Attachment_1_KRV Purchase Description (1).docx

PURCHASE DESCRIPTION

TRUCK, AIRCRAFT FUELING-DEFUELING

Commercial Refueler

1. SCOPE. This Purchase Description (PD) covers the general requirements for a commercial aviation refueling truck (herein referred to as the Refueling Vehicle) that will be used for fuel servicing of both military and commercial aircraft.

2. SALIENT CHARACTERISTICS.

2.1 Refueling Vehicle description. The Refueling Vehicle shall be a tank truck that will receive, transport, store, and pump jet fuels in accordance with ASTM D910, ASTM D1655, MIL-DTL-5624, MIL-DTL-25524, MIL-DTL-83133, GOST 10-227, MoD Def Stan 91-91, MoD Def Stan 91-87, ASTM D6615, and ASTM D7566. Excluding the 3% expansion space, the Refueling Vehicle shall have a 5,000 gallon capacity and shall be capable of the following:

a. Issuing fuel to aircrafts at volumetric flow rates of at least 450 gpm and no more than 600 gpm through a filtration system, a flow meter, a primary and secondary pressure control system, a ground servicing hose, and a single point nozzle.

b. Defueling aircraft into the cargo tank through the single point nozzle, ground servicing, the filtration system, and the flow meter at a minimum flow rate of 80 gpm without the assistance of aircraft boost pumps and at flow rates of at least 300 gpm with the assistance of aircraft boost pumps.

c. Bottom loading fuel into the cargo tank at flow rates up to 600 gpm with overfill protection.

2.1.2 Vehicle Warranty.

2.1.2.1 Truck Chassis. The chassis is subject to the warranty period of the original manufacturer.

2.1.2.1.2 Upper Parts (Aircraft Refueling System). Subject to the warranty period of the original manufacturer.

2.2 Design and construction. The design shall promote cost effective, life-cycle sustainability by addressing considerations such as incorporating open standards, reducing pollutant emissions and wastes, and increasing fuel economy, while satisfying system performance requirements. It shall be designed and constructed so that no parts will work loose in service, and to withstand the strains, jars, vibrations, and other conditions incident to shipping, storage, installation, and service. It shall be weatherproof and designed to prevent the intrusion of water, sand, and dust into critical operating components.

2.2.1 Materials, protective coatings, and finish.

2.2.1.1 Protective coatings. Materials that deteriorate when exposed to sunlight, weather, or operational conditions normally encountered during the service life of the item shall not be used or shall have means of protection against such deterioration that does not prevent compliance with the performance requirements specified herein. Protective coatings that chip, crack, or scale with age or extremes of climatic conditions or when exposed to heat shall not be used. Exposed surfaces of fasteners, handles, and fittings shall also be primed and painted

2.2.1.2 Finish. The exterior finish color of the Refueling Vehicle and the inner surfaces of compartments shall be the manufacturer’s standard finish.

2.2.1.3 Exclusion of water. The design of the Refueling Vehicle shall be such as to prevent water leaking into, or being driven into, any part of the Refueling Vehicle interior when either in an operating or travelling configuration. All windows, doors, panels, covers, etc., shall be provided with sealing arrangements such that the entry of water is minimized when these items are correctly closed. Particular care shall be taken to prevent wetting of equipment and heat and sound proofing materials. Sharp corners and recesses shall be avoided so that moisture and solid matter cannot accumulate to initiate localized attack. Sealed floors with suitable drainage shall be provided for storage compartments, engine compartments, and other areas in the Refueling Vehicle that could collect and retain water.

2.2.1.3.1 Fluid traps and faying surfaces. There shall be no fluid traps on the Refueling Vehicle. Faying surfaces of all structural joints, except welded joints, shall be sealed to preclude fluid intrusion.

2.2.1.3.2 Ventilation. Ventilation shall be sufficient to prevent moisture retention and buildup.

2.2.1.3.3 Drainage. Drain holes shall be provided to prevent collection or entrapment of water or other unwanted fluid in areas where exclusion is impractical. All designs shall include considerations for the prevention of water or fluid entrapment and ensure that drain holes are located to effect maximum drainage of accumulated fluids. The number and location of drain holes shall be sufficient to permit drainage of all fluids when the Refueling Vehicle is on a 10-degree longitudinal slope facing both up and down and on a 10-degree side slope in each direction (right and left side facing up the slope). The minimum size of the drain holes shall be 0.375 inch.

2.2.2 Markings. Marked on Sides and Rear in English & Korean (Black Paint):

(1) FLAMMABLE – Marked on both sides, front bumper, and the back of the tank body, stenciled in block letters, 6 inches (152.4 mm) high and shall be of a color contrasting sharply with the sign background for visibility in English and Korean.

(2) NO SMOKING WITHIN 50 FEET – Marked on both sides and the back of the tank body, stenciled in block letters 3 inches (76.2 mm) high and shall be of a color that contrasts with the background for visibility (prefer black) in English and Korean

(3) Gals & Liters – Marked on both outsides and rear of tank with the gallon & filter capacity stenciled in block letters and numbers, 2 inches (50.8mm) high and shall be of a color that contrasts with the background for visibility (prefer black).

(4) International Placard: – Will be posted on all four sides of vehicles

2.2.2.1 Jet fuel product designation shall be marked on each side and the rear of the cargo tank in 6-inch letters. Markings shall be in accordance with the table below unless otherwise noted by the government. Base location will be specified in ordering data (see 6.1).

TABLE I. Product markings.

2.2.3 Identification and information plates.

2.2.3.1 Identification plate. An identification plate in accordance with MIL‑STD‑130 shall be securely attached to the Refueling Vehicle in a readily accessible location. The Refueling Vehicle and any of its components for which the Government’s unit cost is more than $5,000, is serially managed, or the procuring agency determines is mission essential, shall have Unique Identification (UID) (also known as Item Unique Identification (IUID)) information permanently affixed on or near the respective identification plate(s), marked in accordance with MIL‑STD‑130. UID information shall be included as both a 2D Data Matrix and human readable markings. The identification plate shall contain the following information:

a. Nomenclature

b. Air Force vehicle registration number

c. Part number

d. Serial number

e. Date of manufacture

f. Contract number

g. Manufacturer’s name

h. Manufacturer’s address and phone number

i. Commercial and Government Entity (CAGE) code

j. Date of warranty expiration (if applicable)

k. National Stock Number (NSN)

l. Vehicle weight, unloaded (pounds)

m. Gross vehicle weight (pounds)

n. Engine fuel type

o. Engine oil viscosities for ambient temperatures ranging from -40°F to +125°F

p. Cargo tank capacity (gallons)

2.2.3.2 Transportation data plate. A transportation data plate shall be securely attached to the Refueling Vehicle in a readily accessible location. The plate shall contain at least the following information:

a. Side and rear silhouette views of the Refueling Vehicle.

b. Horizontal and vertical location of the center of gravity of the Refueling Vehicle marked on the silhouette views.

c. Shipping weight.

d. Loading cubage.

e. Overall height, width, and length.

f. Front and rear axle loads.

g. Tie down information.

2.2.3.3 Lubrication data plate. The Refueling Vehicle shall be provided with a permanently marked lubrication data plate constructed of a non-corroding metal, mounted on the exterior surface of the Refueling Vehicle that shall direct attention to all lubrication fittings and components that require lubrication. The plate shall identify the type and grade of lubricant required.

2.2.4 Environment, Safety, and Occupational Health (ESOH).

2.2.4.1 Component protection. All space in which work is performed during operation, service, and maintenance shall be free of hazardous protrusions, sharp edges, or other features which may cause injury to personnel. All rotating and reciprocating parts and all parts subject to high operational temperatures or subject to being electrically energized, that are of such nature or so located as to be hazardous to personnel, shall be guarded or insulated to eliminate the hazard. All wires, cables, tubes, and hoses shall be supported and protected to minimize chafing and abrasion and shall be located so as to provide adequate clearance from moving parts and high operational temperatures. Grommets shall be provided wherever wires, cables, tubes, or hoses pass through bulkheads, partitions, or structural members.

2.2.4.2 Foreign object damage (FOD). All loose metal parts, such as pins or connector covers, shall be securely attached to the Refueling Vehicle with wire ropes or chains. “Dog tag" style beaded chains shall not be provided. Removable panels, if provided, shall be attached with captive fasteners. Tire valve stem caps shall be made of plastic.

2.2.4.3 Fire extinguisher. Two Type I, Class 2, Size 20 fire extinguishers, in accordance with A-A-393, shall be installed, one on each side of the truck. The fire extinguishers shall be accessible to personnel standing on the ground and shall be protected from tire splash.

2.2.4.4 Electrostatic discharge (ESD). The design of the Refueling Vehicle shall preclude equipment damage due to ESD, protect personnel from electrical shock due to static charging, and prevent ignition of explosive atmospheres due to sparking.

2.2.4.5 Grounding cables and reels. Two Type I, spring rewind, grounding reels with cables and cable guides shall be installed side by side on the driver’s side of the truck. The reels and cables shall be in accordance with A-A-50696. One cable shall have a welder style clamp, and the other cable shall have a grounding plug. The cables shall have cable stops to prevent the clip or plug from striking the cable guide. The cables shall be electrically bonded to the tanker chassis frame.

2.2.6 Cargo tank and related components.

2.2.6.1 Cargo tank. The Refueling Vehicle shall have single compartment cargo tank with a capacity of 5,000 gallons plus a minimum three percent expansion space. The cargo tank shall be in accordance with all requirements of NFPA 385, NFPA 407, and 49CFR178.346 (DOT 406). The cargo tank shall be constructed of aluminum. There shall be no metal-to-metal contact between the tank mounting brackets and the truck chassis mounting brackets.

2.2.6.2 Tank inventory management system (TIMS). The cargo tank shall have a tank inventory measuring system installed. The TIMS shall have a LED digital display that is readable from a distance of 15 feet during daytime or nighttime operations. Tank inventory shall be displayed in gallons.

2.2.6.3 Bottom loading system. The bottom loading system shall be capable of filling the cargo tank from a pressurized fuel source through a single point receptacle with the engine off. The system shall accept fuel flow up to 600 gpm.

2.2.6.4 Bottom loading internal valve. An air-operated bottom loading internal valve shall be interlocked so that it only opens after the truck parking brakes are set and the automatic vent system is open. The bottom loading internal valve shall automatically activate when a single point nozzle is connected to the bottom loading inlet receptacle. The valve must be equipped with a fusible link or a plug that closes the valve in the event of a fire.

2.2.6.5 Overfill prevention system. A dual, independent, automatic overfill prevention system shall be installed to stop fuel flow during bottom loading and defueling operations. The system used shall be a Scully Load Anywhere System or equivalent. The system shall be compatible with Scully ST-15 single point overfill prevention control unit, Scully Intelliltrol 2, or an equivalent system that uses a dual socket adapter and includes a pretest momentary-on push button located on the bottom loader control panel for test verification of the tank-level sensor. The socket adapter shall be equipped with ground verification.

2.2.6.6 High level sensor. The high-level sensor used for the overfill prevention system shall be a mechanical jet level sensor.

2.2.6.6.1 Overfill prevention system override. A mechanical, momentary-on, push button shall be used to temporarily disable the overfill prevention system in order to allow for recirculation or gravity discharge of fuel if the high-level sensor is wet. The override shall be located near the bottom loading inlet and protected with a tamper proof cover that can be secured with a padlock. The padlock will be installed by the government upon receipt.

2.2.6.7 Cargo tank water drain. The water sump on the cargo tank shall have a 1-inch minimum self-closing drain valve. The drain valve shall be directed toward the ground, guarded from damage, accessible without crawling under the tank, and designed to prevent fuel contact with the operator.

2.2.6.8 Cargo tank vent system. The cargo tank vent system shall be a two-part system. The primary system shall be an automatic vent system. The automatic vent system shall be interlocked and fail-safe during refueling, defueling, and bottom loading operations so that flow cannot commence unless the vent(s) are fully open. The automatic vent system shall be sized for a cargo tank fill rate of 600 gpm and a single-point nozzle discharge rate of at least 450 and no more than 600 gpm. The secondary system shall be an emergency vent in accordance with 49CFR178 (DOT 406).

2.2.7 Pumping System.

2.2.7.1 Piping. All piping shall be aluminum or stainless steel with a minimum 150 psi working pressure.

2.2.7.2 Pump. The pump shall be a self-priming, centrifugal, aviation fuel dispensing pump. The pump shall be driven directly or hydraulically by the truck transmission PTO or by a split shaft gear box. A bypass system or relief valve shall be provided to protect the pump.

2.2.7.3 Pump inlet strainer. An in-line Y-style strainer shall be installed in the piping between the tank suction header and the pump. The strainer shall have a serviceable 10 to 20 mesh screen that is rated for flow of at least 450 and no more than 600 gpm. The strainer shall be positioned in an easily accessible location for servicing.

2.2.7.4 Pump maintenance shutoff valve. A pump maintenance shutoff valve shall be located both upstream and downstream of the pump. There shall be no devices, branch connections, or bypass/relief connections between the shutoff valves and the pump. The valves shall be a manual, quarter turn design and shall be operable while standing or kneeling on the left or right side of the truck.

2.2.7.5 Flow meter. All fuel flow through the pumping system shall be metered through a temperature compensated flow meter. The flow meter shall have a resettable totalizer capable of displaying the amount of fuel delivered in gallons. The flow meter shall be capable of capturing flow during both fueling and defueling operations.

2.2.7.6 Pressure control system. The pressure control system shall consist of an independent primary and secondary pressure control system. The pressure control system shall limit the single point nozzle pressure to a maximum peak surge pressure of 120 psi during a complete aircraft fueling operation. Valve(s) closure shall occur in a maximum timeframe of two seconds. Any surge pressure developed shall not exceed the pressure rating of any single component in the Refueling Vehicle pumping system. The pressure control system shall include a pump bypass system or a relief valve. The pressure control system shall sense the single point nozzle pressure through a pressure sensing type component that consistently and repeatedly simulates the fuel pressure at the single point nozzle. Locked in pressure at the single point nozzle shall not exceed 55 psi for more than 15 seconds after flow stops. The system shall resume from an induced no-flow condition to primary pressure control system-controlled flow within 15 seconds by disengaging and then re-engaging the dead man.

2.2.7.6.1 Primary pressure control system. The primary pressure control system shall be set to control and limit the single-point nozzle pressure 50 ± 5 psi using a pressure control valve.

2.2.7.6.2 Secondary pressure control system. The secondary pressure control system shall be set to control and limit the single-point nozzle pressure to a maximum of 55 psi if the primary pressure control system should fail. The secondary pressure control system shall be a hose end pressure control valve.

2.2.8 Filtration System. The filtration system shall be rated for a minimum of 450 and no more than 600 gpm and 150 psi. The filter vessel and elements shall be qualified in accordance with the requirements of EI-1581 Specification and Qualification Procedures for Aviation Jet Fuel Filter Separators, Category M, Type S, Two Stage system configuration.

2.2.8.1 Filter vessel water drain. The water sump on the filter vessel shall be equipped with a one inch manually operable ball-type valve with a spring return handle that renders the valve normally closed. The drain valve shall be directed toward the ground, guarded from damage, accessible without crawling under the truck, and designed to prevent fuel contact with the operator.

2.2.8.2 Filter vessel maintenance shutoff valve. A filter vessel maintenance shutoff valve shall be located both upstream and downstream of the filter vessel. There shall be no devices, branch connections, or bypass/relief connections between the shutoff valves and the filter vessel. The valves shall be a manual, quarter turn design and shall be operable while standing or kneeling on the left or right side of the truck.

2.2.8.3 Differential pressure gauge. A non-calibrating differential pressure gauge shall be installed to continuously monitor the pressure drop across the filter coalesce stage during operation. The gauge shall register and hold the highest pressure drop achieved during operation. The gauge shall be resettable.

2.2.8.4 Fuel sampling. A fuel sampling valve shall be provided downstream of the filtration system and prior to the flow meter. The valve shall be easily accessible while standing at the operator control panel.

2.2.9 Hose assemblies.

2.2.9.1 Underwing hose. One 2” x 50’ aviation fueling hose shall be provided for underwing fueling operations.

2.2.9.2 Underwing hose reel. One single wrap hose reel sized for 2 ½” x 50’ hose shall be provided. The reel shall have explosion proof electric rewind motor and switch with an auxiliary manual rewind.

2.2.9.3 Underwing nozzle. The underwing nozzle shall be D-3 universal single point nozzle. The nozzle shall have a 60 mesh stainless steel strainer and an automatic vacuum breaker.

2.2.9.4 Overwing hose. 1 ½” x 50’ aviation fueling hose shall be provided for overwing fueling operations.

2.2.9.5 Overwing hose reel. One single wrap hose reel sized for 1 ½” x 50’ hose shall be provided. The reel shall have explosion proof electric rewind motor and switch with an auxiliary manual rewind.

2.2.9.6 Overwing nozzle. The overwing nozzle shall be a type I, size 2, class B, style 2 nozzle in accordance with A-A-52030 (such as an OPW model 295AF nozzle or equivalent). The overwing nozzle shall have a 100 or 60 mesh stainless steel strainer and the grounding wires shall be jacketed.

2.2.10 Night servicing lights. Two adjustable, vapor proof, service lights shall be installed to facilitate nighttime operations. One light shall be installed at the near the pumping compartment on the driver’s side. The other light shall be installed at the rear of the cargo tank on the driver’s side. The lights shall be approximately eight feet above the ground. Each light shall have its own on/off switch and be adjustable by a control handle that is within reach of a person standing on the ground. The combined light levels of these two lights shall illuminate the entire side of the vehicle.

2.2.11 Accessory lighting. Adequate lighting shall be provided at the control panel, bottom loading interface, and filter separator to facilitate nighttime operations.

2.5 Transportability.

2.5.1 Surface transportability. The Refueling Vehicle shall be transportable via all modes of surface shipment (highway, rail, and water) in accordance with MIL‑STD‑1366, and shall be capable of withstanding the mechanical shock and vibration characteristics of highway, rail, and water transport, except that design for rail impact testing (see 5.2.5 of MIL‑STD‑1366) is not required.

2.6 Maintainability.

2.6.1 Special tools. The design of the item shall minimize the requirement for special tools. All special tools shall be provided with, and stored on, the Refueling Vehicle.

2.6.2 Diagnostic software. A copy of any diagnostic software required or recommended for maintaining the Refueling Vehicle shall be provided with each Refueling Vehicle on CD‑ROM or DVD‑ROM.

2.7 Performance.

2.7.1 Underwing fuel servicing. When conducting underwing fuel servicing operations, the primary pressure control system shall maximize flow rate into the aircraft while limiting the single point nozzle pressure to no more than 50 ± 5 psi. There shall also be an independent secondary pressure control system that will limit the nozzle pressure to 55 psi. In the event that the secondary pressure control system is activated, fuel flow shall continue. Stopping the fuel flow is not an acceptable secondary pressure control system. When operating in this mode, the pumping system shall be capable of issuing fuel to an aircraft from the cargo tank, through the filtration system, the flow meter, ground servicing hose, and the single point nozzle at a flow rate of at least 450 and no more than 600 gpm.

2.7.2 Overwing fuel servicing. When conducting overwing fuel servicing operations, the throttle controller and overwing nozzle shall be used to control both flow rate and nozzle pressure. The pumping system shall be capable of delivering fuel at rates up to 100 gpm.

2.7.3 Defueling. When conducting defueling operations, the flow rate shall be maximized while preventing pump suction pressure from dropping below that required to maintain adequate NPSH. With the fuel level height at 10 feet above the ground, the pumping system shall be capable of defueling fuel from an aircraft through the single-point nozzle and hose, the filtration system, the flow meter, and into the cargo tank at a flow rate of at least 80 gpm without the assistance of aircraft boost pumps and at least 300 gpm with the assistance of aircraft boost pumps. Both hoses shall be capable of performing defueling operations.

2.7.4 Bottom loading. When bottom loading, the refueling vehicle shall be capable of filling the cargo tank from a pressurized fuel source through a single point receptacle at flow rates up to 600 gpm with the truck engine off.

2.7.5 Recirculation. When recirculating, the pumping system shall recirculate fuel form the cargo tank through the filtration system, flow meter, and internal piping and then back into the cargo tank. Recirculation shall not use the servicing hoses. The fuel flow rate shall be controlled by the throttle controller. The control system shall not allow recirculation if the high-level sensor is wet.

2.8 Mobility.

2.8.1 Transmission. The Refueling Vehicle shall be equipped with an automatic transmission which shall include a hydraulic torque converter and not less than five forward gear ratios. The net torque capacity and the net power rating of the transmission shall exceed the output ratings of the engine.

2.8.2 Axles. The Refueling Vehicle shall be equipped with axles rated at least equal to the load imposed on each axle, measured at the ground, with the Refueling Vehicle loaded to its GVWR.

2.8.3 Suspension. The Refueling Vehicle shall be equipped with a suspension system with components having a rated capacity at least equal to the load imposed on each member, measured at the ground, with the Refueling Vehicle loaded to its GVWR.

2.8.4 Steering. The Refueling Vehicle shall be equipped with a power assisted steering system, with manual steering available in the event of power assist failure.

2.8.5 Brakes. The Refueling Vehicle shall be equipped with an air brake system. A brake override shall be provided for maintenance or towing applications.

2.8.6 Spare tire and wheel assembly. When specified (see 4.1), a spare tire and wheel assembly (the tire mounted on the wheel) shall be shipped with the Refueling Vehicle; the wheel and tire shall be identical to the others provided. The assembly shall be securely stowed so that it does not come loose during transport.

2.8.7 Spare wheel. When specified (see 4.1), a spare wheel shall be shipped with the Refueling Vehicle; the wheel shall be identical to the others provided. The wheel shall be securely stowed so that it does not come loose during transport.

2.8.8 Engine. The Refueling Vehicle shall be equipped with a diesel engine.

2.9 Technical data.

2.9.1 Manufacturer’s publications. The contractor shall furnish all manufacturer’s publications listed in this paragraph, in Indexed Portable Document Format (IPDF).

2.9.1.1. Electronic Deliverable on Disc (CLIN 0002). The contractor shall deliver one digital copy of all manufacturer’s publications on a disc, listed below in paragraph 2.9.1.1.1 a. through g. The disc shall be furnished to 7AF/A4 30 days prior to the first hardware delivery, at the address located in paragraph 2.9.1.2 below. All manuals shall be delivered with either unlimited data rights or as a minimum, a Government Purpose License, to allow the Air Force to electronically store, print, distribute and update the manual.

2.9.1.1.1 Deliverable for Each Vehicle (CLIN 0002). The contractor shall also deliver one digital copy (on a disc) and one printed, paper copy per vehicle, in both Hangul and English. This deliverable shall be delivered with each vehicle.

Manufacturer’s Publications (digital and printed/paper copy)

0. Certificate of manufacturer for each truck specifying USAF as the vehicle’s owner and temporary license plates at the time of delivery.

0. Operator’s Manual with lubrication charts for tanker body and equipment.

0. Detailed Operational, Maintenance, and Illustrated Parts Breakdown (IPB) for the engine, transmission, and chassis.

0. IPB for tanker body and equipment including power takeoff (PTO).

0. Tanker Shop Maintenance, Service & Repair Manual. This manual shall contain information regarding diagnosis, servicing techniques, disassembly, repair and assembly procedures for the Tanker Body and associated equipment.

0. The contractor shall prepare Service Bulletins as required to notify the government of new maintenance problems and/or procedures to be implemented on the contractor’s equipment prior to the issuance of permanent changes to the technical manuals. Service bulletins shall also be prepared when the program office has identified a trend of a potential problem or failure that has occurred at field level. The Service Bulletins shall identify any potential safety hazards. Service Bulletins shall be submitted in Indexed Portable Document Format (IPDF).

0. SAFETY. New trucks shall comply with Korean domestic safety and exhaust emission control requirements.

2.9.1.2 Manufacturer’s Publications Deliverable Mailing Address (CLIN 0002). In accordance with paragraph 2.9.1.1, the electronic/digital copy (on disc) of the manufacturer’s publications shall be sent to the following address:

7 AF/A4L

군우 2047

APO AP 96278-2047

OR

English Address:

7 AF/A4L

Unit 2047

APO AP 96278-2047

2.10 Physical Address for Vehicle Delivery (CLIN 0001). The vehicles shall be delivered to the following addresses :

FB5294 51 LRS LGRDDC

CP 011-82-505-784-5085

오산AB빌딩 신장동 824호

평택시 KR 17759

English Address:

FB5294 51 LRS LGRDDC

CP 011-82-505-784-5085

OSAN AB BLDG 824 SINJANG DONG

PYEONGTAEK CITY KR 17759

FB5284 제8 물류지원비행대대 수송운영과

군산 공군기지 823번 건물 수령과 전라북도 군산시 45-54 164

FB5284 8 LRS LGRD

KUNSAN AB BLDG 823 RCVG SECT

GUNSAN CITY 45 54 164

English Address

FB5232 607 MMS LGS OL A

MF GWANGJU CP 011 82 62 940 6899

GAWANG JU AB BLDG 1204 GWANGSAN GU

GWANG JU CITY KR 62376

Hongul Address

FB5232 607 MMS LGS OL A

광주AB, 빌딩 1204, 광산구

광주광역시, 대한민국 62376

Daegu:

FB5230 607 MMS LGS

CP 011 82 53 980 4174

DAEGU K2 AB BLDG 3571 DONG GU

DAEGU CITY KR 41052

FB5230 607 MMS LGS

CP 011 82 53 980 4174

대구 K2 AB, 빌딩 3571, 동구,

대구광역시, 대한민국 41052

Suwon:

FB5261 607 MMS LGS OL B

MF SUWON CP 011 82 31 220 4992

SUWON AB BLDG 2214 GYEONGGIDO

SUWON CITY KR 16659

FB5261 607 MMS LGS OL B

MF SUWON CP 011 82 31 220 4992

수원 AB, 빌딩 2214, 경기도

수원특례시, KR 16659

Gimhae:

FB5213 607 MMS LGS OL D

MF GIMHAE CP 011 82 51 979 4204

GIMHAE AB BLDG 2001

GANGSEO GU BUSAN KR 46719

FB5213 607 MMS LGS OL D

MF GIMHAE CP 011 82 51 979 4204

김해 AB, 빌딩 2001,

강서구, 부산광역시, 대한민국 46719

2.10.1 Points of Contact for Vehicle Delivery (CLIN 0001).

SMSgt Jay Pickle – email address: jay.pickle@us.af.mil SMSgt Chris Macfadden – email address: christopher.macfadden@us.af.mil MSgt Marshall Thompson – email address: marshall.thompson.2@us.af.mil MSgt Cade Browning – email address: cade.browning@us.af.mil MSgt Michael Natalello – email address: michael.natalello@us.af.mil Org Box – email address: 7AF.A4R.SUPPLY@us.af.mil

2.11 Cleaning. The Refueling Vehicle shall be thoroughly cleaned. Loose, spattered, or excess solder; welding slag; stray bolts, nuts, and washers; rust; metal particles; pipe compound; and other foreign matter shall be removed during and after final assembly.

3. PACKAGING. Preservation, packing, and marking shall be as specified in the contract or order.

4. NOTES.

4.1 Ordering data. Acquisition documents should specify the following:

a. Title, number, and date of this CID.

b. If a spare tire and wheel assembly is required (see 2.8.6).

c. If a spare wheel is required (see 2.8.7).

OPSEC and AT Statement:

5. Anti-terrorism (AT) statement: The contractor’s personnel or any representative of the contractor entering installation/base shall abide by all security regulations imposed by installation commander or base commander at all times and shall be subject to security checks. The contractor’s personnel and property shall be subjected to search and seizure upon entering the confines of the installation/base, while on, and upon leaving confines of the installation/base.

5.1. AT Level I Training: The contractor employees, to include sub-contractor employees, requiring access Air Force installations, facilities, and controlled access areas may be required to complete AT Level I Awareness training within thirty (30) calendar days after contract start date or effective date of incorporation of this requirement into the contract, whichever is applicable. In that case, the contractor shall submit certificates of completion for each affected contractor employee and subcontractor employee, to the COR within five (5) calendar days after completion of training by all employees and sub-contractor personnel.

5.1.1. Access and General Protection/Security Policy and Procedures: The contractor and all associated sub-contractor employees shall provide all information required for background checks to meet installation access requirements. The contractor workforce must comply with all personal identity verification requirements (FAR clause 52.204-9, Personal Identity Verification of Contractor Personnel). In addition to the changes otherwise authorized by the changes clause of this contract, should the Force Protection Condition (FPCON) at any individual facility or installation change, the Government may require changes in contractor security matters or processes.

5.1.2. For contractors that do not require CAC, but require access to a DoD facility or installation: The contractor and all associated sub-contractor employees shall comply with adjudication standards and procedures using the National Crime Information Center Interstate Identification Index (NCIC-III) and Terrorist Screening Database (Army Directive 2014-05/AR 190-13), applicable installation, facility and area commander installation/facility access and local security policies and procedures (provided by the Government representative); or, at OCONUS locations, in accordance with status of forces agreements and other theater regulations.

5.1.3. iWATCH Training: The contractor and all associated sub-contractors may be required to brief all employees on the local iWATCH program (training standards provided by the requiring activity ATO). This local developed training will be used to inform employees of the types of behavior to watch for and instruct employees to report suspicious activity to the COR. In case when iWATCH Training is required, this training shall be completed within thirty (30) calendar days of contract award and within five (5) calendar days of new employees commencing performance with the results reported to the COR no later than thirty (30) calendar days after contract award.

5.1.4. For Contracts that Require OPSEC Training: Per AR 530-1, Operation Security, the contractor employees may be required to complete Level I OPSEC Awareness training. In that case, new employees must be trained within thirty (30) calendar days of their reporting for duty and annually thereafter. The contractor and all associated sub-contractors will practice Operations Security. The contractor shall not talk about work outside of the work area nor discuss the work being performed on social media. The contractor shall not take pictures/videos (to include operation of dashcams or other recording devices in contractor operated vehicles) inside sensitive locations without prior coordination with the organization’s OPSEC representative and contracting officer representative. It will be the responsibility of the contractor to safeguard all documents provided. Documents will be stored away from view when not being used. Documents, media, drawings, and other associated material that are no longer needed must be destroyed via approved methods.

5.1.5. For Contract Requiring Performance or Delivery in a Foreign Country: DFARS Clause 252.225-7043, Antiterrorism/Force Protection for Defense Contractors Outside the US. The clause may be used in solicitations and contracts that require performance or delivery in a foreign country. This clause applies to both contingencies and non-contingency support. The key AT requirement is for non-local national contractor personnel to comply with theater clearance requirements and allows the combatant commander to exercise oversight to ensure the contractor’s compliance with combatant commander and subordinate task force commander policies and directives.

5.1.6. Controlled Unclassified Information (CUI): The contractor is required to comply with NIST 800-171 based on DFARS clause 252.204-7012. Also DFARS provision 252.204-2019 may be included into solicitation with which the contractor is required to comply.

5.1.7. Threat Awareness Reporting Program: For all contractors with security clearance, per AR 381-12 Threat Awareness and Reporting Program (TARP), the contractor employees may be required to receive annual TARP training by a CI agent or other trainer.

5.2. OPSEC statement: The contractor and all associated sub-contractors will practice Operations Security. The contractor shall not talk about work outside of the work area nor discuss the work being performed on social media. The contractor shall not take pictures/videos (to include operation of dashcams or other recording devices in contractor operated vehicles) inside sensitive locations without prior coordination with the organization’s OPSEC representative and contracting officer representative. It will be the responsibility of the contractor to safeguard all documents provided. Documents will be stored away from view when not being used. Documents, media, drawings, and other associated material that are no longer needed must be destroyed via approved methods.