16--LEVER ASSEMBLY,AXLE, IN REPAIR/MODIFICATION OF

CONTACT INFORMATION|4|N733.08|N00383|+1 (555) 000-0000|contact@example.gov| ITEM UNIQUE IDENTIFICATION AND VALUATION (MAR 2022)|19|||||||||||||||||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT|8|X|||||||| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (DEC 2018)|16|Invoice and Receiving Report Combo|Invoice and Receiving Report Combo|TBD|N00383|TBD|TBD|SEE SCHEDULE|TBD||||||||| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUN 2003)|6|365 Days|45 days of the last delivery under this contract||||| EQUAL OPPORTUITY FOR WORKERS WITH DISABILITIES (JUN 2020)|2||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM - BASIC(DEVIATION 2020-O0019) (MAR 2022))|3|||| LIMITATIONS ON PASS-THROUGH CHARGES (JUN 2020)|1|| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|||||||||||||| BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE (DEVIATION 2020-O0019) (JUL 2020))|3|||| BUY AMERICAN--BALANCE OF PAYMENTS PROGRAM (NOV 2014)|1|| ROYALTY INFORMATION (APR 1984)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAY 2022)|13|336413|1,250|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PREPAREDNESS, ANDENERGY PROGRAM USE (APR 2008))|2||X DO rated order certified for national defense| The purpose of this amendment is to incorporate the following changes: 1. The total quantity is increased by 1 unit, from 2 units to 3 units. All other terms and conditions remain the same. This contract/delivery order/purchase order/modification is issued by the Government when deposited in the mail, transmitted by facsimile or sent by any electronic commerce method, including email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to issue this contract/delivery order/purchase order/modification. \ The Small Business Administration representative at NAVSUP WSS has reviewed this requirement and determined that a set-aside recommendation was not applicable for this procurement. This RFQ is for repair and will be using competitive procedures. The requested RTAT is 252.9 days. This requirement will be awarded to the offeror with the lowest price technically acceptable (LPTA) quote. Quotes may be emailed to the below email address and must be received on or before on the closing date listed on page 1 of the solicitation. contact@example.gov. \ 1. SCOPE REPAIR MANUAL/PROCEDURES Overhaul IAW with the following Government Furnished Information (GFI) Technical Data: MAIN LANDING LEVER ASSEMBLY P/N: (76301)74A410506-1009/-1010/-1011/-1012 LES-NI-31026-92 / Revision B Release 21 FEB 2018 Technical Manual, Main Landing Gear Axle Lever Assembly, A1-422AC-130-050 Intermediate and Depot Level Technical Manuals A1-F18AC-SRM-300 Nondestructive Inspection WP069 05 Part Drawings (76301) 74A410506 Boeing Process Specifications (PS) 1.1 Articles to be furnished hereunder shall be repaired, tested andinspected in accordance with the terms and conditions specified in theRequirements Section of this document. 1.2 Unless expressly provided for elsewhere in this clause, equipment suchas fixtures, jigs, dies, patterns, mylars, special tooling, test equipment, orany other manufacturing aid required for the manufacture and/or testing of the subject item(s) will not be provided by the Government or any other source and is the sole responsibility of the contractor. The foregoing applies notwithstanding any reference to such equipment or the furnishing thereof that may be contained in any drawing or referenced specification. 1.3 The use of MIL-W-81381 wire in any item to be delivered under this procurement is prohibited. The foregoing prohibition applies notwithstanding any reference to MIL-W-81381 wire that may be made in any of the drawings or specifications for this procurement. SAE-AS22759 series wire shall be used in lieu of MIL-W-81381 wire, in any place where MIL-W-81381 wire is cited in this procurement. Any questions concerning this requirement should be directed to the Procuring Contracting Officer. 1.4 If MIL-STD-454 is referenced in the drawings or in the specification,the contractor is expected to show compliance with IPC/EIAJ-STD-001C Personnel performing tasks in accordance with IPC/EIAJ-STD-001C shall be trained and certified as requried by IPC/EIAJ-STD-001C paragraph 5.1.4. 2. APPLICABLE DOCUMENTS - NOT APPLICABLE 3. REQUIREMENTS Main Landing Gear Lever Assembly LES (LES-NI-31026-92 / Amendment 3) Additional QA Characteristics, See Hard copy Statement of work dated 21 Feb 2018 4. QUALITY ASSURANCE First Article Inspection Requirements: NAVAIR Landing Gear Engineer(s) or its designated government representative will witness First Article assembly and testing. Contractor is responsible for providing the necessary personal and resources to expedite the First Article assembly and testing. Notification At least 45 days before beginning of First Article Testing, the contractor must notify the PCO, in writing, of the time and location of the testing so that the Government may witness the testing. In addition to the PCO, the contractor must notify the Navy First Article Test manager via e-mail at contact@example.gov so that the Navy may witness the FAT or delegate FAT approval to DCMA QAR, according to the discretion of the Navy. U.S. Government personnel, including the DCMA QAR and NAVAIR Landing Gear Engineer(s) or its designated government representative, will witness testing at the contractor's facility. Inspection records and completed router/traveler must be submitted for review prior to assembly. The router/traveler approval will be provided by NAVAIR Landing Gear Engineer or its designated government representative. Upon approval contractor is responsible to coordinate with PCO and NAVAIR Landing Gear Engineer(s) for onsite inspection/and witness of First Article Test. Test Report The FAT Report must be in accordance with the requirements of AS9102 (Aerospace First Article Inspection Requirement), MIL-HDBK-831 or equivalent, and must be submitted via the cognizant DCMA Contract Administration Office to the PCO. The contractor must submit the FAT Report via the PCO within 15 days from the date of completion of First Article Testing to NAVAIR Landing Gear Engineers for approval. At a minimum, the following processes will be demonstrated by witnessing NAVAIR Landing Gear Engineer Bearing and Bushing Removal Bearing and Bushing Installation Strip Electroplated Coating Degreasing Temper Etch for Burns Magnetic Particle Inspection Cadmium, Nickel and/or Chrome plating as required Machining Abrasive Blasting Shot Peening Dimensional Inspection Magnetoelastic (Rollscan) X-ray Diffraction (XRD) Ultrasonic Inspection Penetrant Inspection NAVAIR Landing Gear Engineer may waive demonstration requirements for any specific processes, in lieu of verification of Certificates of Conformance. NAVAIR Landing Gear Engineer or its designated government representative must provide First Article Acceptance or the necessary path to Acceptance prior to production. 5. PACKAGING- MIL-STD 2073 PACKAGING APPLIES AS FOUND ELSEWHERE IN THE SCHEDULE 6. NOTES - NOT APPLICABLE DATE OF FIRST SUBMISSION=ASREQ DATE OF SUBSEQUENT SUBMISSION=ASREQ Paragraphs 10.1, 10.2, 10.2.1, 10.2.2, 10.2.4 and 10.5 apply. Block 9: Statement B, US Government, Naval Inventory Control Point Block 12: First submission to be made upon submission of ;FAT; testing sample. ^ Block 14: Make submission to ;NAVAIR LANDING GEAR ENGINEER NAVSUP CODE N23 DCMA-QAR; . Block 13: Second submission required if the process/operation changes after approval of ;FAT; test. ^^ Block 14: Make submission to ;NAVAIR LANDING GEAR ENGINEER NAVSUP CODE N23 DCMA-QAR ; . Block 14: When NAVICP 02 is referenced in distribution, forward to the NAVICP code cited on Block 10.A. on page 1. DATE OF FIRST SUBMISSION=ASREQ DATE OF SUBSEQUENT SUBMISSION=ASREQ Paragraphs 10.1, 10.2, 10.2.1, 10.2.2, 10.2.4 and 10.5 apply. Block 9: Statement B, US Government, Naval Inventory Control Point Block 12: First submission to be made upon submission of ;FAT; testing sample. ^ Block 14: Make submission to ;NAVAIR LANDING GEAR ENGINEER NAVSUP CODE N23 DCMA-QAR ; . Block 14: When NAVICP 02 is referenced in distribution, forward to the NAVICP code cited on Block 10.A. on page 1. DATE OF FIRST SUBMISSION=ASREQ DATE OF SUBSEQUENT SUBMISSION=ASREQ Block 6: Forward additional copy to ASO code cited in Block 10.A on page 1. 1. This Data Item Description (DID) contains the format, content and preparation instructions for the data product resulting from the work task described in paragraph 5.4.3.4 or 5.4.8.3.3 of MIL-STD-973. 2. Copies of the Request for Waiver form are available from the DODSSP, Standardization Documents Order Desk, Building 40, 700 Robbins Avenue, Philadelphia, PA 19111-5094 3. Format an Content: The request for Deviation format and content shall be in accordance with Appendix E of MIL-STD-973 DATE OF FIRST SUBMISSION=ASREQ DATE OF SUBSEQUENT SUBMISSION=ASREQ Paragraphs 10.1, 10.2, 10.2.1, 10.2.2, 10.2.4 and 10.5 apply. Block 9: Statement B, US Government, Naval Inventory Control Point Block 14: When NAVICP 02 is referenced in distribution, forward to the NAVICP code cited on Block 10.A. on page 1. Block 3: Separate reports shall be provided for the below listed subtitles and shall include certification that all vendors performing these processes are prime (OEM) approved sources. In the case where other than the OEM's specifications are to be utilized, separate certifications are required. BLOCK #5: Contract Reference: ;Material and process subcontractors must be approved by Boeing in accordance with Boeing Approved Vendor list D1-4426.;