FY26 Expeditionary Refueling System
Overview
Buyer
Place of Performance
NAICS
PSC
Set Aside
Original Source
Timeline
Qualification Details
Fit reasons
- NAICS alignment with historical contract wins in similar service areas.
- Scope strongly matches core technical capabilities and delivery model.
Risks
- Past performance thresholds may require one additional teaming partner.
- Potential clarification needed on staffing minimums before bid/no-bid.
Next steps
Validate eligibility requirements, assign capture owner, and schedule partner outreach to confirm teaming strategy before submission planning.
Quick Summary
The Department of the Air Force, specifically FA4855 27 SOCONS LGC, is conducting market research through a Sources Sought notice for an FY26 Expeditionary Refueling System. This initiative aims to identify businesses capable of providing a single-point refueling system designed for the Polaris MRZR, intended for refueling USAF/AFSOC aircraft in austere environments. This is a Total Small Business Set-Aside. Responses are due by February 24, 2026.
Scope of Work
The requirement is for a robust refueling system with the following key specifications:
- Integration: Must fit within the Polaris MRZR cargo bed (48.5in W x 36.0in L x 35.0in H), with additional equipment fitting in the rear seat area.
- Operational Environment: Capable of operating in austere land environments from -30F to 120F.
- Fuel Compatibility: Must store and transfer JP8, JETA, and JETA1 fuels.
- Performance: Required discharge rate of 200-250 gallons/min, with a nozzle pressure limit of 50.0 PSI and pressure relief at 55.0 PSI.
- Components: Includes one 5K collapsible bladder, Camlock 2.0in hose connections, and a multi-fuel internal combustion pump with electric start and manual backup.
- Safety & Features: Must be Mil-Spec compliant, include a 30.0ft kill switch/deadman emergency stop, test ports, a flow meter, and de-fuel capability.
- Portability: Maximum system weight of 500lbs, with handles for 4-man carry/lift.
- Hoses: Two 50.0ft collapsible hoses with Camlock Ends & D3 Nozzle, and one 10.0ft suction side hard hose. Maximum discharge distance of 100.0ft.
- Nozzles: Specific nozzle types detailed, including options for underwing use, regulators, dry break disconnects, strainers, handles, and grounding cables. HEPCV is required.
- Training & Support: Includes system training for 10 trainees over 1 day (at Cannon AFB or company location), operations manual, fuel testing kit, maintenance tools, and parts.
Contract & Timeline
- Type: Sources Sought (Market Research)
- Set-Aside: Total Small Business Set-Aside (FAR 19.5)
- Product/Service Code: 4930 - Lubrication And Fuel Dispensing Equipment
- Response Due: February 24, 2026, 04:00 PM EST
- Published Date: February 17, 2026
- Place of Performance: Cannon AFB, NM 88103, United States
Evaluation
This notice is for market research purposes only and will not result in an award. Responses will be used to determine industry capability.
Additional Notes
Interested contractors should confirm their ability to provide this item or an 'or equal' capability. Responses must include detailed brochures, pamphlets, and/or technical specifications. This is for planning purposes only and does not constitute a solicitation.