Attachment J.10 DC BUS Grounding Requirements.pdf

PDF 19 KB Posted

Attached to
Direct Current Back-Up System (DC BUS) Power Supply Federal contract opportunity
Solicitation number
693KA8-20-R-00008
Issued by
Department of Transportation Federal Aviation Administration Headquarters

About this file

This document outlines requirements for a federal solicitation seeking life cycle in-service support of Direct Current Back-Up System (DC BUS) uninterruptible power supplies. Offerors must provide conditioned, uninterruptable electrical power to support critical National Air Space communication and electronic equipment through an Indefinite Delivery Indefinite Quantity contract with the Federal Aviation Administration worth up to $10 million over a potential 10-year period of performance. Questions are due by March 10th, 2020, with responses by March 18th. Proposals are due by March 27th. The contract type will be IDIQ with one two-year base period and four two-year option periods. The solicitation specifies requirements for grounding DC BUS equipment and connecting various system components to grounding plates in facilities.

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Other files for this federal contract opportunity

Other files attached to Direct Current Back-Up System (DC BUS) Power Supply, newest first.
File Type Posted
Section M _Eval Factors For Award_Amend 00004.pdf PDF
Section L _Instructions Conditions and Notices to Offerors_AMEND 00004.pdf PDF
SF 30 _ Amend 00004.pdf PDF
Section L _Instructions Conditions and Notices to Offerors_AMEND 00003.pdf PDF
FAA Response to Questions Requests for Clarifications_Amend 00003.pdf PDF
Section L_Instructions Conditions and Notices to Offerors_Amend 00002.pdf PDF
Attach J.02 CDRLs and DIDs _Amend 00002.pdf PDF
FAA Responses to Questions Requests for Clarifications_ Amend 00002.pdf PDF
Section M_Evaluation Factors For Award_Amend 00002.pdf PDF
Section F_Deliveries or Performances_Amend 00002.pdf PDF
SF 33_Amend 00001 and 00002.pdf PDF
Attach J.01 DC BUS Specification_Amend 00002.pdf PDF
Section B.4_Price Schedule_Amend 00002.xlsx XLSX spreadsheet
DC BUS Section L _ Information for ConsiderationAffecting Offeror Proposal Submission_AMENDMENT 00001.pdf PDF
Section D _ Packaging Marking.pdf PDF
Section I _ Contract Clauses.pdf PDF
Section C _ Statement of Work.pdf PDF
Attachment J.11 Excavation and Handling of Contaminated Material.pdf PDF
Attachment J.30 FAA Order 6950.27A.pdf PDF
Attachment J.23 Module Performance - L.1.doc DOC document
Section E _ Inspection Acceptance.pdf PDF
Attachment J.21 Project Schedule Example Waco TX.pdf PDF
Attachment J.14 CDLS User Guide.pdf PDF
Attachment J.27 Business Declaration.docx DOCX document
Attachment J.20 DC BUS CDLS Depot Inventory.xlsx XLSX spreadsheet
Attachment J.25 DC BUS Equipment Characteristics - L.3.xls XLS spreadsheet
Attachment J.17 DC BUS CDLS Quarterly Depot Shipments.xlsx XLSX spreadsheet
Attachment J.05 FAA-STD-028C.pdf PDF
Section M _ Evaluation Factors for Award.pdf PDF
Section G _ Contract Admin Data.pdf PDF
Attachment J.02 CDRLs and DIDs.pdf PDF
Attachment J.28 FAA Order 4600.27C.pdf PDF
Attachment J.01 DC BUS Specification.pdf PDF
Attachment J.12 PreConstruction Conference Agenda and Checklist.pdf PDF
Section F _ Deliveries or Performances.pdf PDF
Attachment J.06 DC BUS Battery Test and Appendix.pdf PDF
Attachment J.04 SOP FAA Field Site Requests.pdf PDF
Attachment J.09 DC BUS UXTM CAI Checklist.pdf PDF
Attachment J.03 DC BUS Frequently Used Acronyms.pdf PDF
Section B.4_Price Schedule.xlsx XLSX spreadsheet
DC BUS Section L _ Information for ConsiderationAffecting Offeror Proposal Submission.pdf PDF
Attachment J.18 DC BUS CDLS Cumulative Warrantied Orders.xlsx XLSX spreadsheet
Attachment J.16 DC BUS CDLS Quarterly Tracking Trending and Cost.xlsx XLSX spreadsheet
Attachment J.29 FAA Form 3900-17.pdf PDF
Section J _ List of Attachments .pdf PDF
Attachment J.19 DC BUS CDLS Cumulative Spare Orders Depot Receipts.xlsx XLSX spreadsheet
Section H _ Special Contract Requirements.pdf PDF
Attachment J.07 FAA Form 3900-20_Pre-Construction and Maintenance Checklist.pdf PDF
Attachment J.24 DC BUS Module Performance - L.2.xls XLS spreadsheet
Attachment J.22 DC BUS Past Performance Questionnaire.doc DOC document
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Text version

SIR 693KA8-20-R-00008

ATTACHMENT J.10, DC BUS Grounding Requirements

09/24/19

REMOTE AIR TO GROUND COMMUNICATION FACILITIES (RCAG, RTR,

AND BUEC)

The DC Bus System ground bar must be connected to the Main Ground Plate via a 1/0 AWG solid green cable with brass tags on each end. The tags must identify the far end termination, and be embossed with “Do Not Disconnect lead". This connection (Reference Ground / Grounding Electrode Conductor) must be a dedicated run.

Note: The Main Ground Plate should be connected to the counterpoise via a 500 (or 2-

250) kcmil cable. This connection is the FAA’s responsibility.

The DC Bus System equipment rack (chassis) must be connected to the Multipoint Ground via a 2 AWG green/orange cable. A secondary path to ground for the equipment rack must be accomplished via an existing grounded cable tray, or a DC BUS-installed 4 x 4 square duct raceway (DC Wireway) installed above the DC Bus System equipment rack that runs between the equipment rack and the radio cabinets. The raceway sections must be bonded together following FAA-STD-019F para. 4.7.4.2. If raceway does not follow FAA-STD-019F para. 4.7.4.2, then the individual sections or metallic cable tray and wireway systems must be bonded with a minimum 6 AWG insulated copper conductor. One raceway end must be connected to the radio cabinets (via metal to metal, or via external bonding conductor on the flex conduit); both raceway ends must be connected to Multipoint Ground via a 6 2 AWG green/orange cable.

Note: The Multipoint Ground Plate should be connected to the Main Ground Plate via an existing 4/0 cable. This connection is the FAA’s responsibility.

The DC Bus System battery frame must be connected to the Multipoint Ground via a 2 AWG green/orange cable.

Note: For proper performance of the DC Bus System, the negative return for the batteries is connected to the DC Bus System ground bar via the Anderson quick disconnect and the 4/0 AWG cable.

The ERMS P1 and P7B Panels must be connected to the Multipoint Ground via a 6 AWG green/orange cable (as long as they are within 13 ft. of a multipoint plate, if not see FAA- STD-019F table 3). A secondary ground path from the ERMS panels to multipoint ground is not required, as other (fortuitous) grounds exist. Ex: the AC power cables are installed in grounded ¾” EMT, there are shielded cables in the panels, etc.

Note: If only one ground (Main Ground Plate or Multipoint Ground) is available at the facility, all connections must be made to this ground. This ground should be connected by the FAA to the counterpoise via a 500 (or 2-250) kcmil cable.

SIR 693KA8-20-R-00008

ATTACHMENT J.10, DC BUS Grounding Requirements

09/24/19

SMALL AIR TRAFFIC CONTROL TOWERS (ATCT)

The DC Bus System ground bar must be connected to Building Steel or the Main Ground Plate via a 1/0 AWG solid green cable with brass tags on each end. The tags must identify the far end termination, and be embossed with “Do Not Disconnect lead". This connection (Reference Ground / Equipment Grounding Conductor) must be a dedicated run.

Note: From building steel an existing cable should be connected to Multipoint Ground.

The Multipoint Ground should be connected to the Main Ground Plate via a 4/0 AWG cable. The Main Ground Plate should be connected to the counterpoise via a 500 kcmil cable. These connections are the FAA’s responsibility.

The DC Bus System equipment rack (chassis) must be connected to the Multipoint Ground via a 2 AWG green/orange cable. A secondary path to ground for the equipment rack must be accomplished via an existing grounded cable tray or conduit, or a DC BUS-installed 4 x 4 square duct raceway (DC Wireway) installed above the DC Bus System equipment rack that runs between the equipment rack and the radio cabinets. The raceway sections must be bonded together following FAA-STD-019F para. 4.7.4.2. If raceway does not follow FAA-STD-019F para. 4.7.4.2, then the individual sections or metallic cable tray and wireway systems must be bonded with a minimum 6 AWG insulated copper conductor. One raceway end must be connected to the radio cabinets (via metal to metal, or via external bonding conductor on the flex conduit); both raceway ends must be connected to Multipoint Ground via a 6 2 AWG green/orange cable.

The DC Bus System battery frame must be connected to the Multipoint Ground via a 2 AWG green/orange cable.

Note: For proper performance of the DC Bus System, the negative return for the batteries is connected to the DC Bus System ground bar via the Anderson quick disconnect and the 4/0 AWG cable, or larger (to minimize voltage drop),if necessary.

When the batteries are located more than 25 feet from the DC Bus System, an over-current protection device must be installed at the battery; a 200 Amp circuit breaker is preferred.

The Environmental Remote Monitoring System (ERMS) P1 and P7B Panels must be connected to the Multipoint Ground via a 6 AWG green/orange cable (as long as they are within 13 ft. of a multipoint plate, if not see FAA-STD-019F table 3). A secondary ground path from the ERMS panels to multipoint ground is not required, as other (fortuitous) ground paths exist. Ex: the AC power cables are installed in grounded ¾” EMT, there are shielded cables in the panels, etc.

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