SAM #SPRPA126RVC35

T56 QECA Engine Shipping and Storage Containers and Inner Frame Adapter Assemblies Procurement

This procurement opportunity from DLA Aviation at Philadelphia seeks manufacturers for specialized shipping and storage containers for the T56 QECA engine. - Government Buyer: - Defense Logistics Agency (DLA) Aviation, Philadelphia, PA - OEMs and Vendors: - Container Research Corporation (CAGE 05259) - Hilman Inc. (CAGE 28013) - Products/Services Requested: - T56 QECA Engine Shipping and Storage Container (Outer Shell) - Part number: 706E001 - Aluminum construction, desiccant placement, UID marking - Inner Frame Adapter Assembly (IFAA) for T56 QECA Engine Container - Manufactured per technical data package - Roller Assembly - Hilman Inc. alternate source - Part number: 5-OT-03119, Rev. 9 - Unique/Notable Requirements: - Strict compliance with Container Research Corporation drawings and referenced specifications - First Article Testing (FAT) required for new manufacturers - Rigorous welding, leak, and drop test standards - UID marking for traceability - Contractor must provide all manufacturing aids and test equipment - Quality assurance and inspection procedures detailed in solicitation

Description

CONTACT INFORMATION APAC.41 S8X 445-737-3493 MAKAYLA.HAUSER@DLA.MIL ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023) 19 HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT 8 X STOP-WORK ORDER (AUG 1989) 1 FMS DELIVERY AND SHIPPING INSTRUCTIONS 3 michael.e.galanek.civ@us.navy.mil WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023) 16 INVOICE AND RECEIVING REPORT (COMBO) TBD TBD SPRPA1 TBD TBD SEE SCHEDULE TBD NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18) 1 MANDATORY USE OF WORKFLOW PRO (WFP) MOD ASSIST MODULE 1 ROBYN.GRINARML@DLA.MIL VALUE ENGINEERING (JUN 2020) 3 INTEGRITY OF UNIT PRICES (NOV 2021) 1 EQUAL OPPORTUNITY FOR WORKERS WITH DISABILITIES (DEV 2026-O0040)(FEB 2026) 4 TRANSPORTATION OF SUPPLIES BY SEA (OCT 2024) 2 BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM-BASIC (FEB 2024) 11 LIMITATION OF LIABILITY--HIGH-VALUE ITEMS (FEB 1997) 1 NOTICE OF TOTAL SMALL BUSINESS SET-ASIDE (DEV 2026-O0037)(FEB 2026) 1 SECURITY PROHIBITIONS AND EXCLUSIONS (CLASS DEVIATION 2026-O0025)(FEB 2026) 7 BUY AMERICAN-FREE TRADE AGREEMENTS-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024) 5 BUY AMERICAN--BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (FEB 2024) 1 ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (DEVIATION 2026-O0043)(FEB 2026) 13 ROYALTY INFORMATION (APR 1984) 1 NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PREPAREDNESS, AND ENERGY PROGRAM USE (APR 2008) 2 X ONLY ONE OFFER (DEVIATION 2026-O0048)(MAR 2026) 1 ITEM DESCRIPTION AND INSTRUCTIONS THIS ITEM REQUIRES ENGINEERING SOURCE APPROVAL BY THE DESIGN ACTIVITY IN ORDER TO MAINTAIN THE QUALITY OF THE PART. IF YOU HAVE NOT MANUFACTURED THIS ITEM BEFORE FOR DLA WEAPONS SUPPORT PHILADELPHIA AND WANT TO BECOME AN APPROVED SOURCE OF SUPPLY, PLEASE CONTACT THE BUYER BY EMAIL TO INQUIRE ABOUT SOURCE APPROVAL REQUEST PROCEDURES. FOR ALL DRAWING REQUESTS, PLEASE CONTACT THE BUYER BY EMAIL. MAKAYLA.HAUSER@DLA.MIL 1. SCOPE 1.1 PRE-AWARD / POST AWARD REQUIREMENTS: Due to the critical use of this item and its quality history, a pre-award survey and post-award conference may be required for all new manufacturers. For all previous sources, a post-award conference may be recommended. 1.2 Container shell material is Aluminum. Manufacturing this item requires two individual pieces to be made. One being the outer shell or the container that houses the T-56 QECA. The second being the Inner Frame Adapter Assembly (IFAA). They are a set item under this TDP. 1.3 When discrepancies exist between these requirements and those on current manufacturer's drawings, contact code Buyer on Page One or code N241.10 1.4 Articles to be furnished hereunder shall be manufactured, tested and inspected in accordance with Container Research Corporation drawing number (05259) 706E001, Revision latest, and all details and specifications referenced therein. 1.5 Unless expressly provided for elsewhere in this clause, equipment such as fixtures, jigs, dies, patterns, mylars, special tooling, test equipment, or any 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. 1.6 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. 2. APPLICABLE DOCUMENTS STD-225 | 05259 | | | C | STD-228 | 05259 | | | C | STD-295 | 05259 | | | C | STD-360 | 05259 | | | C | 13C099 | 05259 | | | C | 13C102 | 05259 | | | C | 15930 | 80132 | | | D | 17E070 | 05259 | | | C | 706B009 | 05259 | | | C | 706D010 | 05259 | | | C | 706D012 | 05259 | | | C | 706D013 | 05259 | | | C | 706D014 | 05259 | | | C | 706D020 | 05259 | | | C | 706E001 | 05259 | | | C | 706E002 | 05259 | | | C | 706E003 | 05259 | | | C | 706E004 | 05259 | | | C | 706E005 | 05259 | | | C | 706E006 | 05259 | | | C | 706E007 | 05259 | | | C | 706E008 | 05259 | | | C | 706E011 | 05259 | | | C | 706E015 | 05259 | | | C | 706E016 | 05259 | | | C | 706E017 | 05259 | | | C | 706E018 | 05259 | | | C | 706E019 | 05259 | | | C | DOCUMENT REF DATA=MIL-I-45208 | | | A | 810724 | A | 1 | 3. REQUIREMENTS One third (1/3) unit of desiccant (MIL-D-3464, Type II nondusting) per cubic foot of container interior volume shall be placed in desiccant holder of each container at time of shipment. At faying surfaces, discontinuous welds, or other areas where atmospheric liquids may be retained by capillary action, the crevice shall be sealed using Sealing Compound MIL-S-81733 or equivalent. Reference to Cadmium plating shall be deleted and the following substituted: "Finish shall be electrodeposited alkaline Zinc-Nickel Alloy in accordance with ASTM B 841 Class 1, Type B, Grade 3." The shock mount listed in the drawing package (whether identified as sole source, recommended, or suggested) has been tested and approved for the shock mitigation system of this container. No other shock mount may be substituted without written permission of Naval Inventory Control Point, Philadelphia unless an alternate is specifically identified in this contract. No Other is an approved alternate mount. Acceptance Criteria for Aluminum fabrication: All welds shall be visually inspected. Visual inspection shall include 5 power magnifications when suspect condition is to be examined beyond the capability of normal vision. A weld shall be acceptable if it shows: No cracks Through fusion exists between adjacent layers of weld metal, and between weld metal and base metal Weld profiles conform with AWS D1.2 D1.2M:2003 Porosity is not permitted Critical and major welds on the IFAA shall be subjected to further non-destructive testing using dye penetrant inspection to determine the presence of surface cracks. Welding and welder qualifications shall meet current AWS D1.2 Standards. Additionally, cleaning preparations shall be in accordance with MIL-C-5541 and the welding requirement section of the contract. All containers must be affixed with a nameplate that includes a Unique Identification (UID) marking as referenced in the drawing (80132) 15930 and IAW Mil-STD-130 latest revision. The contractor shall contact NAVICP code Contact Buyer found on Page 1 of the Contract or code 0771.10 for the serial number group that makes up part of the UID. The UID will be included on the nameplate in data matrix format. Welding and welder qualifications shall be in accordance with AWS D1.1 for steel, AWS D1.2 or MIL-W-22248, Class 4 for aluminum, AWS D1.3 for sheet steel, and AWS D1.6 for stainless steel. Proper controls shall be used to prevent melt through or burn through. For aluminum, filler for welding 6061 alloy shall be 4043; filler for welding 5000 series alloys to themselves or to 6061 shall be 5356 or 5556. Welding and inspection shall include visual inspection with 5X magnification, non-destructive testing as prescribed, and proper documentation. Work instructions shall be posted at the operator's work station giving procedures to control the welding process, including filler material, weld size, electrical and gas characteristics, including flow rate. Materials and materials control: The quality program shall ensure that materials used in fabrication or processing conform to applicable requirements, with supplier’s certification being sufficient. Controls: Weld filler materials shall be clearly identified and segregated. The work environment shall be controlled to prevent adverse conditions. Cleaning: Parts to be welded shall be cleaned to remove surface soils, avoiding uninhibited alkaline solutions. Deoxidizing: Cleaned parts shall be chemically deoxidized no more than 10 days prior to welding, or 3 days if exposed outdoors. Mechanical cleaning methods shall be applied just prior to welding to remove oxides. Chemical Treatment: Use nitric acid, sulfuric chromic, phosphoric chromic, or equivalent solutions for deoxidizing. Sodium hydroxide solutions shall not be used. Coverage must extend at least 2 inches from the weld site. Mechanical Means: Mechanical cleaning shall be applied immediately prior to welding, using methods like wire brushing, scraping, filing, or sanding, avoiding iron, steel wool, copper alloys that may cause galvanic corrosion. Contact code N241.11 or N241.10 to arrange for first article test facility location. Submit drawings, contracts, ECOs, deviations, waivers, and modifications accordingly. Each container shall be assigned a serial number in the format "contract#_no_dashes-000X". 4. QUALITY ASSURANCE 100% PRODUCTION LEAK TEST: Containers shall be tested for leakage using pneumatic-pressure technique, with specific procedures and rejection criteria outlined. Weld inspections shall follow AWS standards, including visual and dye penetrant testing. First Article tests include dimensional, form, fit, and functional requirements, with specific procedures and documentation. Disposal of FAT samples: destroyed during testing unless otherwise specified. Test sample coating instructions: unpainted, with corrosion areas coated with light preservative. FAT approval criteria: delivery of one unit within 160 days, marking, and documentation requirements, with procedures for disapproval and re-submission. Alternate offers and waiver of First Article approval: conditions and procedures outlined, including submission of two prices and potential schedule adjustments. Additional testing procedures, shipping instructions, and responsibilities are detailed. 5. PACKAGING Mil-Std 2073 packaging applies as found elsewhere in the schedule. 6. NOTES - NOT APPLICABLE This NIIN and TDP are setup for procurement of both an inner-frame and an outer-shell container for the T56 QECA engine. Contact I. Stanke at 0771.13 x2458, 03/25/05 for further details. This buy has updated drawings for the extrusion, which are no longer source controlled. Additionally, on drawing number 706E005, the roller assembly (Part Number 17C069-1) listed as item 26 has an alternate source of supply: Hilman Inc., cage 28013, part number from drawing 5-OT-03119, Rev. "9". Contact I. Stanke at 0771.13 x2458, 09/27/05. Additional Links: See Solicitation SPRPA126RVC35

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