements
- 3.5.1 Allowable Damage Limits
- 3.5.2 External Bonded or Bolted Repairs
- 3.5.3 Scarf Repairs
- 3.5.4 Multiple Repairs
- 3.5.5 Aerodynamic Smoothness
- 3.5.6 Material Selection
- 3.5.7 Repair Classification
- 3.5.8 Repair Method Selection
- 3.6 SRM Repair Types
- 4.0 Repair Analysis and Validation (3.0 hrs.)
- 4.1 Shear stress distribution
- 4.2 Thermal influences
- 4.3 Stiffness match considerations
- 4.4 Damage Tolerance considerations
- 4.5 Strength and failure criteria
- 4.6 Adhesive joint analysis
- 4.7 Bolted repairs
- 4.8 Testing and Validation
- 4.8.1 Building Block approach
- 4.8.2 Testing
- 5.0 Bolted Repair Process (3.0 hrs.)
- 5.1 Geometric arrangement of the fastener pattern
- 5.2 Fastener type, material, head configuration, and shank diameter
- 5.3 Patch material, thickness, shape
- 5.4 Proper drilling procedures Hand Drilling through CFRP/Ti Issues/Concerns
- 5.5 Special considerations
- 5.6 Typical repair procedure
- 5.7 Examples of Bolted Repairs
- 5.8 Videos of Bolted Repair
- 6.0 Bonded Repair Process (4.5 hrs.)
- 6.1 Types (sandwich, external patch, scarf patch, step patch)
- 6.2 Removal of damage skin material
- 6.3 Removal of damaged core material
- 6.4 Typical Bonded Repair Procedures (1.5 hrs)
- 6.4.1 Wet Lay-up Repair Procedure
- 6.4.2 Pre-impregnated Repair Procedure
- 6.4.3 Add in other SRM Chapter 51 procedures
- 6.5 Examples of Bonded Repairs
- 6.6 Videos of Bonded Repairs
- 6.7 Role of pressure and heat
- 6.8 Effects of moisture on bonded repair
- 6.9 Thermal Considerations
- 6.10 Post-repair inspection
- 7.0 Bonded and Bolted repairs (1.5 hrs.)
- 7.1 Load sharing
- 7.2 Alternate load paths
- 7.3 Through thickness reinforcement/peel stress
- 7.4 Jigging and bonding advantages
- 8.0 Post-Repair Activities (3.0 hrs.)
- 8.1 Lightning and Electrostatic Protection Designs, Damage and Repair
- 8.1.1 Flame Spray
- 8.1.2 Aluminum and Copper Foil
- 8.1.3 Expanded oil Mesh
- 8.1.4 Diverter Strips
- 8.1.5 Picture Frames
- 8.1.6 Anti-Static and Conductive Coating
- 8.1.7 Damage at a Fastener and Surrounding Structure
- 8.1.8 Typical Lightning Strike Damage Scenarios
- 8.2 Repair Inspection and re-inspection
- 8.3 Analysis of Repair Deviations
- 9.0 Service History and Selected In-Service Issues (1.5 hrs.)
- 10.0 Heatcon Demo of Repair Techniques (3.0 hrs.)
Questions
If you have questions about this program, please call UW Educational Outreach Advising at 206-685-8936 in the greater Seattle area or 1-800-543-2320. If you have questions about registration for this program, please call the UW Educational Outreach Registration Department at 206-543-2310 or 1-800-543-2320.
For more information about Boeing initiatives in composites education,email Michael Richey, Boeing Learning Training and Development, Engineering & Operations Group.