SQR-010 Rev E - Vought

1 Supplier Hardness/ Conductivity Requirements Rev E Page 1 of 6 Supplier Harness/ Conductivity Testing Requirements SQR-010 Revision Date: 02 December 2016 Approved Frank Mariot Supply Chain Quality Manager Suppliers may view this document via the Internet at: To obtain a hard copy, please notify Triumph Aerostructures, LLC or Triumph Aerostructures Tulsa, LLC Procurement Representative Supplier Hardness/ Conductivity Requirements Rev E Page 2 of 6 REVISION RECORD The latest issue of this manual may be confirmed by viewing the Suppliers web site (address shown on the cover). Revision Date Revision Date Revision Date Rev.

2 A 30 Sep 2003 Rev. B 27 Oct 2010 Rev. C 22 Nov 2010 Rev. D 25 Feb 2014 Rev. E 02 Dec 2016 The following is for Triumph Aerostructures, LLC and Triumph Aerostructures Tulsa, LLC internal use only: The information contained in SQR-010 is controlled by the owner listed in the signature sign-off block and is linked to applicable command media. The owner is responsible for the integrity and maintenance of the SQR. PROPRIETARY RIGHTS Triumph Aerostructures, LLC and Triumph Aerostructures Tulsa, LLC proprietary rights are retained for the information contained herein. The recipient, by acceptance of this document, agrees that neither this document nor the information contained herein, nor any part thereof shall be reproduced or transferred to any other document, used or disclosed to others for any purpose, except as specifically authorized in writing by Triumph Aerostructures, LLC and Triumph Aerostructures Tulsa, LLC.

3 Employees of Triumph Aerostructures, LLC or Triumph Aerostructures Tulsa, LLC may reproduce information contained in this document for internal purposes as necessary. All such copies must be prominently identified as REFERENCE ONLY and/or UNCONTROLLED COPY. Supplier Hardness/ Conductivity Requirements Rev E Page 3 of 6 Rev E Summary of Changes Logos information updated Triumph Aerostructures, LLC and Triumph Aerostructures Tulsa, LLC Approvals (Authorizing Signature on File) Frank Mariot -Supply Chain Quality Manager Introduction Section This Document is effective for the following Triumph Aerostructures Companies: Triumph Aerostructures, LLC and Triumph Aerostructures Tulsa, LLC from here on inclusively refer to as Triumph.

4 Supplier Hardness/ Conductivity Requirements Rev E Page 4 of 6 TABLE OF CONTENTS Section Title Page Cover sheet 1 Revision Record 2 Summary of Changes 3 Table of Contents 4 Introduction 5 Requirements 5 Table Title Page 1 Temper Validation Sampling Plan 6 Supplier Hardness/ Conductivity Requirements Rev E Page 5 of 6 Introduction This Document is effective for the following Triumph Aerostructures Companies: Triumph Aerostructures, LLC and Triumph Aerostructures Tulsa, LLC from here on inclusively refer to as Triumph.

5 This document specifies the requirements for Hardness/Conductivity testing by Triumph suppliers as identified in the Supplier Quality Assurance Requirements (SQAR) document. The scope of this document applies to all metallic details at the PO line item level and the metallic details that feed into Assemblies. It is not applied at the Assembly level. Affected Suppliers must have hardness and conductivity testing capability for metallic parts or a detailed procedure for purchasing the service. The requirement must be addressed in the supplier's procedures to the extent necessary to ensure compliance, including control of subcontractors if the service is purchased.

6 The supplier is required to flow all of the SQR-010 requirements down to their sub-tiers. Requirements A second temper verification is required for all products regardless of initial or purchased temper condition. This verification (conductivity only) shall be performed post processing in accordance with Table I sampling plan except for steel parts. For steel parts temper verification (hardness only) shall be performed prior to processing in accordance with Table I sampling plan. Note: Prior to processing is defined as completed parts less all surface treatments such as shot peening, chemical process, prime, and paint.

7 Post processing is defined as completed parts including all surface treatments. All nonconforming material must be submitted to Triumph in accordance with SQR-003. Annealed parts/material or parts with thickness less than in. thick and non-structural detail parts such as fillers, painted, tapered or laminated shims DO NOT require 2nd temper verification. Supplier shall annotate on form CD-4020 or CD-4020B, if parts/material is in the annealed condition in block 20 (remarks). For suppliers that are not P3 (Delegate Source), record actual results on either CD-4020 or CD-4020B as objective evidence. P3 suppliers must annotate results on the packing slip or certifications.

8 The results shall include the customer requirements, actual readings, and quantities tested. Document high and low readings and perform rounding as required by the customer specification. Supplier Hardness/ Conductivity Requirements Rev E Page 6 of 6 Table 1 TEMPER VALIDATION SAMPLING PLAN C=0 95% Reliability Lot size up to 10 All 11 to 22 10 23 to 33 11 34 to 80 12 81 to 4371 13 4372 and up 14