SOW 3KCERS Ver 4.docx

Statement of Work FY24 Containerized Refueling Platform Joint Base McGuire-Dix-Lakehurst

1. General The contractor shall provide a containerized refueling platform, containing all the required equipment to perform refueling operations in an austere environment that is built to the MIL-PRF.

2. Scope of Work Per Contingency Response requirements the following requirements need to be met:

1. Provide a self-contained system capable of fitting inside one ISU90 NSN 8145-01-465-3621 (Dimensions: 108x88x91.35”). It is a shipping container designed to fit in a military cargo aircraft and be Air Transportation Test Loading Activity (ATTLA) certified.

2. Capable of pumping fuel at minimum rate of 350 gpm with maximum of 600 gpm.

3. Contain a filter separator capable of filtering fuel of sediment and contaminants IAW T.O. 42B-1-1 Table 4-1 4c Quality Control of Fuels and Lubricants at a minimum rate of 350 gpm.

a) Particulate matter will be tested by color and particle assessment method/DP. Per T.O. 42B-1-1 Table 4-2. Color max = 4 and particle max = Acceptable. Matched weight or gravimetric determination, 0.5 mg/L max and 10 PPM for free water. Testing parameters and analysis will be derived from Appendix C Test Procedures Part C.2.1 to C.2.7 for color of T.O. 42B-1-1.

4. Contain a minimum of two 3,000-gallon collapsible fuel bladders.

a) Made from military grade polyurethane using nylon base fabric and hold 3,000 gallons.

b) Working temperature of -25° to 160° F.

c) Fuel bladders must be made of coated fabric 35 to 62 Oz/yd2.

d) It must be high puncture resistant (150 to 225 lbs, min).

e) Drain port opening must be 4“.

f) Fittings must be chemically and mechanically bonded fittings.

g) Permeability must be 0.06 fl-oz/sq-yd/day

h) It must be rated to store JP8, JP5, Diesel, and Aviation Gasoline.

i) Tank must be 180”(4.57m) L x 180” (4.57m) W with est’d fill height at 30” (0.76m).

5. Contain secondary containment for the fuel bladders

6. Contain a minimum of 100’ of two 4” non-collapsible hoses

7. Contain a minimum of 1,000’ of 2” collapsible hoses

8. Contain sufficient space for 2 or more Pelican cases containing various refueling nozzles, rebuild kits, and associated fitting/tools. Refueling nozzles will be a single-point nozzle for severe duty.

· Nozzle will conform to SAE-AS5877.

· The adapter will connect to MS24484 Single Point Adapter. The adapter will use square register pins that provides positive alignment with square slots in the aircraft adapter.

a) The nozzle should not be able to be removed from the adapter until the operating lever is rotated to the fully-closed position.

b) The nozzle will use a stainless steel bayonet ring cast within the aluminum collar of the nozzle.

c) The crank shaft of the nozzle extends across the entire width of the interior flow path and is supported from end-to-end by a structural wall that splits the flow path.

d) It will have a variable swivel inlet, a 100-mesh strainer, dry-break quick disconnect, and 2-inch NPT threads. Further dimensions are referenced in the attached engineering specification of the nozzle.

3. Objectives Provide a tactical fuel system meeting all highlighted parameters outlined in the scope of work and Appendix A to the 621 CRW.

4. Personnel The selected vendor will provide delivery of this item. The maintenance, accountability and operating of this item will be solely the responsibility of the 621 CRW.

5. Equipment Requirements See Appendix A

6. Deliverables

a. The vendor will only deliver new products. Refurbished or used products will not be accepted by the government.

b. Warranty:

The contractor shall provide any Original Equipment Manufacturer (OEM) standard commercial warranty applicable to the products being purchased at no additional cost to the Government. Prior to project acceptance, the contractor shall provide the customer with all manufacturer warranties as needed for any component incorporated into this project such as equipment manuals, literature, CDs and DVDs and other documentation on all equipment. Prior to project acceptance, the contractor shall provide written procedures, points of contact within company, and required information for all warranty services prior to project acceptance. This information shall include written confirmation of the warranty period, phone numbers and contact information/procedures for technical support, troubleshooting assistance, and replacement of faulty equipment.

c. Delivery shall occur within 16 weeks of award.

d. POC for this request is MSgt Brandon Earl

i. Telephone: 609-754-8034

ii. Email: brandon.earl@us.af.mil

iii. Address: Bldg 3422, Broidy Road JBMDL, NJ 08641

Appendix A

BRANDON R. EARL, MSgt, USAF Section Chief, Fuels Information Service Center, 621 CRSS