Bowser_Spec_sheet.pdf

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Attached to
UAV Fuel Bowser Federal contract opportunity
Solicitation number
CAMPBELL2-160CVH0008
Issued by
Department of the Army

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Physical Characteristics

1. Size/ Shape- Approximately 127” length x 58-1/8” Width x 48- 1/2” height (tow bar not included) Dimensions are estimates only not inspection criteria

2. Weigh- 2200lbs maximum Weight is estimate only not inspection criteria

3. Power- Pump operation can be operated by:

- Onboard Batteries of type MIL 8565/ 5-2 o Battery is NSN 6140-01-502-4405 o Unit be equipped with sufficient number of batteries to provide a minimum of 3 hours of pump run time between charges.

o Onboard charging capability taking power from either of the connectors defined below 28vDC supplied via NATO connector 110vAC supplied by NEMA connector

4. Color/ Finish Tank and undercarriage are FED-STD-595 color 33303 (SAND) using coating, aliphatic polyurethane, and chemical resistant (CARC) paint to

MIL-DTL-53039B

Decals & Markings Fuel/ De-Fuel Cart is decaled to include warning decals, product decals, placards and “JP-8 fuel”

5. Interface, Electrical

- 24-28.5 V DC and

- 110vAC 50-60hz

6. Connectors, Electrical

- For 28vDC: NATO Standard per MS3506-1

- 110vAC: NEMA 5-15 male standard

7. Operating Environment- Pumps must operate without performance degradation in the following environments:

1. Ambient air temperatures from 25 degrees Fahrenheit to 140 degrees Fahrenheit

2. Relative humidity from 5% to 95% (non-condensing)

3. Density altitudes up to 9000 feet.

8. Mechanical Interface

- Fueling Nozzle

- De-fueling adapter assembly

Fuel Container

The fuel tank is a 250 gallon nominal capacity tank with an actual capacity of 280 gallons to accommodate vapor expansion. The tank is a top fill, baffled and pressure tested vessel. Tank includes the following design features:

- Stainless Steel construction with secondary containment

- DOT406 Style manway/ top fill opening with cove access & overpressure protection

- Low point sump with water drain

- Fuel level indicator with ¼ tank capacity increments

- Vent shield kit to prevent rain intrusion

Chassis and Fuel Transfer

The fuel/ de-fuel cart undercarriage must use a towable two axle, four wheeled rolling chassis design that is self-supported on its own rigid or non-suspension axle mount configuration suitable for ramp usage at speeds up to 15 MPH. It must be designed with a steerable front tow bar so that it is easily towed or tugged with normal aircraft ramp equipment. The tow bar must include a mechanism to hold it in the upright position when not configured for towing to mitigate tripping hazards.

Fuel/ De-fuel cart must include two pumps; one for fueling and a second, smaller pump for de-fueling operations. The main fueling pump will be capable of recirculation fuel from the reservoir, through the filter-separator elements for the field fuel decontamination. The same fuel line with quick-disconnect fitting on the end will be used for both fueling and de-fuel fitting, and operating a switch and/or valve both the fueler. Fuel will be filtered in both operations utilizing Aviation grade, dual stage fuel filtration - required to be Category “M” filter/separators are for use in military JP-8 (NATO F-34), Jet A-1 (NATO F-35), F-24 (Jet A++). Required to be tested in fuel containing Stadis 450, DCI-4A, and anti-icing additive Di-EGME. (Note: testing to Category “M” also qualifies for Category “C”.) (Particulates, first stage water removal) and a Monitor (second stage fuel dryer)

Additional Features

• Removable tow bar utilizing a Pintel Hook with quick release

• Parking break with quick release

• Retractable hose reel

• Full length stainless hose guides

• Lockable nozzle, manway and fill port

• Reel mounted bonding / grounding clamps

• Bottom drain / tank sample port

• Pre and post filter fuel quality sample ports

• PPE stowage

• Onboard Spill kit

• Fuel log stowage

• Heavy-duty mobility tie downs

• Fork-lift pockets, both sides

• Lockable top manway and fuel fill port to prevent fuel contamination

• Non-slip side step for access to top of the tank

• Sealed LED Working Lights

• Great Plains Industries (GPI) Aviation Pump and Meter Combo M-3120-AV-

PO/MR 5-30-G8N (MAIN FUELING)

• Great Plains Industries (GPI) Aviation pump and Meter Combo M-3025CB-AV-

PO/MR 5-30-G8N (DEFULEING)

• Two 50 foot long static discharge grounding cables mounted on a retractable reel

• Fuel filter; fuel must be filtered during fueling and defueling operations

• SPR (pressure) nozzle compatible

• 35' Carbon impregnated, static dissipating refueling hose prevent static build-up fuel hose

• Two Velcon VF61 housing, one fitted with a Velcon coalescer/ separated element, P/N: OS-51288; the other fitted with one Velcon element kit, P/N: CK- VF61CDF, and five Velcon monitor elements, P/N: CDF-210

• Automatic Diesel fueling nozzle, Great Plains Industries P/N 110376-01;

connected to fill hose via quick disconnect

• One de-fuel adapter termination in fitting

• One De-Fuel adapter dust cap

• Two 20lbs. “Purple K” fire extinguisher mounted for fast and easy access

• Metal electrical box, grounded and sealed against vapors and weather

• Capable of operating off of 12v stand-alone on-board batteries

• 120v power supply battery charging capability (on board and plug into an outlet)

• PPE stowage

• Onboard Spill kit/ remediation kit

• Two fuel quality sampling ports (Gamomon Technical Products, P/N: gtp-3 or industry equivalent; including plug mounted on lanyard). One port mounted upstream of the filter system and one mounted downstream from the filter system.

• Name Plate adhering to the following standard (each unit will have a permanent nameplate that, will at a minimum, contain the following information in the formatted order)

Description: FUEL/ DEFUEL CART, 250 Gallon Serial Number: XXXX Nominal Capacity US Gallons Tank Material Max Towing Speed

Fuel Pump Specifications

Fueling Pump

Description-

• Minimum 20 gallons per minute (GPM) capable pump that meets NFPA 407 Standard for Aircraft Fuel Servicing, refuel fill rate meter with rated capacity equal to the maximum flow rate of the loading station.

Manufacture Part Number-

• Great Plains Industries (GPI) Aviation Pump and Meter Combo M-3120-AV-PO/MR 5-30-G8N

De-Fueling Pump

Description-

• De-Fuel pump with fill rate meter with rated capacity equal to the maximum flow rate of the loading station.

• 3 Gallon per minute (GPM) 12 amp max draw @ 28v

Manufacture Part Number-

• Great Plains Industries (GPI) Aviation pump and Meter

Combo M-3025CB-AV-PO/MR 5-30-G8N or industry equivalent

Performance Requirements

1. Fueling Rate- Minimum fuel delivery rate must be 8.4 GPM at nozzle for a single 30 minute interval. (8.4 gal/min x 30min= 252 gallons without rest)

2. De-Fueling Rate- Minimum fuel extraction rate is 1.5 GPM at quick-disconnect fitting for a single 25 minute interval (1.5 gal/min x 25min= 37.5)

3. Fuel Meter Accuracy- Accuracy of + or – 2% or better at the minimum fueling rate of 8.4 GPM

4. Filtering Standards- Fuel will be filtered in both operations utilizing Aviation grade, dual stage fuel filtration - required to be Category “M” filter/separators are for use in military JP-8 (NATO F-34), Jet A-1 (NATO F-35), F-24 (Jet A++).

Required to be tested in fuel containing Stadis 450, DCI-4A, and anti-icing additive Di-EGME. (Note: testing to Category “M” also qualifies for Category “C”.)

(Particulates, first stage water removal) and a Monitor (second stage fuel dryer)

Quality Assurance Provisions

Contractor

1. The contractor’s quality system must provide adequate controls to meet all the requirements set forth in the requirement and not supply the United States Army any nonconforming product.

2. Manufacture must provide a Certificate of Conformance.

3. Manufacture must provide a Quality Assurance Worksheet.

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