DT&M Workshop Session: Bonded Repair (BR)

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Presentation transcript:

DT&M Workshop Session: Bonded Repair (BR) Mike Borgman Spirit AeroSystems, Inc. Wichita, KS, USA

Prologue Facts Reaction Meanwhile… ND bond strength validation methods do not exist Bond problems occasionally observed in service Reaction Must assume bond failure in sizing PSE repairs Essentially means non-OEM entities cannot define PSE repair Meanwhile… Shops with rigorous bond process controls have many repairs flying without incident Can we level performance of bond shops to mitigate reason for fear and doubt in bonding?

CTDT&M WS Bonded Repair (BR) Session Objective Garner industry input on BR state-of-practice Strategies to minimize occurrence of weak-bond? Is fleet knowledge transfer sufficient to prevent misuse of BR? Strategies to mitigate risk of insufficient PSE BR substantiation? Thoughts on current efforts and going-forward plans? Does the effort seem prudent or pointless?

CTDT&M WS Bonded Repair (BR) Session Objective Garner industry input on BR related topics What are best strategies to minimize weak-bond occurrences? Knowledge transfer and competency verification? Technician certifications? What is feasible? Service provider facilities certifications? Service provider management certifications? Right-process at right-time? Unification of BR materials, processes and practices? Other

BR Session Presentation Request (non-OEM) Objective it to explore the industry position on need for technician/engineer/management training and certification. WS discussion on the following subjects would be helpful. History of robust bonded repair performance with worker credentials Bonded repairs that performed poorly and had to be replaced Examples of MRO’s cutting corners to win work Performance issues associated with plethora of repair materials and non-harmonized work instruction Observed inconsistent BR performance and associated technician training and experience Other perspectives to help bring forward consensus on the need, or lack thereof, training/certifications

CTDT&M WS Agenda Bonded Repair Sessions 2015 FAA/Bombardier/TCCA/EASA/Industry Composite Transport Damage Tolerance and Maintenance Workshop 2015 FAA/Bombardier/TCCA/EASA/Industry Composite Transport Damage Tolerance and Maintenance Workshop Tuesday (September 15, 2015) Wednesday (September 16, 2015) Thursday (September 17, 2015) Regulatory Perspectives (FAA, EASA, TCCA) Session 3: High Energy, Wide Area, Blunt Impact (HEWABI) Session 6: Damage Tolerance (Special Subjects) 8:30-9:00 "Welcome/Introduction/Workshop Objectives" - Bombardier and Larry Ilcewicz (FAA) 8:30-8:50 "HEWABI as Related to Safety and Certification" - Larry Ilcewicz (FAA) "Composite Fatigue & Damage Tolerance Design & Service Experience" - Kevin Davis (Boeing) 9:00-9:30 "FAA Composite Plan" - Cindy Ashforth (FAA) 8:50-9:20 "UCSD FAA Research" - Hyonny Kim (UCSD) "Validation of Thermal Loads for Hybrid Structure" - Jean-Philippe (Bombardier) 9:30-10:00 "EASA Composite Safety Issues" - Simon Waite (EASA) 9:20-9:40 "EASA Research" - Simon Waite (EASA) 9:30-9:45 "Thermal Loads of Horizontal Tail Plane Structure" - Jan Waleson (Fokker) 10:00-10:30 "2015 Industry/Authorities FAA Composite Transport DT and Maintenance Workshop – TCCA Perspectives" - Maurizio Molinari (TCCA) 9:40-10:00 "Airline Experiences" - Eric Chesmar (United), Ray Kaiser (Delta) "Perspectives on Damage Detection and Inspection" - Larry Ilcewicz and Rusty Jones (FAA) 10:30-10:45 Break HEWABI Recap Session 10:00-10:15 Session 1: Sandwich Disbond Assessments 10:15-10:45 "Composite Damage Tolerance Speical Topics Recap" - Led by Larry Ilcewicz (FAA), D.M. Hoyt (NSE) and Waruna Seneviratne (WSU) 10:45-11:30 "CMH-17 Honeycomb Sandwich Disbond Growth Team Status - Mid 2015" - Ralf Hilgers (Airbus) and Ronald Krueger (NIA) Session 4A: Composite Fatigue and Damage Tolerance Session 7A: Smarter Damage Tolerance Testing 11:30-11:45 "Sandwich Disbond Recap" - Led by Larry Ilcewicz and Ralf Hilgers (Airbus) 10:45-11:00 "Introduction for Sessions 4 through 6" - Larry Ilcewicz (FAA) and D.M. Hoyt (NSE ) "Smarter DT Testing - Boeing Perspectives" - Kevin Davis (Boeing) Session 2A: Bonded Repair 2A (Part 1) 11:00-11:15 "Perspectives on Fatigue and Damage Tolerance Standardization" - Mark Nienhaus (Textron Aviation) "Smarter Testing - Airbus Approach" - J-l Leon Dufour, S. Rabois, and John van Doeselaar (Airbus) 11:45-12:00 "Sessions 2A and 2B - Introduction and Objectives" - Michael Borgman (Spirit AeroSystems, Inc.) 11:15-11:30 "TBD" -Reserved for ATR, Dassault or Gulfstream "Smart Testing - Bombardier Thoughts" - Salamon Haravan (Bombardier) 12:00-12:30 "Operator Field Experiences" - Eric Chesmar (UAL) 11:30-12:00 "Boeing Composite Fatigue & Damage Tolerance Certification Experiences" - Allen Fawcett (Boeing) "Smarter DT Testing - Summary" - Kevin Davis (Boeing) 12:30-1:15 Lunch "Airbus Composite Fatigue and Damage Tolerance Certification Experiences" - L. Ratier and C. Fualdes (Airbus) 11:45-12:30 Session 2A: Bonded Repair 2A (Part 2) Session 7B: Use of Probabilistic Methods 1:15-1:45 "Airbus Bonded Repair Applications to Pressurized Fuselage" - J. Charles and C. Fualdes (Airbus) Session 4B: Composite Fatigue and Damage Tolerance 12:30-1:30 Intro (J. van Doeselaar Airbus) 5 min Bombardier thoughts - Salamon Haravan- 10 min with Q&A Boeing thoughts - Alan Fawcett- 15 min with Q&A Airbus thoughts - Emilie Morteau; Chantal Fualdes- 15 min with Q&A WS participant experiences/closing remarks + Q&A (Airbus led) - 15 min 1:45-2:15 "Substantiation Approaches for Bonded Repairs" - Allen Fawcett (Boeing) "Rear Pressure Bulkhead Large Damage Capability Demonstration" Jean-Philippe Marouze (Bombardier) Session 2B: Bonded Repair 2B (Part 1) "Aviation Rulemaking Advisory Committee (ARAC) Tasking on § 25.571" - Walt Sippel (FAA) and Mike Gruber (Boeing) 2:15-2:45 "Lessons Learned from CACRC Depot Bonded Repair Round Robin Exercise" - Dr. John Tomblin & Lamia Salah (WSU) "NIAR Research on Certification of Composite-Metal Hybrid Structures" - Dr. Waruna Seneviratne and Dr. John Tomblin (WSU) Session 7C: Major Structural Modifications, Alterations & Repairs 2:45-3:15 "Effect of Processing Parameters on Bonded Repair Quality and Strength" Dr.Pascal Hubert (McGill Univ.); Dr.Rushabh Kothari, David Wilson, Geoff Walsh (Bombardier) "CMH-17 Durability & Damage Toleranc Roadmap" - D.M. Hoyt, Patrick Enjuto, and Tom Walker (NSE) 1:30-2:00 "Issues Associated with Modification and Repair of Primary Aircraft Composite Structures " - Steve Forness (Air Flight Technical) 3:15-3:30 2:00-2:30 "Examples of Substantiation Testing and Documents to Support Large Areas of Composite Repair" - John Welch, Jim Epperson (Spirit Aerosystems) Session 2B: Bonded Repair 2B (Part 2) Session 5: Damage Tolerance (Special Subjects) 2:30-2:45 3:30-4:00 "Bonded Repair Service Provider - Service History and Substantiation" - John Welch (Spirit Aero Systems) "The Aging Composite Airframe" - John Halpin (Consutant) 2:45-3:45 "Near-Term Emerging Technology Recap" - Led by Boeing (TBD), Airbus (TBD), Bombardier (TBD) and Cindy Ashforth (FAA) 4:00-4:30 "Composite Operational Issues" - Rusty Jones (FAA) and Simon Waite (EASA) "Some Thoughts on Strategies for Building Block Approach Development" - Eric Pomerleau and Dr. Isabelle Paris (Bombardier) 3:45-4:00 Recap/Actions/Closure - Larry Ilcewicz (FAA) 4:30-4:45 "Standards for Substantiation of Bonded Repairs" -Michael Borgman (Spirit Aero Systems) 4:30-5:30 "Composite Fatigue and Damage Tolerance Recap" - Led by Larry Ilcewicz (FAA), D.M. Hoyt (NSE) and Waruna Seneviratne (WSU) 4:45-5:45 "Bonded Repair Recap" - Led by Larry Ilcewicz & Rusty Jones (FAA) and Mike Borgman (Spirit) Tuesday (Sep. 15) Wednesday (Sep. 16) Thursday (Sep. 17)

CTDT&M WS: Bonded Repair Sessions 2015 FAA/Bombardier/TCCA/EASA/Industry Composite Transport Damage Tolerance and Maintenance Workshop 2015 FAA/Bombardier/TCCA/EASA/Industry Composite Transport Damage Tolerance and Maintenance Workshop Tuesday (September 15, 2015) Wednesday (September 16, 2015) Thursday (September 17, 2015) Regulatory Perspectives (FAA, EASA, TCCA) Session 3: High Energy, Wide Area, Blunt Impact (HEWABI) Session 6: Damage Tolerance (Special Subjects) 8:30-9:00 "Welcome/Introduction/Workshop Objectives" - Bombardier and Larry Ilcewicz (FAA) 8:30-8:50 "HEWABI as Related to Safety and Certification" - Larry Ilcewicz (FAA) "Composite Fatigue & Damage Tolerance Design & Service Experience" - Kevin Davis (Boeing) 9:00-9:30 "FAA Composite Plan" - Cindy Ashforth (FAA) 8:50-9:20 "UCSD FAA Research" - Hyonny Kim (UCSD) "Validation of Thermal Loads for Hybrid Structure" - Jean-Philippe (Bombardier) 9:30-10:00 "EASA Composite Safety Issues" - Simon Waite (EASA) 9:20-9:40 "EASA Research" - Simon Waite (EASA) 9:30-9:45 "Thermal Loads of Horizontal Tail Plane Structure" - Jan Waleson (Fokker) 10:00-10:30 "2015 Industry/Authorities FAA Composite Transport DT and Maintenance Workshop – TCCA Perspectives" - Maurizio Molinari (TCCA) 9:40-10:00 "Airline Experiences" - Eric Chesmar (United), Ray Kaiser (Delta) "Perspectives on Damage Detection and Inspection" - Larry Ilcewicz and Rusty Jones (FAA) 10:30-10:45 Break HEWABI Recap Session 10:00-10:15 Session 1: Sandwich Disbond Assessments 10:15-10:45 "Composite Damage Tolerance Speical Topics Recap" - Led by Larry Ilcewicz (FAA), D.M. Hoyt (NSE) and Waruna Seneviratne (WSU) 10:45-11:30 "CMH-17 Honeycomb Sandwich Disbond Growth Team Status - Mid 2015" - Ralf Hilgers (Airbus) and Ronald Krueger (NIA) Session 4A: Composite Fatigue and Damage Tolerance Session 7A: Smarter Damage Tolerance Testing 11:30-11:45 "Sandwich Disbond Recap" - Led by Larry Ilcewicz and Ralf Hilgers (Airbus) 10:45-11:00 "Introduction for Sessions 4 through 6" - Larry Ilcewicz (FAA) and D.M. Hoyt (NSE ) "Smarter DT Testing - Boeing Perspectives" - Kevin Davis (Boeing) Session 2A: Bonded Repair 2A (Part 1) 11:00-11:15 "Perspectives on Fatigue and Damage Tolerance Standardization" - Mark Nienhaus (Textron Aviation) "Smarter Testing - Airbus Approach" - J-l Leon Dufour, S. Rabois, and John van Doeselaar (Airbus) 11:45-12:00 "Sessions 2A and 2B - Introduction and Objectives" - Michael Borgman (Spirit AeroSystems, Inc.) 11:15-11:30 "TBD" -Reserved for ATR, Dassault or Gulfstream "Smart Testing - Bombardier Thoughts" - Salamon Haravan (Bombardier) 12:00-12:30 "Operator Field Experiences" - Eric Chesmar (UAL) 11:30-12:00 "Boeing Composite Fatigue & Damage Tolerance Certification Experiences" - Allen Fawcett (Boeing) "Smarter DT Testing - Summary" - Kevin Davis (Boeing) 12:30-1:15 Lunch "Airbus Composite Fatigue and Damage Tolerance Certification Experiences" - L. Ratier and C. Fualdes (Airbus) 11:45-12:30 Session 2A: Bonded Repair 2A (Part 2) Session 7B: Use of Probabilistic Methods 1:15-1:45 "Airbus Bonded Repair Applications to Pressurized Fuselage" - J. Charles and C. Fualdes (Airbus) Session 4B: Composite Fatigue and Damage Tolerance 12:30-1:30 Intro (J. van Doeselaar Airbus) 5 min Bombardier thoughts - Salamon Haravan- 10 min with Q&A Boeing thoughts - Alan Fawcett- 15 min with Q&A Airbus thoughts - Emilie Morteau; Chantal Fualdes- 15 min with Q&A WS participant experiences/closing remarks + Q&A (Airbus led) - 15 min 1:45-2:15 "Substantiation Approaches for Bonded Repairs" - Allen Fawcett (Boeing) "Rear Pressure Bulkhead Large Damage Capability Demonstration" Jean-Philippe Marouze (Bombardier) Session 2B: Bonded Repair 2B (Part 1) "Aviation Rulemaking Advisory Committee (ARAC) Tasking on § 25.571" - Walt Sippel (FAA) and Mike Gruber (Boeing) 2:15-2:45 "Lessons Learned from CACRC Depot Bonded Repair Round Robin Exercise" - Dr. John Tomblin & Lamia Salah (WSU) "NIAR Research on Certification of Composite-Metal Hybrid Structures" - Dr. Waruna Seneviratne and Dr. John Tomblin (WSU) Session 7C: Major Structural Modifications, Alterations & Repairs 2:45-3:15 "Effect of Processing Parameters on Bonded Repair Quality and Strength" Dr.Pascal Hubert (McGill Univ.); Dr.Rushabh Kothari, David Wilson, Geoff Walsh (Bombardier) "CMH-17 Durability & Damage Toleranc Roadmap" - D.M. Hoyt, Patrick Enjuto, and Tom Walker (NSE) 1:30-2:00 "Issues Associated with Modification and Repair of Primary Aircraft Composite Structures " - Steve Forness (Air Flight Technical) 3:15-3:30 2:00-2:30 "Examples of Substantiation Testing and Documents to Support Large Areas of Composite Repair" - John Welch, Jim Epperson (Spirit Aerosystems) Session 2B: Bonded Repair 2B (Part 2) Session 5: Damage Tolerance (Special Subjects) 2:30-2:45 3:30-4:00 "Bonded Repair Service Provider - Service History and Substantiation" - John Welch (Spirit Aero Systems) "The Aging Composite Airframe" - John Halpin (Consutant) 2:45-3:45 "Near-Term Emerging Technology Recap" - Led by Boeing (TBD), Airbus (TBD), Bombardier (TBD) and Cindy Ashforth (FAA) 4:00-4:30 "Composite Operational Issues" - Rusty Jones (FAA) and Simon Waite (EASA) "Some Thoughts on Strategies for Building Block Approach Development" - Eric Pomerleau and Dr. Isabelle Paris (Bombardier) 3:45-4:00 Recap/Actions/Closure - Larry Ilcewicz (FAA) 4:30-4:45 "Standards for Substantiation of Bonded Repairs" -Michael Borgman (Spirit Aero Systems) 4:30-5:30 "Composite Fatigue and Damage Tolerance Recap" - Led by Larry Ilcewicz (FAA), D.M. Hoyt (NSE) and Waruna Seneviratne (WSU) 4:45-5:45 "Bonded Repair Recap" - Led by Larry Ilcewicz & Rusty Jones (FAA) and Mike Borgman (Spirit) Tuesday (Sep. 15) Wednesday (Sep. 16) Thursday (Sep. 17)

First Speaker Eric Chesmar (UAL)