N68335-16-R-0172_Solicitation_released_6-29-2016.docx

N68335-16-R-0172

Section A - Solicitation/Contract Form

PROCUREMENT INFORMATION

Government Contract Department Point of Contact:

Ms. Shannan Germond Contract Specialist Phone: (732) 323-2778 E-Mail: Shannan.Germond@navy.mil

1. This solicitation is a 100% Small Business Set-Aside per FAR 52.219-6.

2. The purpose of this contract action is for the manufacturing, installation, start-up, documentation, and warranty of two (2) Combined Temperature/Altitude/Humidity/Vibration Environmental Test (CET) Chambers.

3. It is anticipated that this will be a Firm Fixed Price (FFP) type contract.

4. IMPORTANT INFORMATION: Registration in the Department of Defense DoD System for Award Management (SAM) database will be a prerequisite for receiving an award. For more information on the SAM, refer to the SAM website at https://www.sam.gov/portal/public/SAM.

5. Proposal Validity shall be for 180 days or longer as annotated by the Offeror in Block 12 of the cover page of the SF33.

Section B - Supplies or Services and Prices

CET Chamber

FFP

Two (2) Combined Environmental Test Chambers designed, built, and delivered in accordance with the Statement of Work in Section C.

FOB: Destination

NET AMT

Lot

Technical Data

FFP

Contract Data Requirements List A002, A004, A005, A007 and A008.

NET AMT

Section C - Descriptions and Specifications

STATEMENT OF WORK - 22 MAR 16

DESCRIPTION/SPECIFICATION/STATEMENT OF WORK

1. BACKGROUND

The Naval Air Warfare Center - Aircraft Division (NAWCAD) has a requirement to procure two (2) CET Chambers in the Electrical Test Operations & Maintenance (ETO&M) Branch Laboratory. The ETO&M Branch Laboratory is a testing facility which consists of numerous test areas that are designed to evaluate electrical power generation, battery and power conversion systems, electrical power distribution systems, electrical power quality, electrical starting and emergency electrical power and avionics systems under simulated flight conditions. A Test Control Cell (TCC) is a centrally located control room in the ETO&M Branch Laboratory that test operators monitor and remotely control numerous laboratory operations including the CET Chambers.

The CET Chambers will be utilized to provide controlled environments during testing of Naval aircraft/shipboard/ground electrical, avionic or mechanical components and systems. The predominant test methods will come from MIL-STD-810, MIL-HDBK-781, and MDC A4241 for combined temperature, altitude, humidity, and vibration environments. The results of the testing will be used for Naval reliability, qualification, safety of flight, flight worthiness, and evaluation programs. With the use of the ETO&M branch electrical bus-ways along with the CET Chambers, full aircraft simulations can be used to assess thermal, mechanical, and electrical synergetic stresses on both legacy and new technologies.

2. SCOPE

2.1 The contractor shall provide for manufacturing, delivery, installation, start-up, documentation, and warranty of two (2) CET Chambers and all ancillary equipment required as detailed in this statement of work.

CLIN 0001 – CET CHAMBER – QUANTITY 2

The CET Chamber shall meet all minimum requirements as follows:

3. CET CHAMBER TECHNICAL REQUIREMENTS

3.1 Controlled Chamber Parameters

3.1.1 The chamber shall simultaneously control the temperature, pressure altitude, humidity, vibration and conditioned air flow and temperature.

3.1.2 Ambient Temperatures

3.1.2.1 The Chamber shall utilize a minimum of two control thermocouples; one for ambient air and one for blast air.

3.1.2.2 The Chamber shall utilize a minimum of two thermocouples for high temperature safety limiters.

3.1.2.3 The Chamber shall utilize a minimum of six thermocouples for unit under test response temperature monitoring.

3.1.2.4 The Chamber shall control the temperature between -70.0°C and 150.0°C.

3.1.2.4.1 Temperature transients shall be applicable between site altitude and 65,000 feet altitude.

3.1.2.4.2 Temperature Tolerance

3.1.2.4.2.1 The temperature (return air) shall be controlled within a tolerance of plus or minus 1.0°C under steady state conditions (after the set point temperature is attained with no control changes).

3.1.2.4.3 Temperature Rate of Change

3.1.2.4.3.1 The chamber shall change the temperature between -65.0°C and 80.0°C. at a rate of 11.5°C/minute minimum for heating and 10.0°C /minute minimum for cooling. Requirement 3.1.2.4.4.1 is not applicable when blast air is being supplied into the chamber.

3.1.2.5 Mass and Live Load Capacity

3.1.2.5.1 The chamber shall meet requirement 3.1.2.4.3 when a continuous heat load of 2,000 watts is being dissipated into the chamber from the unit under test and a mass load of 500 pounds of aluminum.

3.1.3 Pressure Altitude

3.1.3.1 The chamber shall control the pressure altitude between site altitude and 80,000 feet.

3.1.3.2 The chamber shall control the pressure altitude between site altitude and 65,000 feet with the full 5.0 pounds/minute mass flow rate entering the chamber.

3.1.3.2.1 Pressure Tolerance

3.1.3.2.1.1 Under steady state conditions (set point is attained with no control changes), the pressure altitude shall be controlled within the tolerances listed below.

3.1.3.2.1.1.1 0 to 20,000 feet altitude: +/- 200 feet

3.1.3.2.1.1.2 20,000 to 50,000 feet altitude: +/- 500 feet

3.1.3.2.1.1.3 50,000 to 80,000 feet altitude: +/- 1,000 feet

3.1.3.2.2 Pressure Altitude Rate of Change

3.1.3.2.2.1 The chamber shall change the pressure altitude (increasing or decreasing) between:

3.1.3.2.2.1.1 Site pressure and 50,000 feet in a minimum of 5 minutes (nominal 10,000 feet/minute)

3.1.3.2.2.1.2 Between 50,000 and 80,000 feet in a minimum of 10 minutes (nominal 5,000 feet/minute)

3.1.3.2.2.2 Requirement 3.1.3.2.2 is not applicable when blast air is being supplied into the chamber.

3.1.3.2.3 Pressure Relief Valve

3.1.3.2.3.1 The chamber shall incorporate a manual pressure relief valve to vent the chamber to site pressure.

3.1.4 Humidity

3.1.4.1 The chamber shall control the humidity between 20% and 95% relative humidity (RH) as limited by a 4.5°C minimum dew point and a maximum dry bulb temperature of 85°C.

3.1.4.2 Humidity operation shall be applicable at site pressure only and shall be capable of being locked out during operation at altitude. Requirement 3.1.4 is not applicable when blast air or altitude is being supplied into the chamber.

3.1.4.3 The Chamber shall not allow condensation to drip onto the test space volume as identified in Section 3.2.4.1.

3.1.4.4 Humidity Tolerance

3.1.4.4.1 The humidity shall be controlled within a tolerance of plus or minus 3% RH under steady state conditions (after the set point humidity is attained with no control changes).

3.1.4.5 Humidity Rate of Change

3.1.4.5.1.1 The chamber shall change the humidity (increasing or decreasing) between 20% and 95% RH in a minimum of 1 hour.

3.1.4.5.2 Humidity Measurement

3.1.4.5.2.1 A direct readout sensor shall be used to measure humidity.

3.1.4.5.2.1.1 A dry/wet bulb shall not be used to measure humidity.

3.1.4.5.2.2 The sensor shall operate over the required temperature range for humidity control and shall not be degraded or damaged throughout the operating temperature and pressure altitude range of the chamber.

3.1.5 Conditioned Air Supply (Blast Air)

3.1.5.1 An independent air supply temperature and flow system shall be provided to condition Government provided air up to 5 pounds/minute.

3.1.5.2 Cooling shall be provided with mechanical refrigeration.

3.1.5.3 The blast air shall be accessible in the chamber by a two (2) inch pipe.

3.1.5.3.1 The two (2) inch blast air pipe shall protrude into the chamber test area no more than six (6) inches.

3.1.5.4 Temperature Range

3.1.5.4.1.1 The blast air system shall control the temperature of the outlet air in the chamber between -65°C to +85°C.

3.1.5.4.2 Temperature Tolerance

3.1.5.4.2.1 The blast air system shall control the temperature of the outlet air to within plus or minus 2°C.

3.1.5.4.3 Temperature Ramp Rate

3.1.5.4.3.1 The blast air system shall be designed with split cooling and heating loops to allow rapid transients of blast air temperature.

3.1.5.4.3.1.1 The Government supplied air shall be routed to one or both loops dependent on the temperature set-point and recombined prior to entering the chamber.

3.1.5.4.3.2 The blast air system shall be capable of ramping temperature across the full range of -65°C to +85°C at a minimum rate of 82°C/minute limited by the piping temperature prior to the temperature transient.

3.1.5.4.3.3 The blast air system shall have an adjustable temperature limiter on the heating elements.

3.1.5.4.4 Flow Range

3.1.5.4.4.1 The blast air flow rate shall be controllable from 0.5 pounds/minute to 5.0 pounds/minute.

3.1.5.4.5 Flow Tolerance

3.1.5.4.5.1 The blast air system shall control flow to plus or minus 0.2 pounds/minute

3.1.6 Vibration System

3.1.6.1 The vibration system shall include an electro-dynamic shaker and amplifier.

3.1.6.2 The shaker shall not be adversely affected by the temperature, altitude, and moisture conditions generated within the chamber work space.

3.1.6.3 Shaker Interface (Seal)

3.1.6.3.1 The shaker interface (seal) between the shaker head and the chamber floor shall be designed for pressure differentials associated with the altitude conditions specified in section 3.1.3.1.

3.1.6.3.2 The shaker interface connections on the shaker and the chamber floor shall be accessible and designed for ease of maintenance.

3.1.6.3.3 The shaker interface shall be designed to endure long reliability tests of up to 6 months without the need of replacement or maintenance.

3.1.6.3.4 The shaker interface materials shall not be adversely affected by the temperature, altitude, vibration, and moisture conditions generated within the chamber work space.

3.1.6.3.5 The shaker interface shall not degrade performance of the vibration system identified in section 3.1.6.5.

3.1.6.4 The vibration system shall be compatible with a Government provided Vibration Research Inc., Model VR 9500 Controller.

3.1.6.5 Vibration System Performance

3.1.6.5.1 The vibration system shall be capable of continuous duty at full rated output except where limited by displacement and/or velocity.

3.1.6.5.2 The vibration system shall consist of an electro-dynamic shaker with a usable minimum force rating of 12,000 pounds force peak and 10,000 pounds force Root Mean Square (RMS) accounting for any extensions or interface seal weight.

3.1.6.5.3 Frequency Range

3.1.6.5.3.1 The vibration system frequency range shall be 5 to 2,000Hz at a minimum in sine, random and sine-on-random modes of operation.

3.1.6.5.4 Displacement

3.1.6.5.4.1 The displacement of the vibration system shall be a minimum of 2 inches peak-to-peak.

3.1.6.5.5 The shaker armature shall remain centered to utilize the full peak to peak displacement throughout the entire altitude range identified in section 3.1.3.1 and accounting for up to the maximum Payload Weight in section 3.1.6.5.10.

3.1.6.5.6 System Hum and Noise

3.1.6.5.6.1 The vibration system hum and noise shall be less than 0.1 Root Mean Square Acceleration (grms).

3.1.6.5.7 Shaker Head Mounting Surface

3.1.6.5.7.1 The mounting surface shall be a minimum of 24 inches in diameter.

3.1.6.5.7.2 The mounting surface shall include 25 each, 0.50 inch stainless steel, 13 internally threaded standoffs for specimen and fixture mounting

3.1.6.5.7.3 The configuration shall be 24, 16, 8 inch diameter bolt circles and shaker head mounting surface center. Spacing between threaded standoffs shall be 45 degrees.

3.1.6.5.8 Isolation

3.1.6.5.8.1 Vibration isolation shall be provided between the vibration shaker and the laboratory floor.

3.1.6.5.9 Power Amplifier

3.1.6.5.9.1 The shaker power amplifier circuitry shall be solid state.

3.1.6.5.9.2 The shaker power amplifier shall be designed for air cooling.

3.1.6.5.9.3 The shaker power amplifier shall be designed to meet all requirements in 3.1.6.5.

3.1.6.5.10 Payload Weight

3.1.6.5.10.1 The Government maximum payload weight will not exceed 750 pounds (fixture and UUT).

3.2 Environmental Chamber

3.2.1 The environmentally conditioned portion (working space) of the temperature-altitude-humidity-vibration CET chamber shall be insulated and accessed by a hinged door.

3.2.2 The environmental chamber shall have a stainless steel interior.

3.2.3 The interior shall have continuously welded seams so that oil or other fluids cannot seep into the insulation.

3.2.4 Volume

3.2.4.1 The environmental chamber shall have a usable interior volume with minimum interior dimensions for the height, width, and depth of 48.0 inches.

3.2.4.2 The outside height of any machine section shall be less than 11 foot.

3.2.5 Circulating Air Blower/Fan

3.2.5.1 The environmental chamber shall have an internal blower or fan to circulate air within the environmental chamber.

3.2.5.2 The blower/fan shall not protrude into the usable environmental chamber volume.

3.2.5.3 The electric motor for the blower/fan shall be located external to the environmental chamber.

3.2.5.4 The blower/fan shall circulate air to maintain uniform temperature or temperature humidity within the environmental chamber as defined in Sections3.1.2 and 3.1.4.

3.2.5.5 The fan shall have a manual on/off switch and indicator light on the control and display unit.

3.2.5.6 Blower/Fan Speed

3.2.5.6.1 To compensate for lower air mass flows at altitude, the blower/fan speed shall automatically increase/decrease with altitude so that the temperature requirements in 3.1.2.4.2 are met.

3.2.6 Windows

3.2.6.1 The environmental chamber shall have an observation window to allow visual inspections into the chamber working space.

3.2.6.2 The window shall be a minimum of 12 inches by 12 inches.

3.2.6.3 The window shall be heated.

3.2.6.4 Window Wiper

3.2.6.4.1 A manually controlled wiper shall be provided to clear moisture or frost from the inside of the observation window glass.

3.2.7 Interior Lights

3.2.7.1 The environmental chamber shall have interior lighting.

3.2.7.2 The lights shall be positioned to provide uniform light distribution inside the environmental chamber.

3.2.7.3 The lights shall not protrude into the usable interior space of the environmental chamber.

3.2.7.4 The lights shall be controlled by a manual switch located on the Operator Control Interface.

3.2.8 Access Ports

3.2.8.1 The environmental chamber shall have two 3.0 inch diameter ports installed on the side of the environmental chamber which allows access for test item support equipment.

3.2.8.2 The access ports shall be supplied with removable metal caps or covers on the outside of the environmental chamber that shall seal the environmental chamber when installed.

3.2.8.3 Access ports shall not protrude into the usable space on the interior of the environmental chamber.

3.2.9 Electrical Feed Throughs

3.2.9.1 All feed throughs shall be electrically isolated from the chamber walls.

3.2.9.2 All feed throughs shall be sealed to prevent pressure leaks throughout the altitude, humidity, vibration and temperature ranges.

3.3 Operator Control Interface

3.3.1 The chamber shall have a discrete package for controlling chamber operation and displaying set point and measurement data.

3.3.2 Local operation of the chamber shall be by entering set points for immediate execution or by entering sequences of steps for timed automatic operation.

3.3.3 The Operator Control Interface unit shall control all operations of the chamber.

3.3.4 Calibration and/or repair of all measuring devices, such as, meters, displays, data acquisition, and controllers/programmers, shall be performed by facilities located within the Contiguous United States.

3.3.5 The Operator Control Interface shall have two (2) programmable event relays for Government use.

3.3.5.1 The contacts shall be rated for up to 28Vdc or 120Vac with a current rating of 2 amperes.

3.3.6 The Operator Control Interface shall have an Emergency Stop switch/button that de-energizes all chamber systems.

3.3.7 The Operator Control Interface shall record all test parameters for later downloading into a Microsoft Excel® spreadsheet.

3.3.8 Switches

3.3.8.1 The Operator Control Interface unit shall have manually operated switches to enable/disable the following systems:

3.3.8.1.1 Control Power

3.3.8.1.2 Circulator Fan

3.3.8.1.3 Lighting

3.3.8.1.4 Heaters

3.3.8.1.5 Cooling

3.3.8.1.6 Humidity

3.3.8.1.7 Dehumidify

3.3.8.1.8 Altitude

3.3.8.1.9 Remote Control

3.3.8.2 An indicator light shall be provided for each on/off switch.

3.3.9 Remote Operation

3.3.9.1 The Operator Control Interface unit shall accept remote computer entered commands for set point and timed automatic operation via Ethernet from the Test Cell Control (TCC).

3.3.9.2 All parameters that are available from the Operator Control Interface shall be accessible remotely in the TCC.

3.3.9.3 The Government will use the Application Programming Interface National Instruments© LabVIEW code in the TCC.

3.3.9.3.1 The Operator Control Interface command-set shall be compatible with LabVIEW code. (CDRL A001)

3.3.9.4 The Operator Control Interface shall monitor the TCC settable watchdog timer and abort current commands and initiate a safe shutdown to laboratory ambient conditions if communications is lost from the TCC Room.

3.3.10 Chart Recorder

3.3.10.1 The chamber shall have a circular chart type recorder to record the following:

3.3.10.1.1 Temperature

3.3.10.1.2 Altitude

3.3.10.1.3 Humidity

3.3.10.1.4 Conditioned Air Flow

3.3.10.1.5 Conditioned Air Temperature

3.3.11 High/Low Temperature Limiter

3.3.11.1 An independent temperature limiter shall be incorporated into the Operator Control Interface to provide safety to the unit under test.

3.4 General Requirements

3.4.1 Exterior Finish

3.4.1.1 The exterior shall be suitable to withstand an industrial laboratory environment which shall not be adversely affected by the fluids described in Section 3.4.9.

3.4.2 Condensation Drain

3.4.2.1 A drain shall be provided to remove condensation from the environmental chamber during humidity and temperature operations.

3.4.2.2 The drain shall not interfere with the automatic operation of the chamber and shall not require manual operation when temperature, altitude or vibration operation is required in a test sequence.

3.4.3 Refrigeration

3.4.3.1 The chamber shall use mechanical refrigeration systems.

3.4.3.2 Remotely located refrigeration systems shall have means to continuously feed refrigerant to the evaporator coils with minimal delay, such as bypass loops.

3.4.3.3 All pressure vessels shall be ASME certified.

3.4.3.4 Safeties

3.4.3.4.1 The refrigeration systems shall have protection for:

3.4.3.4.1.1 High pressure

3.4.3.4.1.2 Low pressure

3.4.3.4.1.3 Low oil pressure

3.4.3.4.1.4 High discharge temperature

3.4.3.4.2 A reset button shall be provided for resetting tripped safeties.

3.4.3.5 An indicator light shall indicate refrigeration over/under limits of 3.4.3.4 Safeties

3.4.3.6 A pressure relief valve shall be provided for the refrigeration systems.

3.4.3.7 Refrigerants

3.4.3.7.1 The refrigerants used shall be hydrogenated chlorofluorocarbons (HCFC's) or equivalent.

3.4.3.7.2 Chlorofluorocarbons (CFC's) shall not be used.

3.4.3.7.3 Refrigerant types shall be marked on the compressors.

3.4.3.7.4 Refrigeration charge information shall be marked on the machinery cabinet.

3.4.3.7.5 R-507 shall be used for the high stage of the cascaded system.

3.4.3.7.6 R-508B shall be used for the low stage of the cascaded system.

3.4.3.8 Gauges and Sight Glasses

3.4.3.8.1 Clearly visible gauges/sight glasses shall be provided for maintenance of the refrigeration systems.

3.4.3.9 Piping

3.4.3.9.1 Insulation shall be used on cold piping to reduce condensation.

3.4.3.9.2 Hot piping shall be protected to prevent unintended personnel contact.

3.4.4 Electric Power

3.4.4.1 The chamber shall operate from 480 volt, three-phase, and 60 Hz power.

3.4.4.2 A main power disconnect with an externally accessible switch shall be provided on each machinery cabinet.

3.4.4.3 A main power disconnects shall have 36 inches of clearance to any other machine cabinets or walls.

3.4.4.4 A terminal block shall be provided to connect a Government supplied electric power cable.

3.4.4.5 The electric power terminals shall be clearly marked.

3.4.4.6 The electrical power cabinet shall be accessible from above for main power connection conduit.

3.4.4.7 The chamber shall not be damaged by application of electric power with reverse phase rotation.

3.4.4.8 The chamber shall not be damaged with one or two phases of the three-phase AC power missing (blown fuses).

3.4.4.9 All chamber systems shall shutdown and not attempt to restart in the event of an AC power interruption or abnormal AC power (blown fuse on one or more phases).

3.4.4.10 A manual reset shall be required to restart the system.

3.4.4.11 Circuit Protection

3.4.4.11.1 All circuits in the chamber including the Operators Control Interface unit shall be protected with circuit breakers or fuses.

3.4.4.12 Wiring

3.4.4.12.1 All wiring used in the chamber shall meet National Electrical Code (NEC) standards.

3.4.5 Water

3.4.5.1 The chamber shall use water for condensing the high stage refrigerants.

3.4.5.1.1 Water will be supplied from a Government provided closed loop cooling system at 35 PSID between the supply and return connections.

3.4.5.1.2 The closed loop supply water temperature is controlled and will generally be between 55°F and 65°F and will not exceed 70°F.

3.4.5.1.3 The Chamber shall provide clearly marked water connections (supply and return).

3.4.5.2 Humidity Water Supply

3.4.5.2.1 The chamber shall use water for the humidity system.

3.4.5.2.2 Water for humidity will be supplied from a Government potable water source.

3.4.5.2.3 A water connection shall be supplied and clearly marked for connection to the government source.

3.4.5.2.4 Water Filtration

3.4.5.2.4.1 The chamber shall incorporate a replaceable cartridge type filter or other means to de-ionize/de-mineralize the supply water used for humidity to a resistance of not less than 500,000 ohms.

3.4.6 Heat Interlocks

3.4.6.1 An independent controlled high heat limit interlock shall be provided to prevent over temperature of the chamber or damage to heating elements.

3.4.7 Fan Interlocks

3.4.7.1 An interlock shall be provided to prevent operation of the chamber with the fan not operating.

3.4.8 Operation Environment

3.4.8.1 The chamber shall operate in unconditioned spaces (limited heat and no air-conditioning) with ambient temperatures above freezing to 46.1°C.

3.4.9 Fluid Compatibility

3.4.9.1 The interior of the environmental chamber shall be compatible with:

3.4.9.1.1 Synthetic engine oil (MIL-L-23699)

3.4.9.1.2 Oil vapor

3.4.9.1.3 Lubricating greases

3.4.9.1.4 Water

3.4.9.1.5 Water vapor

3.4.9.1.6 Industrial cleaning compounds

3.4.9.2 All components in the chamber shall be compatible with an industrial test laboratory environment.

3.4.10 Maintenance

3.4.10.1 All chamber systems shall be maintainable by the Government.

3.4.10.2 All subsystems shall be accessible for maintenance without removal of major components (vacuum pumps, refrigeration compressors, heat exchangers, vibration shaker, and vibration amplifier).

3.4.10.3 All interior and exterior electrical interconnections shall be clearly and permanently labeled.

3.4.10.4 All interior and exterior mechanical interconnections shall be clearly and permanently labeled.

3.4.10.5 All major component onsite repairs (vacuum pumps, refrigeration compressors, heat exchangers, vibration shaker, and vibration amplifier) shall be performed by Original Equipment Manufacturer (OEM) certified repair personnel.

3.4.10.6 All major component return repairs (vacuum pumps, refrigeration compressors, heat exchangers, vibration shaker, and vibration amplifier) shall be performed by Original Equipment Manufacturer (OEM) facilities located within the Contiguous United States.

3.4.11 Vacuum System

3.4.11.1 The chamber vacuum system shall be capable, at a minimum, of achieving the requirements of Section 3.1.3.

3.4.11.2 The system shall be designed to protect the vacuum pump from water during test cycles that requires high humidity prior to altitude operations.

3.4.11.2.1 Vacuum Exhaust

3.4.11.2.2 The exhaust from the vacuum system shall be clear of oil prior to being exhausted through the government supplied exhaust pipe (4 inch).

3.4.12 Installation

3.4.12.1 The environmental chamber shall fit through a 12 foot wide, 11 foot high door either in a single section or multiple sections.

3.4.12.2 Reserved.

3.4.12.3 The environmental chambers shall be installed on a flat 6 inch reinforced concrete floor.

3.4.12.4 The Contractor shall adhere to the space parameters defined in the floor plan DWG NO. 216B for allocation space with utilities locations and the conditioned air supply.

3.4.12.4.1 It is the Contractor’s responsibility to verify all measurements and utility locations as outlined in DWG NO. 216B.

3.4.12.5 A chamber system scaled drawings with overhead and side views including dimensions shall be provided to the Government detailing the major component locations in the floor space allocated, emphasizing efficient use for chamber system maintainability and maximizing floor space for reutilization by the government.

3.4.12.5.1 The Contractor shall provide a minimum of 18 square feet floor space clearance around the chamber access ports to accommodate test item support equipment.

3.4.12.6 The Government will place the chambers into the work space identified in DWG NO. 216B.

3.4.12.6.1 The Contractor shall provide on-site support to perform multiple section assembly and interconnections.

3.4.12.7 The Government will install the electrical power, water, and vacuum exhaust hookups, according to Contractor installation instructions.

3.4.12.8 Start Up

3.4.12.8.1 After all utilities are installed on the unit; the manufacturer shall perform an on-site inspection at Patuxent River, MD of the Government’s installation, to ensure correct connection to all utilities.

3.4.12.8.2 The Contractor shall then start-up the chamber and performs an on-site performance test of the chamber systems to ensure all requirements in Section 3 are achieved.

3.4.12.8.3 Upon satisfactory Contractor start-up and performance testing final acceptance of the unit will be by the Government at Destination on-site at Patuxent River, MD.

CLIN 0002 – TECHNICAL DATA – NOT SEPARETELY PRICED (NSP)

4. ILLUSTRATIONS/DRAWINGS/MANUALS/SPECIFICATIONS

4.1 Maintenance Manual (CDRL A001)

4.1.1 Contractor shall provide documentation/manuals detailing routine maintenance of all systems.

4.1.2 Contractor shall provide documentation/manuals detailing overhaul maintenance of all systems.

4.1.3 Contractor shall provide a detailed parts list with illustrated parts breakdown.

4.1.4 Contractor shall provide technical details (data sheets) of all systems.

4.1.5 Contractor shall provide documentation/manuals detailing troubleshooting procedures of all systems.

4.1.6 Contractor shall provide a spare parts list (CDRL A002).

4.2 Operator Manual (CDRL A003)

4.2.1 Contractor shall provide documentation/manuals detailing operation of all systems both locally and remotely.

4.3 Calibration Manual (CDRL A004)

4.3.1 Contractor shall provide procedures for system calibration.

4.3.2 Contractor shall provide system calibration requirements.

4.4 Software

4.4.1 All CET Chamber software shall comply with requirements specified within Department of Defense Instruction 8500.01, Cybersecurity.

4.4.2 Operating System with License Requirement as applicable (CDRL A005)

4.4.2.1 Microsoft Windows 7 Professional®

4.5 Warranty (CDRL A006)

4.5.1 The Contractor shall include a one (1) year standard warranty effective Full Operational Capability (FOC).

4.6 Engineering Drawings/Schematics (CDRL A007)

4.6.1 The Contractor shall provide final 100% dimensional drawings at FOC.

4.6.2 The Contractor shall provide electrical wiring schematics.

4.6.3 The Contractor shall provide mechanical drawings/schematics.

4.7 Specifications

4.7.1 The Contractor shall provide specifications for chamber and subsystems.

Section D - Packaging and Marking

DELIVERY INFORMATION

Delivery FOB Destination, Patuxent River Maryland

4.8 All shipments required for the CET Chamber shall arrive in palletized packaging for ease of unloading at the EPSEF.

4.9 Any shipment exceeding four-thousand (4,000) pounds shall be defined as a Heavy Shipment.

4.9.1 Each Heavy Shipment shall adhere to the following:

4.9.1.1 Contractor shall notify the Government not less than one (1) week in advance of shipment.

4.9.1.2 Selected shipper shall schedule the specific date of delivery.

4.9.1.3 Selected shipper shall schedule the specific time of delivery.

4.9.1.4 Shipper shall notify the Government immediately upon any deviation to the delivery schedule.

CLAUSES INCORPORATED BY FULL TEXT

Section E - Inspection and Acceptance

INSPECTION AND ACCEPTANCE

Upon satisfactory Contractor start-up and successful completion of the Acceptance Test Procedure final acceptance of the unit will be by the Government at Destination on-site at Patuxent River, MD and documented by DD Form 250.

INSPECTION AND ACCEPTANCE TERMS

Supplies/services will be inspected/accepted at:

Section F - Deliveries or Performance

CDRL DELIVERY INFORMATION

All Contract Data Requirements Lists (CDRLs) shall be delivered in accordance with the DD Form 1423s provided under Exhibit A in Section J.

DELIVERY INFORMATION

MICHAEL GOODNOW

48298 SHAW ROAD

BLDG 1461

PATUXENT RIVER MD 20670

301-342-0814

N00421

31-JUL-2017

CLAUSES INCORPORATED BY REFERENCE

Section G - Contract Administration Data

TBD

No functions are retained.

(2) The following additional contract administration functions are assigned (see FAR 42.302(b)):

No additional functions are assigned.

(c) Inquiries regarding payment should be referred to: MyInvoice at https://myinvoice.csd.disa.mil//index.html.

Section H - Special Contract Requirements

Section I - Contract Clauses

CLAUSES INCORPORATED BY REFERENCE