F-16 Flap, Wing Dive Brake

Solicitation / RFP / RFQ

This solicitation is for the "Other Aircraft Part and Auxiliary Equipment Manufacturing" category, identified by NAICS code 336413 with a size standard of 1,250 employees. The acquisition is restricted to qualified sources, specifically listing CAGE codes 1XKR3, 29957, and 81755. Contractors must submit a qualification package to become a qualified source, as detailed in clause 52.209-1 and the attached Manufacturing Qualification Requirement.

• The solicitation details specific line items for aircraft parts, including NSNs and part numbers for F-16 components (e.g., FLAP, WING DIVE BRAKE).

• First Article Test Reports (FATR) are required for certain items (e.g., 0001AA, 0002AA).

• Items require Unique Item Identification (UID).

• Packaging and marking must comply with MIL-STD-130 and MIL-STD-129/ASTM-D-3951.

• Specific clauses address supply chain traceability, manufacturing phase-out, and obsolete materials.

• The contract type is not explicitly stated but implies a Firm Fixed Price structure for production articles.

• The period of performance is indicated by delivery dates extending into 2028.

• The estimated value is not stated.

• Offers are due by 16-MAR-2026 at 11:59 PM.

• Late offers are subject to late proposal provisions.

• Evaluation criteria include Price or Cost as the most important factor, with other factors being significantly less important.

• First Article Testing costs will be a factor in the evaluation.

• This acquisition is restricted to qualified sources as listed.

• Solicitation is approved for U.S. Contractors Only.

• Less than truckload shipments and early/partial deliveries are acceptable at no additional cost.

• Various clauses related to government property, contract administration, payment instructions (WAWF), and representations and certifications are included.

Form / Attachment / Pricing Sheet

This document, a Special Packaging Instruction (SPI), details the specific requirements for packaging the item "FLAP, WING DIVE BRAKE" (Part or Drawing No. 16V1022-812, NSN 1560-01-282-1029 WF). It outlines the materials, methods, and markings necessary for military preservation and shipment.

• Military Preservation: Specifies methods like MIL-STD-2073, including serviceability and unserviceability procedures.
• Materials: Lists specific components for packaging, such as strapping, washers, bolts, blocking, cushioning, and lumber, along with their specifications (e.g., ASTM, ASME standards).
• Dimensions & Weight: Provides detailed internal and external dimensions, gross cubic feet, gross weight, and design fragility for the container.
• Markings: Mandates specific markings, including the SPI number and instructions regarding reusable containers.
• Closure: Details closure requirements according to ASTM D6256.
• Revisions: Notes updates to the document, such as the addition of a preservation method and distribution statement.
• International Standards: Addresses requirements for wood packaging material (WPM) in compliance with ISPM No. 15, focusing on heat treatment and debarking to prevent invasive species.
• Caution Notices: Includes important advisories regarding repackaging, SPIRES listings, material substitution, and overseas/FMS packaging.

This document is critical for any bidder intending to supply the "FLAP, WING DIVE BRAKE." It dictates the exact packaging standards that must be met for successful delivery. Failure to comply with these detailed packaging instructions could lead to rejection of the shipment or other contractual issues. Bidders must carefully review all specified materials, methods, dimensions, and markings to ensure their proposed packaging plan aligns with these requirements.

Form / Attachment / Pricing Sheet

This document is a Contract Data Requirements List (CDRL) detailing the requirements for a "Test/Inspection Report" (Data Item No. A001) for the "Flap, Wing Dive Brak" system. It specifies the format, content, and submission requirements for the "First Article Test Report."

• Data Item Title: Test/Inspection Report (First Article Test Report)
• Contract Line Item Number (CLIN): A
• Contract/PR Number: FD2020-26-00305
• Requiring Office: 416 SCMS/GUEAA
• Format Clarification: The contractor's format is acceptable, but specific requirements for listing dimensions, material identification and certification, and material processing certification must be met.
• Distribution Statement: IAW DoD Instruction 5230.24, with specific distribution to 416 SCMS/GUEAA and a warning regarding export-controlled technical data.
• Submission: The report is to be submitted concurrently with the "First Article" item or separately. Specific shipping instructions and an email address for electronic submission are provided.

This CDRL outlines the specific documentation required from the contractor for the "First Article" of the "Flap, Wing Dive Brak." Bidders should review the detailed requirements for the "Test/Inspection Report" to understand the expected content, format, and submission procedures, including material certifications and compliance with export control regulations. This information is crucial for proposal preparation and ensuring compliance with contract deliverables.

Forms / Attachments / Pricing Sheets

This document is an Engineering Data List (EDL) that provides a comprehensive list of engineering drawings, part numbers, and associated data required for the F-16 aircraft's "FLAP, WING DIVE BRAK" end item. It serves as a reference for material specifications, processes, and components.

• Drawing Numbers and Revisions: Lists specific engineering drawing numbers and their revision levels.
• Part Numbers and Descriptions: Details component part numbers and their descriptions (e.g., "BRACKET-WIRING HARNESS SUPPORT", "ALUMINUM ALLOY PLATE").
• Manufacturer Information: Identifies the manufacturer (Lockheed Martin Corporation) and their CAGE code.
• Material and Process Specifications: References various materials (e.g., sealants, adhesives, aluminum alloys) and processes (e.g., heat treatment, welding, plating) with associated qualified material lists (QML) or qualified processor lists (QPL).
• Furnished Method Codes: Indicates how the data is supplied (e.g., furnished with solicitation, government document, contractor must acquire).

This document is crucial for bidders to understand the specific components, materials, and processes required for the F-16 "FLAP, WING DIVE BRAK" assembly. It helps in determining the feasibility of manufacturing, sourcing materials, and adhering to specified quality and performance standards. Bidders can use this list to identify potential supply chain requirements and ensure compliance with the technical specifications outlined in related solicitations or contracts.

Form / Attachment / Pricing Sheet

This document is an Engineering Data List (EDL) that serves as a comprehensive catalog of engineering drawings, parts, and associated data required for the "FLAP, WING DIVE BRAK" end item (F-16 aircraft). It details specific components, materials, and processes, along with their revision levels and associated qualified material lists (QML) or qualified process list (QPL).

• Drawing Numbers: Lists specific engineering drawing numbers (e.g., 16W1022, FMS-1044).
• Component/Material Descriptions: Provides brief descriptions of parts, assemblies, materials (e.g., "BRACKET-WIRING HARNESS SUPPORT", "ALUMINUM ALLOY PLATE 2124", "SEALANT, INTEGRAL FUEL").
• Processes: Details required processes such as "HEAT TREATMENT OF STEELS", "ADHESIVE BONDED ASSY", "CHEMICAL MILLING OF METALS", and "PENETRANT INSPECTION".
• Revision and Status: Indicates revision levels (REV) and furnished/distribution codes.
• Qualified Material/Process Lists (QML/QPL): References associated QML or QPL documents, which are critical for ensuring approved materials and processes are used.
• Manufacturer: Lockheed Martin Corporation is listed as the manufacturer.

This document is crucial for bidders as it defines the exact specifications, materials, and processes required for components related to the F-16 aircraft's dive brake system. Vendors must ensure their proposed products and manufacturing processes align with the detailed requirements outlined in this EDL and its referenced QML/QPL documents. It directly impacts material sourcing, manufacturing capabilities, and quality control requirements for any vendor seeking to supply parts or services related to this opportunity.

Solicitation / RFP / RFQ

This document outlines the manufacturing qualification requirements for the FLAP, WING DIVE BRAKE (NSN: 1560-01-282-1028, 1560-01-282-1029; P/N: 16W1022-811, 16W1022-812) for the F-16 Aircraft. It details the criteria and processes potential sources must satisfy to become a qualified supplier for this component.

• Prequalification Notice: Offerors must notify the government of their intent to qualify.

• Facilities, Testing, and Inspection Capabilities: Offerors must certify access to or ownership of necessary facilities, equipment, and personnel for manufacturing, inspection, testing, packaging, and storage.

• Data Verification: A complete data package, including procedures and drawings (e.g., LM Aero drawing 16W1022), must be verified.

• Master Tooling: Access to necessary master tooling must be documented and verified by the engineering authority.

• Manufacture/Process Verification: The item must be manufactured to conform to ESA-approved engineering/technical data, including UID requirements. Offerors must provide data showing compliance with quality, performance, and environmental evaluations.

• Test and Evaluation: Offerors must submit a qualification test plan/procedure for approval and a complete test report after testing. The government may inspect testing processes.

• Qualification Article: A pre-contract award qualification article must be provided for form, fit, and function evaluation.

• Estimated Qualification Costs: $8500.

• Estimated Qualification Time: 90 days.

• Eligibility: Offerors must be fully qualified before the contract award date. Qualification does not guarantee award.

• Qualification Article Evaluation: Offerors will be notified of qualification status within 120 days of submitting a product for testing.

• Award Timeline: The award will not be delayed to allow vendors to meet qualification standards.

• Source Qualification Waiver Criteria (QWC): Waivers may be applied for under specific conditions (e.g., prior supply to government, qualification on a similar part, previous qualification of the item).

• A post-contract award first article exhibit may be required to verify production capability, even if a waiver is granted.

Statement of Work (SOW) / Performance Work Statement (PWS)

This document outlines the requirements for preservation, packaging, marking, and shipment of items to be delivered under a contract. It aims to ensure that all materials are handled and transported in compliance with various military and international standards.

• Preservation, Packaging & Marking: Develop and maintain procedures for preservation, packaging, and packing of all items. This includes adherence to AFMCI 24-201 and MIL-STD-2073-1 for packaging, and MIL-STD-129 for markings and labeling. Specific tags (DD Form 1574/1574-1) are required.
• Phytosanitary Measures (ISPM 15): Use approved wood packaging material regulations for international trade, complying with UN-implemented restrictions on wood packaging material (WPM) to prevent invasive species.
• Electrostatic Material: Apply MIL-STD-2073-1 for solid-state devices sensitive to electrostatic forces, using electrostatic-free barrier materials and appropriate labeling.
• Palletized Unit Loads: Comply with MIL-STD-147 for preparing and shipping bonded palletized unit loads.
• Specialized Shipping Containers: Adhere to MIL-STD-648 for design guidelines and testing of specialized shipping containers.
• Hazardous Materials: Ensure compliance with ICAO, CFR Title 49, IATA, IMDG, and AFMAN 24-204 for hazardous shipments. Packaging must meet DOT or UN specifications. Safety Data Sheets (SDS) are required.
• Reporting Discrepancies: Use WebSDR to submit/reply to Supply Discrepancy Reports (SDRs) for improperly packed assets.

Not explicitly stated in this SOW excerpt, but implies worldwide shipments and delivery to DoD facilities.

• Compliance with numerous military standards (MIL-STD) and Air Force Instructions (AFI).
• Use of the ASSIST website to access specifications and standards.
• Specific contact information for AFSC (406 SCMS/GULAA) is provided for inquiries.
• Contractors may need to acquire Competent Authority Approval (CAA) for hazardous material shipments.
• Access to the SPIRES website for packaging instructions is available.

Form / Attachment / Pricing Sheet

This document, "ENGINEERING DATA REQUIREMENTS (ATTACHMENT 'A')", outlines specific instructions and requirements for the manufacture of the "FLAP, WING-LEADING EDGE MANEUVER, ASSY" with Part Number 16W1022-811 and National Stock Number 1560-01282-1028WF.

• Manufacturing Instructions: Specifies that certain military specifications/standards will be used in lieu of indicated data, and superseded data will not be furnished.
• Source/Material: States that listed source/materials on standards, specifications, and drawings are the only ones to be used, with substitutions requiring prior approval.
• Deviations: Prohibits deviations from specifications in control drawings without prior approval.
• Standards: Mandates the use of MIL-STD-130 in lieu of FPS-3008.
• Data for 16W1022-812: Specifies the use of IGES LOFT data (16W329-8, 16W391-8, 16W1330-10) for manufacturing 16W1022-812, as 16PR006 is not furnished.
• Master Tooling: Notes that the government does not have access to the master tooling required for this part, and interested manufacturers must contact Lockheed Martin Co.
• IUID Requirements: Details Item Unique Identifier (IUID) requirements, including contractor drawing updates, label content, use of Human Readable (HRI) and Machine Readable Matrix (USAF not equipped to read barcode), visibility, permanence, and compliance with MIL-STD-130, ANSI/AIM BCII, ISO 15434, ISO 15415, and ISO 15418.
  • IUID Marking Specifications: Includes requirements for minimum 1/8 inch lettering on human-readable labels (CAGE, P/N, Serial Number) and minimum 1/4 inch square on machine-readable 2D matrix (CAGE, P/N, Serial Number).
• 16PR100: States that 16PR100 is not required for manufacture and will not be furnished.
• Delivery Condition: Requires parts to be delivered in a primed condition, without finished paint coating.

This document is critical for bidders intending to manufacture the specified flap assembly. It outlines essential technical requirements, material sourcing, compliance standards (including IUID marking), and specific delivery conditions. Bidders must pay close attention to the master tooling requirement and the need to contact Lockheed Martin Co. for access. The IUID requirements are detailed and must be incorporated into the manufacturing and labeling process. The final delivery condition (primed only) is also a key instruction.

Form / Attachment / Pricing Sheet

This document, "ENGINEERING DATA REQUIREMENTS (ATTACHMENT 'A')", provides specific instructions and requirements for the manufacture of the "FLAP, WING-LEADING EDGE MANEUVER, ASSY" (Part Number: 16W1022-812, National Stock Number: 1560-01282-1029WF).

• Applicable Standards: Specifies the use of MIL-STD-130 in lieu of FPS-3008 and references IGES LOFT DATA (16W329-8, 16W391-8, 16W1330-10) for manufacturing.
• Master Tooling: The government does not possess master tooling; manufacturers must contact Lockheed Martin Co. to obtain it.
• IUID Requirements: Details Item Unique Identifier (IUID) requirements, including the use of human-readable and machine-readable matrix (USAF not equipped for barcode), visibility, permanence, and specific marking standards (MIL-STD-130, ANSI/AIM BCII, ISO 15434, ISO 15415, and ISO 15418).
• Marking Specifications: Requires minimum 1/8 inch lettering for human-readable markings (CAGE, P/N, Serial Number) and minimum 1/4 inch square for machine-readable 2D matrix.
• Other Items: 16PR006 and 16PR100 are not furnished.
• Delivery Condition: Parts must be delivered in a primed condition; finished paint coating is not to be applied.

This attachment is critical for bidders intending to manufacture the specified part. It outlines essential manufacturing standards, data requirements, tooling acquisition procedures, and specific marking instructions (including IUID) that must be adhered to. Failure to comply with these requirements could impact proposal accuracy and contract execution.