FAA Composite Plan and Associated Research Topics - Presented to AMTAS By Cindy Ashforth, FAA November 6, 2019
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FAA Composite Plan and Federal Aviation Administration Associated Research Topics Presented to AMTAS By Cindy Ashforth, FAA November 6, 2019
FY19 FAA Composite Plan Proposed List of Initiatives (as of 5/2019) Changes from last Continuous Operational Safety Certification Efficiency (CE) Workforce Education (WE) approved (COS) version in CE A: Fatigue & Damage Tolerance red COS A: Bonded Structure WE A: Workforce Training Substantiation WE B: Industry Training and COS B: Closed CE B: Closed International Outreach COS C: Failure Analysis of CE C: Composite Structural Composites Subjected to Fire Modifications Defines mitigating actions (Deliverables) for Document that summarizes CE D: Composite Quality Assurance the FAA - rulemaking, potential safety risks and policy, guidance, and opportunities for CE E: Bonded Structure Guidance training materials – and standardization (Initiatives) industry CE F: General Composite Structure associated with the use of Guidance composites in aviation products CE G: Engine Applications Guidance CE H: Composite TSO November 5, 2019 FAA Research Overview Federal Aviation 3 Administration
Continued Operational Safety (COS) Initiatives • Two COS items in the Composite Plan: A. Bonded Structure • Bonded repairs • Bond quality control • Sandwich disbond growth B. Closed • Was HEWABI (high energy wide area blunt impact), which is closed after release of a transport policy and internal webinar. Follow-on tasks for research and industry documentation are moved to initiative CE A for fatigue and damage tolerance. C. Failure analysis of composites subject to fire November 5, 2019 FAA Research Overview Federal Aviation 4 Administration
Being asked: Why duplicate COS Items work? Why can’t a standards group directly publish MOC COS A: Bonding content? Bonding safety Support CMH-17 to publish Volumes 1 and 3 Rev H with new content on bonding, Fall 2021 risks include (includes research funds) bonded repairs, Develop a Short Course for Bonded Repair Design, Substantiation, and Approval based on CMH- bondline 17, Fall 2022 durability* and sandwich disbond Create new AC or update AC 20-107B with additional bonding content, Draft Spring 2023 growth Support CMH-17 to publish Volume 6 Rev B with new content on sandwich structure, Spring 2023 *additional new (includes research funds) rotorcraft emphasis Create new AC or update AC 20-107B with additional sandwich content, Draft Spring 2024 COS C: Failure Analysis of Composites Subjected to Fire Can we determine if there Fund research FY19-FY22 was a structural failure after Publish update to Composite Failure Analysis Handbook (joint publication between the an accident and post- FAA and Air Force, last updated 1995) FY2023 impact fire? November 5, 2019 FAA Research Overview Federal Aviation 5 Administration
Research that Supports COS Initiatives • Moisture Diffusion in Sandwich Composites • Effect of Surface Contamination on Composite Bond Integrity and Durability Project • Durability of Adhesively Bonded Joints for Aircraft Structures Project • Durability of Bonded Aerospace Structures • Improving Adhesive Bonding of Composites Through Surface Characterization • Nanomechanical Characterization of Adhesive Bondlines November 5, 2019 FAA Research Overview Federal Aviation 6 Administration
Certification Efficiency Initiatives • Certification Efficiency (CE) initiatives capture best industry practices via regulatory guidance and industry standards documents. – Goal is to standardize methods to certify composite structures and repairs which will address the current industry practice of using proprietary databases and advanced procedures. • Seven CE initiatives A. Fatigue and Damage Tolerance Substantiation B. Closed • Was Advanced Composites Maintenance – the two deliverables are no longer supported by AFS C. Composite Structural Modification D. Composite Quality Control E. Bonded Structure Guidance F. General Composite Structures Guidance G. Engine Installation Guidance H. Material TSO • Additional standardization activities in the area of transport crashworthiness, fuel tank lightning protection, and composite flammability These FAA initiatives have some components specific to composites, but are not managed as part of the composite plan November 5, 2019 FAA Research Overview Federal Aviation 7 Administration
Can/Should all Certification Efficiency Items information go in an industry publication? CE A: Fatigue and Damage Tolerance F&DT engineering Policy on interpreting existing 25.571 amdt for composite structure, TBD (AIR-675 deliverable) protocols for composite Support 25.571 ARAC Report, due 12/2019 aircraft structures differ significantly from metal Revised 25.571 and associated guidance (may include AC 20-107B update), Draft 12/2020 engineering practices; Ongoing research to supplement documentation in CMH-17, FY19-FY23 hybrid structures an additional complexity CE C: Composite Modifications New applicants modifying critical Identify standards organization to publish portions of the content, 12/2019 composite structures, such as with Support standards organization to publish portion of the content already installation of antennas on 787 or A350 written for the AC, Date TBD aircraft. Safety risk with new applicants do not have experience in modifying critical Publish new AC on composite modifications that will summarize key points composite structure, and FAA offices have from industry publication highlighting what to worry about and why, Date requested guidance TBD to correlate with industry document November 5, 2019 FAA Research Overview Federal Aviation 8 Administration
Certification Efficiency Items CE D: Composite Quality Assurance Recent composite Research report on latest manufacturing techniques and associated key characteristics and manufacturing key process parameters, Draft summer 2019 techniques may not be Create an appendix in AC 21-43 with unique considerations for composite quality system able to utilize traditional oversight and cancel ACs 21-26 and 21-31, Draft winter 2020 quality control methods, Current QC ACs have Identify gaps in M&P guidance from canceling QC ACs and if so, develop plan to supplement type design information advanced M&P policy, AC 20-107 and/or industry standards (most likely CMH-17), Spring 2020 and 2x.605 MOC CE E: Structural Bonding – Same as COS A, but from a certification best practices / cert efficiency perspective CE F: General Composite Guidance With evolving/advancing composite Revise AC 20-107, “Composite Aircraft Structure,” to incorporate advanced technology and expanding composite technologies and lessons learned, draft Spring 2024 (timed to coincide composite applications, AC 20-107 with sandwich structure update under COS A / CE E) “Composite Aircraft Structure” • Will follow CMH-17 Volume 3 Rev H and Volume 6 Rev B requires revision • Will include latest lessons learned from research November 5, 2019 FAA Research Overview Federal Aviation 9 Administration
Certification Efficiency Items CE G: Engine Guidance Engine cert projects with Held CSTA workshop on engine applications and identify scope of engine AC, composites have been managed on September 2019 a case-by-case basis by adapting Write a new AC for composite engine applications, that refers to AC 20-107B, but AC 20-107B for composite aircraft puts in context of engine applications structure. Unique concerns with engines warrant individualized Engage engine industry with CMH-17 CMC and PMC coordination groups by guidance holding joint meeting summer 2020 November 5, 2019 FAA Research Overview Federal Aviation 10 Administration
Research that Supports CE Initiatives Failure of Notched Laminates Under Out-of-Plane Bending CE A Evaluation of Parameters Used in Progressive Damage Models CE A Development and Evaluation of Fracture Mechanics Test Methods for Sandwich CE A Composites - Damage Tolerance Test Method Development Moisture Diffusion in Sandwich Composites CE A Development of a Building Block Approach for Crashworthiness Testing N/A Effect of Surface Contamination on Composite Bond Integrity and Durability CE E Project Durability of Adhesively Bonded Joints for Aircraft Structures Project CE E Durability of Bonded Aerospace Structures CE E Improving Adhesive Bonding of Composites Through Surface Characterization CE E Nanomechanical Characterization of Adhesive Bondlines CE E Certification of Discontinuous Fiber Composite Material Forms for Aircraft CE F, CE D Structure November 5, 2019 FAA Research Overview Federal Aviation 11 Administration
New Certification Efficiency Items proposed initiative since 9/2018 CE H: Composite TSO New initiative for development of basic Hold workshop to gauge industry interest and identify a standards organization(s) to material data plus optional advanced work with, Winter 2019 material data and/or design tools. Allows Identify if any standards organization documentation is required, and scope working companies to demonstrate technology agreement(s), Spring 2020 readiness outside of a certification project. Draft Minimum Performance Standard, TSO, and associated guidance, Winter 2021 November 5, 2019 FAA Research Overview Federal Aviation 12 Administration
Why do we need a TSO? • Under the current system, we do not open certification projects for development of composite data • Some DAHs open projects to develop allowables and associated tools, then cancel the project – Data, however, is FAA approved and can be applied to other projects, when shown to be applicable • Other parties have no avenue to develop data that is approved by the FAA – Some basic material data may be generated under NCAMP system accepted by the FAA, but that ties applicants to one testing house – No higher-level data can be developed and accepted by the FAA (i.e., no conformity or witnessing without a project number) November 5, 2019 FAA Research Overview Federal Aviation 13 Administration
New TSO System • Parties could develop data that would be approved by the FAA without a certification project – The data would be restricted to a well-documented design space – Certification activities are still required in order to use the material and data – it has to be shown to be applicable to the project; however, the tests used to develop the data would not have to be re-performed with project numbers, conformity, and witnessing (this is managed under the TSOA quality system) – Brings parity to third parties so they can develop data in an economical method, the same as current DAHs • There would be a significant advantage to the FAA to receive data packages with the TSO application that describe the limitations of the data – a learning tool and design guide November 5, 2019 FAA Research Overview Federal Aviation 14 Administration
What is it? • We are considering developing a new TSO and associated guidance for composite materials – Guidance is essential in order to implement the TSO, since it is a new concept • Addresses multiple segments of the industry: – Material suppliers – Companies who want to develop data that they can get credit for, independent of an FAA certification project • Includes development of basic material data plus optional advanced material data and/or analytical tools November 5, 2019 FAA Research Overview Federal Aviation 15 Administration
Candidate TSO Content • There could be three classes of data 1. Basic lamina-level M&P control data • NCAMP-style data • Requires a single material and process specification • Could be developed by a material manufacturer (e.g., prepregger) or an end-user (perhaps to develop data for a different cure process) • TSO would reference existing published test standards and statistical methods to generate this data 2. Advanced laminate or detailed design data • Class 1 data is a prerequisite • Likely developed by an end-user (such as a partner responsible for design or supplier to propose an alternative design) for unique design details (e.g., structural joints, effects of defects and strength after impact) above the base lamina level used for material control • TSO would not prescribe test methods (i.e., no existing industry standards) November 5, 2019 FAA Research Overview Federal Aviation 16 Administration
Candidate TSO Content • There could be three classes of data (cont.) 3. Tools that use the data from 1 and/or 2 • Class 1 or 2 is a prerequisite – design and analysis tools must be tied to material control and test data developed under TSO • Allows development of analytical tools (e.g., closed-form solutions or FEM) to use the properties developed in 1 or 2 • Must include documentation of HOW to use the data and LIMITATIONS for the data – Limitations are in addition to the M&P restrictions and could include design details (radii, thickness), loading limitations (e.g., stringer spacing, joint details) or other design constraints (e.g., requirements, limits, criteria) • Essentially creating a stand-alone design guide for a given material system, manufacturing process, and design and installation details November 5, 2019 FAA Research Overview Federal Aviation 17 Administration
Workforce Education Initiatives • An essential component for COS and CE is a comprehensive educational development program • Successful composite safety and certification oversight is dependent upon our workforce being knowledgeable of both basic and advanced composite technologies and terminologies – Includes International Standardization and Outreach • Reorganized into two activities – internal FAA training and external outreach/training – Continuing to update/maintain training classes for AFS, ACO and MIDO workforces – All outreach activities, including workshops, documented under this initiative November 5, 2019 FAA Research Overview Federal Aviation 18 Administration
Workforce Education Initiatives FAA Facilitator Industry Sponsor FAA composite training supports three segments of our workforce: engineering, Education Development Education Development Specialized Training manufacturing and maintenance Compliments training available in industry Safety Awareness and academia Introduction Incl. three levels of competency: FAA Sponsor Degree of Involvement Industry Support And Investment – Introduction (“Composites 101”) – Safety Awareness (courses for each functional discipline) • Skills needed for FAA workforce supporting composite applications – Specific Skills Building (most courses developed by the industry) • Specialized skills needed in the industry and some FAA experts November 5, 2019 FAA Research Overview Federal Aviation 19 Administration
Workforce Education Items WE A: Bonding The FAA has developed Updated CMfgT course offered through WSU with revised content, lesson plans and a composite training for ACO job aid, Fall 2020 (coordinate with revised AC 21-43 under initiative CE C) engineers, MIDO inspectors Updated CSET course offered through WSU with revised content, lesson plans and a and FSDO inspectors. All job aid, 12/2019 classes require periodic updates. Coordinate with AFS to submit request to update CMT course offered through Abaris, Fall 2019 WE B: Industry Training and International Outreach Industry workforce development is Jointly host an educational workshop with an industry partner, winter or spring an important educational initiative, 2020 separate from internal education Deliver certification tutorial and composite training at multiple venues, FY19-20 November 5, 2019 FAA Research Overview Federal Aviation 20 Administration
Questions November 5, 2019 FAA Research Overview Federal Aviation 21 Administration
Reminder - Composite Research Topics • Under Structural Integrity of Composites research group, we create research requirements by top-level subject – Think of as “buckets” projects fit within • For FY2020, the subjects are: – SIC.1: Damage Tolerance of Composite Structures – SIC.2: Composite Maintenance Practices – SIC.12: Continued Operational Safety (COS) and Certification Efficiency (CE) for Emerging Composite Technologies – SIC.14 Certification and Maintenance Protocols for Bonded Joints November 5, 2019 FAA Research Overview Federal Aviation 22 Administration
For Discussion • Be thinking about: – What kind of projects you would like to do? – What “bucket” would it would fit in, or do we need a new one? – Will it support the composite plan? – What role will the research play? 1. Evaluate new tools and techniques proposed by applicants 2. Provide publically available data where none exists that supports continued operational safety (support publishing lessons learned) 3. Answer specific questions related to service events 4. Develop tools to promote standardization and increase certification efficiency November 5, 2019 FAA Research Overview Federal Aviation 23 Administration
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