Clutch Repair Kits

Statement of Work (SOW)

To furnish all required parts, equipment, material, freight, and labor to provide 60 each BAK-12 Clutch Repair Kits to CEMIRT, AFCEC/COMX at Tyndall AFB, Florida.

Contractors must meet one of the following conditions:

• Possess First Article (FAT) approval from AFLCMC as an authorized vendor for BAK-12 Clutch Repair Kits and have successfully delivered production units within the last three years.
• Successfully complete First Article Testing (FAT) requirements as per FAR clause 52.209-4.

Key requirements include:

• Adherence to USAF drawings (referenced in Section 3).

• Production of computer-aided design (CAD) drawings compliant with ASME Y14.1 standards.

• Provision of all necessary tools, equipment, personnel, and facilities.

• Fabrication or acquisition of parts to specific dimensions and tolerances per ASME Y14.5.

• Use of water jet or laser cutting systems for precision parts from large steel sheets.

• Welding and inspection processes in accordance with American Welding Society (AWS) D1.1 for critically loaded structures, with certified welders and inspectors.

• Provide 60 new BAK-12 Clutch Repair Kits.

• Each assembly must meet specifications and notes within the provided drawings.

• No refurbished parts are allowed.

• Specifics for the Parts Kit, Clutch include:

  • National Stock Number (NSN): 3010-01-490-6666
  • Part Number (P/N): 200037000-1

• Eight (8) attachments/drawings are referenced for specific components (e.g., Backing Plate, Pressure Plate, Stator Plate, Rotor Plate Assembly, Rotor Core, Friction Pad, Rivet).

• Drawings must be approved by AFCEC/COMX before work begins and will become Air Force property.

• Required for contractors without existing FAT approval or recent production delivery.

• FAT process to be coordinated through AFCEC/COMX.

• FAT Approval must be obtained no later than 285 calendar days after contract award.

• Contractor shall submit PDF file drawings within 60 days of contract award.

• First article delivery is due no later than 180 calendar days after receipt of government drawing review.

• Government will perform a conformity check within 30 days of receiving the initial first article.

• Contractor is responsible for costs associated with any required third-party verification if deficiencies are found.

• Approved first article will be retained by the government and considered the first production item.

• Coordinate with POCs 30 days prior to delivery.

• Delivery address: AFCEC/COMX, 1001 Mississippi Rd; Bldg. 1141, Tyndall AFB, FL 32403.

• Kits with structural, component, or excessive paint damage will be refused.

Statement of Work (SOW)

To furnish all required parts, equipment, material, freight, and labor to provide 60 new Barrier Arresting Kit (BAK)-12 Clutch Repair Kits to CEMIRT, AFCEC/COMX at Tyndall AFB, Florida.

Contractors must meet specific requirements, including:

• Adherence to USAF drawings, specifications, and industry standards (e.g., ASME Y14.1 for CAD drawings, ASME Y14.5 for fabrication/acquisition of parts).

• Use of precision cutting methods (water jet or laser) for parts from large steel sheets.

• Compliance with American Welding Society (AWS) D1.1 for welding and inspection of critically loaded structures, with certified welders and inspectors.

• Provision of new parts only; no refurbished parts are allowed.

• The contractor is responsible for all required equipment, material, labor, and parts.

• The primary deliverable is 60 each of the Clutch Repair Kit, identified by National Stock Number (NSN) 3010-01-490-6666 and Part Number (P/N) 200037000-1.

• Eight specific drawings related to the kit components are referenced and must be adhered to.

• Revised drawings must be provided to consolidate and fix discrepancies.

• All drawings require approval by AFCEC/COMX before work commences and become Air Force property upon approval.

• FAT is required for contractors without prior FAT approval or recent production unit delivery (within 3 years of solicitation issuance).

• The first article must meet all scope of work, drawing, and technical specification requirements.

• FAT coordination is through AFCEC/COMX.

• FAT approval must be obtained no later than 285 calendar days after contract award.

• Contractors must submit PDF drawings within 60 days of award and the first article within 180 days of government drawing review.

• The government will perform conformity checks within 30 days of receiving the first article.

• Contractors are responsible for costs associated with third-party verification if deficiencies are found.

• The approved first article will be retained by the government and counts as the first production item.

• Coordination with POCs is required 30 days prior to delivery.

• Delivery address: AFCEC/COMX, 1001 Mississippi Rd; Bldg. 1141, Tyndall AFB, FL 32403.

• Heavy Weight Fairlead Beam Assemblies with structural, component, or excessive paint damage will be refused.

Form / Attachment / Pricing Sheet

This document is a drawing for a Repair Kit, Clutch (Part Number 200037000). It serves as a parts list and technical drawing for the kit.

• Parts List: Details components of the Repair Kit, Clutch, including:
  • Rotor Plate Assembly (200037004-10)
  • Stator Plate (200037003-1)
  • Pressure Plate (200037002-1)
  • Backing Plate (200037001-1)
  • Repair Kit, Clutch (200037000-1)
• Notes: Specifies packaging and protection requirements for kit components, including the use of rust preventive dip, corrosion inhibiting packaging material, and desiccant.
• Technical Specifications: Includes tolerances for dimensions and angles.
• Government Information: Identifies the drawing as being developed for the U.S. Air Force, with distribution approved for public release.

This drawing is crucial for bidders to understand the exact components, part numbers, and specifications required for the Repair Kit, Clutch. The detailed notes on packaging and protection are also important for bidders to adhere to during fulfillment if they are awarded a contract for this item.

Solicitation / RFP / RFQ

This solicitation is for the procurement of Clutch Repair Kits, Part Number (P/N): 200037000-1. The acquisition is being conducted using Simplified Acquisition Procedures (SAP) pursuant to FAR Part 13.

• The primary deliverable is Clutch Repair Kits, P/N: 200037000-1.

• Quantity: 60 units.

• The document references an attached Statement of Work (SOW) for detailed requirements.

• First Article Test (FAT) process is a key requirement. Offerors must provide evidence of FAT approval for Clutch Repair Kits and delivery of FAT-approved production units within the last three years, or submit a detailed schedule for meeting delivery requirements.

• Pricing Arrangement: Firm Fixed Price.

• Delivery Schedule: 435 Calendar Days from the Date of Award.

• FOB: Destination.

• The contract will be awarded to the offeror determined to provide the best value to the Government, considering both Price and Technical factors.

• Offerors must submit proposals in two volumes: Volume 1 - Price and Volume 2 - Technical.

• Volume 1 (Price) requires proposed pricing for CLIN 0001, including unit price, extended price, and all transportation and delivery charges.

• Volume 2 (Technical) has a 7-page limit and requires a technical approach detailing tools, equipment, personnel, and facilities for fabrication, and the First Article Test (FAT) process.

• The offeror's technical approach must demonstrate an adequate understanding of the requirements and cannot merely restate the SOW.

• Offer Due Date: 19 February 2026, 01:00 PM.

• Questions are due no later than 7 February 2026 at 1:00 PM CST.

• This acquisition is set aside for Small Business.

• NAICS Code: 336413, Size Standard: 1250 employees.

• Numerous FAR and DFARS clauses are incorporated by reference and in full text, covering various aspects such as payment, contract administration, representations and certifications, and special requirements.

• The solicitation includes detailed instructions for offer preparation and submission, including formatting restrictions.

Form / Attachment / Pricing Sheet

This document is a technical drawing (Drawing #200037005) for a "ROTOR CORE" intended for the U.S. Air Force. It provides detailed specifications for the manufacturing and assembly of this component.

• Material: STEEL, UNS G10200 per ASTM A108.
• Finish: 63 all over except as noted; surface texture per ANSI B46.1.
• Tolerances: Per ANSI Y14.5M-1994, with specific tolerances for dimensions (e.g., ±.01, ±.004) and angles (±.5°).
• Dimensions: Detailed measurements and hole patterns are provided, including diameters, through-hole sizes, and angular specifications.
• Notes: Includes instructions for CAD maintenance, distribution statement (approved for public release, unlimited distribution), and interpretation of drawings per MIL-STD-100G.

This drawing is critical for any bidder involved in the manufacturing, procurement, or integration of the "ROTOR CORE." It defines the precise physical characteristics, material requirements, and quality standards that must be met. Bidders must ensure their proposals and manufacturing capabilities align with these specifications.

Form / Attachment / Pricing Sheet

This document is a technical drawing for the "ROTOR PLATE ASSEMBLY" (Part Number 200037004-10). It provides detailed specifications and dimensions for the assembly and its components.

• Assembly Name: ROTOR PLATE ASSEMBLY
• Part Number: 200037004-10
• Components Listed: ROTOR CORE (98752 200037005-1), FRICTION PAD (98752 200037006-1), RIVET (98752 200037007-1)
• Technical Drawings: Includes top view, side view (Section A-A), and a parts list.
• Notes: Specifies installation requirements for rivets, material specifications, and dimensional tolerances per ANSI Y14.5M-1994.
• Government Information: Includes contract number, contractor, and distribution statement indicating public release is unlimited.

This drawing is critical for bidders who need to understand the exact specifications, materials, and assembly requirements for the Rotor Plate Assembly. It serves as a definitive guide for manufacturing or procuring this specific part, ensuring compliance with government standards and technical requirements.

Form / Attachment / Pricing Sheet

This document is a technical drawing (Drawing #200037007) for a "RIVET" component. It provides detailed specifications for manufacturing this part.

• Part Name: RIVET
• Drawing Number: 200037007
• Material: STEEL, ASTM A36, NORMALIZED
• Finishes: Specified surface texture and zinc plating requirements (ASTM B633).
• Dimensions & Tolerances: Detailed measurements and allowable deviations are provided, with specific tolerances for 2-place and 3-place decimal dimensions, and angles.
• Notes: Includes requirements for material, finish, dimensioning/tolerancing per ANSI standards, and distribution statement for public release.

This drawing is crucial for bidders who need to understand the exact specifications of a component required for the opportunity. It details the physical characteristics, material, and quality standards that the "RIVET" must meet. Bidders will use this information to determine manufacturing feasibility, cost, and compliance with technical requirements.

Form / Attachment / Pricing Sheet

This document is a technical drawing for a "FRICTION PAD" (Part Number 200037006). It provides detailed specifications and dimensions required for the manufacturing or procurement of this part.

• Part Name: FRICTION PAD
• Part Number: 200037006
• Manufacturer/Supplier: FRICTION PRODUCTS CO. (9G780)
• Dimensions: Detailed measurements and tolerances are provided in inches, with specific callouts for lengths, radii, and hole diameters.
• Material: Not explicitly stated, but the part is identified as a "FRICTION PAD."
• Notes: Includes instructions regarding alternate part numbers, dimensioning and tolerancing standards (ANSI Y14.5M-1994), and drawing maintenance.
• Issuing Authority: U.S. AIR FORCE

Bidders responding to an opportunity that requires this specific friction pad must use this drawing to ensure their proposed product meets all specified dimensions, tolerances, and potentially material requirements. It is crucial for manufacturing, quality control, and proposal pricing.

Form / Attachment / Pricing Sheet

This document is a technical drawing (Drawing # 200037001) for a "BACKING PLATE, BAK-12 CLUTCH". It provides detailed specifications for the manufacturing of this part.

• Material: 4130 Alloy Steel Plate (per AMS specifications).
• Finish: Specifies surface finish requirements, including a zinc clad primer and polyurethane topcoat, with specific color (Olive Drab Green).
• Dimensions and Tolerances: Details critical measurements, hole patterns, and tolerances according to ANSI Y14.5M-1994.
• Notes: Includes important manufacturing instructions, such as breaking sharp edges, removing burrs, and protecting unfinished surfaces.
• Part Identification: Specifies marking requirements per MIL-STD-130, including part number, manufacturer's CAGE code, and revision history.

This drawing is crucial for any bidder intending to manufacture or supply the "BACKING PLATE, BAK-12 CLUTCH". It defines the exact technical requirements, materials, and quality standards that must be met. Bidders must ensure their proposed product conforms precisely to these specifications. The drawing also indicates it is for U.S. Air Force use and approved for public release with unlimited distribution.

Form / Attachment / Pricing Sheet

This document is a technical drawing (drawing number 200037003) for a "STATOR PLATE". It provides detailed specifications for the manufacturing of this component.

• Material: 4130 Alloy Steel Plate per AMS 6350 or AMS 6351.
• Finish: 125 all over, with sharp edges broken and burrs removed. Surface texture per ANSI B46.1.
• Marking: Steel stamp per MIL-STD-130 with specific identification numbers.
• Dimensions and Tolerances: Per ANSI Y14.5M-1994. Specific dimensions and tolerances are provided for the plate's features, including diameter, thickness, and the number and size of notches.
• Revision History: Includes a revision record (Revision A) dated 20080807.

This drawing is critical for any bidder needing to understand the precise physical specifications, material requirements, and manufacturing tolerances for the STATOR PLATE. It directly informs manufacturing capabilities, material sourcing, and quality control processes required for this component.

Form / Attachment / Pricing Sheet

This document is a technical drawing for a "PRESSURE PLATE" identified by drawing number 200037002. It provides detailed specifications for the manufacturing of this part.

• Material: 4130 ALLOY STEEL PLATE per AMS 6350, AMS 6351, or AMS 6345.
• Finish: 125 all over, with sharp edges broken and burrs removed. Surface texture per ANSI B46.1.
• Marking: Steel stamp per MIL-STD-130 with specific identification numbers.
• Dimensions and Tolerances: Per ANSI Y14.5M-1994.
• Key Dimensions: Includes overall diameter, various hole sizes and depths, and specific radii.
• Notes: Specifies material, finish, marking, and dimensional tolerance standards.
• Revision History: Details changes made to the drawing.

This drawing is critical for any bidder needing to understand the precise physical specifications, material requirements, and manufacturing tolerances for the "PRESSURE PLATE" component. It directly informs manufacturing capabilities, material sourcing, and quality control processes required for producing this part.