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VIRGIN ISLANDS PORT AUTHORITY Henry E. Rohlsen Airport Post Office Box 301707
St. Croix, VI 00820 St. Thomas, VI 00803
Telephone: (340) 778-9696 Telephone: (340)774-1629
www.viport.com
RUNWAY SHOULDER AND ELECTRICAL VAULT Addendum #3
HENRY E. ROHLSEN AIRPORT Page 1 of 3
ADDENDUM No. 3
RUNWAY SHOULDER AND ELECTRICAL VAULT CONSTRUCTION
HENRY E. ROHLSEN AIRPORT
ST. CROIX, U.S. VIRGIN ISLANDS
TO: ALL PROPOSERS
From:
Kate C. Davis
Procurement and Contract Manager
Date: May 22, 2020
Re: Henry E. Rohlsen Airport – Runway Shoulder and Electrical Vault
Construction
FAA AIP No.: 3-78-0002-040-2020
This addendum modifies or interprets the proposal documents by additions, deletions, clarifications,
corrections, or other type of modifications. Addenda will become part of the Contract Documents.
It is required that all bidders acknowledge receipt of Addenda on Page BF-3 of the Bid Form.
I. CHANGES TO THE PROJECT MANUAL (Volume 1 of 2)
1. The Bid date shall be changed to June 10th, 2020 as follows:
SEALED BIDS will be received by the Virgin Islands Port Authority, St. Croix, U.S. Virgin Islands, at:
Purchasing Department
Virgin Islands Port Authority
Henry E. Rohlsen Airport
St. Croix, U.S. Virgin Islands 00820
until the hour of 2:00 PM, Local Time, on Wednesday, June 10th, 2020, following which time, in the
Engineering Office of the Henry E. Rohlsen Airport Terminal Building, St. Croix, U. S. Virgin Islands,
said bids will be opened and publicly read immediately.
VIRGIN ISLANDS PORT AUTHORITY Henry E. Rohlsen Airport
St. Croix, VI 00820
RUNWAY SHOULDER AND ELECTRICAL VAULT Addendum #3
HENRY E. ROHLSEN AIRPORT Page 2 of 3
2. Remove Bid form checklist page BF-0 and Replace with attached Bid form Checklist page
BF-0. This change updates page numbers on the checklist.
3. Remove Bid price form page BF-5 and Replace with attached bid form page BF-5. This
change updates the quantity of Unclassified Excavation.
4. Remove Bid price form Page BF-10 and Replace with the attached bid form page BF-10.
This change removes the item for topsoil stripping.
5. Remove Designation of Electrical Contractor page BF-13B and Replace with revised
attached page BF-13B. This change removes the timeframe requirements for completed
projects.
II. CHANGES TO TECHNICAL SPECIFICATIONS (VOLUME 2 OF 2)
1. Remove the Specification Section L-127 “Airfield Lighting Control System Performance
Specifications” in its entirety and replace with the attached Specification L-127. Changes to
this section includes the modification to section 127-1.1 and 127-1.2 to clarify responsible
party as either Manufacturer, Contractor or both. In addition, section 127-1.17 was revised to
identify the spare parts to be provided under this contract.
2. Remove the Specification Section 263200 “Packaged Generator Assemblies” in its entirety
and replace with the attached Specification 263200. Changes to this section includes the
removal of the 75-mile and 90% part requirements in section 1.05.
III. CHANGES TO THE CONTRACT DRAWINGS
1. Sheet A002: Add the below door hardware schedule to sheet A002.
PAIR 3’-0” X 7’-0” HM DOORS IN 2” HM FRAME
6 HINGE McKinley T4A3386 4 ½” x 4 ½” US32D NRP US32D
1 SURFACE BOLT Rockwood 580-12 US26D
1 EXIT DEVICE Sargent 43-MD8610 F US32D US32D
1 CORE VERIFY KEYING WITH OWNER
2 HOLD-OPEN Rixson 9-236 652 652
1 ASTRAGAL Pemko 355CP C
2 KICK PLATE Rockwood K1050 8” x 34” US32D US32D
1 RAIN DRIP Pemko 346C C
1 GASKETING Pemko 303CS C
1 THRESHOLD Pemko 2005AT A
2. Sheet S002: Add the following note to item C3 under the properties for concrete table:
Note 6. Concrete mix shall have a water resistant additive. Basis of design product is Hycrete
www.hycrete.com. Acceptable alternate products include Penetron (www.pentron.com) or
Xypex (www.xypex.com) or another approved equal. Installation per manufacturer’s
instructions.
VIRGIN ISLANDS PORT AUTHORITY Henry E. Rohlsen Airport
St. Croix, VI 00820
RUNWAY SHOULDER AND ELECTRICAL VAULT Addendum #3
HENRY E. ROHLSEN AIRPORT Page 3 of 3
3. Sheet C301. DELETE cut and fill table and notes AND REPLACE with the below Cut and
Fill table and Notes. This change adjusts the Excavation quantities to remove the topsoil
stripping volume which is no longer required. Revised Notes to indicate that Excavated
material is to remain property of VIPA and not be hauled off site by the contractor
END OF ADDENDUM No. 3.
VIRGIN ISLANDS PORT AUTHORITY Henry E. Rohlsen Airport Post Office Box 301707
St. Croix, VI 00820 St. Thomas, VI 00803
Telephone: (340) 778-9696 Telephone: (340)774-1629
www.viport.com
RESPONSES TO BIDDERS QUESTIONS
RUNWAY SHOULDER AND ELECTRICAL VAULT CONSTRUCTION
HENRY E. ROHLSEN AIRPORT
ST. CROIX, U.S. VIRGIN ISLANDS
TO: ALL PROPOSERS
From:
Kate C. Davis
Procurement and Contract Manager
Date: May 22, 2020
Re: Henry E. Rohlsen Airport – Runway Shoulder and Electrical Vault
Construction
FAA AIP No.: 3-78-0002-040-2020
I. RESPONSES TO QUESTIONS
1. In consideration of Addendum 2, would VIPA please consider a bid extension till June 3rd
for the Runway 10-28 Shoulder and Electrical Vault Construction at HERA project? There is
quite a bit info to review with respect to Addendum 2, and the Memorial day holiday and
vendor pricing during the covid epidemic is adding time that would not necessarily be a
factor at alternate times. A one week extension is requested to the bid date.
Response: The Bid Date has been moved to June 10th per Addendum No. 3
2. Sheet BF-13B states that the contractor shall designate a superintendent with experience on
the Airfield Lighting Computerized Control Systems to be on site for the entire duration of
the project. The part of the project that includes the ALCMS system represents only a small
portion of the project. The shoulder, lighting and can installation is standard work and should
not need the ALCMS supervisor included. Please clarify if this supervision required under
this section will be for the installation and powering of the ALCC portion of the project only
or for the all portion of the project? Also confirm is this supervisor can be stratified by the
ALCMS systems manufacturer representative that would come down as part of the
VIRGIN ISLANDS PORT AUTHORITY Henry E. Rohlsen Airport
St. Croix, VI 00820
RUNWAY SHOULDER AND ELECTRICAL VAULT Addendum #3
HENRY E. ROHLSEN AIRPORT Page 2 of 4
installation, start up and training of the new system?
Response: The requirement shall be for a superintendent with experience on the Airfield
Lighting Computerized Control System to be onsite during the ALCMS portion of the
project. The ALCMS manufacturer representative does not satisfy this requirement.
3. SPECIFICATION SECTION L-127.1.1, 2 states the following: The ALCMS Contractor
shall have experience in aviation ground lighting control and be listed as an FAA approved
manufacturer in FAA AC 150/5245-568. The companies listed in this ac are qualifed
manufacturers and not installers. They will provide assistance and supervision of the
installation as well as all the startup requirements but they typically do not fill the role of
installers, can you clarify this intent?
Specification shall be revised as follows:
Section 1.1: The word “Contractor” shall be REPLACED with the word “Manufacturer”
in the third sentence TO READ: “The ALCMS Manufacturer shall have experience in
aviation ground lighting control and be listed as an FAA approved manufacturer in FAA
AC 150/5245-56B.”
Section 1.2: The wording shall be revised TO READ: “The ALCMS
Manufacturer/Contractor shall furnish, install, test and commission a complete and
functional computerized airfield lighting system, L-890BB, per FAA Advisory Circular
10/5345-56 latest edition.
4. Specification 263200 section 2.01 -the acceptable dealers as indicated in a and b of this
section do not meet the quality assurance requirements indicated in section 1.05 a and d of
this same specification due to the fact that they are not within 75 mile radius. More than
likely even those eg distributors who do meet the 75 ml radius requirement do not meet some
of the requirements of part d whereas they need to maintain "90% of all generator spare parts
available locally". Is there a more focused definition as to what spare parts means so that we
can present it to potential vendors that do meet the 75 ml radius requirement to verify that
there is an eg vendor that is acceptable? Alternatively, can you provide an eg vendor as basis
of design that is pre qualified based on the requirements of this specification?
Response: The 75-mile and 90% part requirements shall be removed from Specification
263200 Section 2.01.
5. L-127 1.17 calls out for spare parts pricing but its not evident if the spare parts are to be
included in the bid or only the pricing as a means of locking down the price over a period of
time. Can you clarify if we are to include the spare parts in the proposal?
Response: Refer to the revised Specification L-127. The section has been revised to list the
spare parts that are to be included as part of this Contract. Cost for spare parts shall be
inclusive to the pay item for the ALCMS.
6. Can the requirements of designated airfield electrical contractor as per page bf-13b in project
manual be amended to allow an electrical contractor who has succesfull y performed airfield
VIRGIN ISLANDS PORT AUTHORITY Henry E. Rohlsen Airport
St. Croix, VI 00820
RUNWAY SHOULDER AND ELECTRICAL VAULT Addendum #3
HENRY E. ROHLSEN AIRPORT Page 3 of 4
lighting installations in the past of comparable magnitude without imposing 5 year
limitation? This is a small territory with two airports and within the past 5 years there may
have been only two(2) projects between the two airports that would compare to this
one.technically that limits the selection of electrical contractors in the territory to two(2).
Response: Yes, See Revised Contractor Qualifications that remove the time frame for
projects of comparable magnitude.
7. Can the requirements of designated superintendent be modified to remove the time frame
requirement and to allow personnel that have succesfully carried out airfield lighting in the
past, in the territory, and of similar magnitude? For the same reason as above. Due to the
limited amount of airfield projects that are provided in the territory limits the availability of
otherwise qualified electrical contractors to two(2) as well.
Response: Yes, See Revised Contractor Qualifications that remove the time frame related
to completed airfield lighting projects.
1. On a similar job on STT we experienced close to 100 impacted days for action not related to
the contractors fault. In this bid based on the clarifications, the contractor will only be
compensated by delays on the asphalt activities. Contractors will be induced to raise their
number in order to mitigate this risk. We suggest to define an allowance to cover this delays
in order to cover the associated cost
Response: Refer to Special Provisions Section 6.0 in regard to delay claims. If the
Contractor's performance of this contract is delayed, which delay is beyond the
reasonable control and without the fault or negligence of the Contractor or its
subcontractors, or by changes ordered in the work and in either event where such
delay or change in the work impacts the CRITICAL PATH, then the Contract time
shall be extended by Change Order, as determined by the Owner.
Per Special Provision Paragraph 6.6, No additional payment will be granted outside of
the established pay items listed in the Bid set for partial or full night delays. As stated
in Addendum 2, only asphalt paving particular to the Runway will be considered for
the airline delay. It is anticipated that large portions of the taxiway and electrical vault
will be available to work on in the event of an airline delay to prevent loss of
production to avoid any critical path impacts.
8. If NOTAM is active and an air craft is to land on the runway, can the contractor be held
responsible to any citation or a violation an FAA regulations?
Response: Aircraft are not permitted to land if a NOTAM is in place without approval
from the Tower either in STX or from SJU. In the event the tower permits an
emergency landing, the contractor may be directed to leave the area by airfield
operations, the tower or by the Engineer. The contractor can be held responsible for
not following any direct orders from the Tower or Airport operations per Special
Provision Section 4.0.
VIRGIN ISLANDS PORT AUTHORITY Henry E. Rohlsen Airport
St. Croix, VI 00820
RUNWAY SHOULDER AND ELECTRICAL VAULT Addendum #3
HENRY E. ROHLSEN AIRPORT Page 4 of 4
9. Will there be personnel at the Control tower while works are been executed?
Response: No, the tower is closed and direct communication to pilots is the only
communication during nighttime hours. During periods of tower closures aircraft fall
under San Juan’s Tower Direction (SJU), but the contractor will not have direct
communication with San Juan.
10. Please provide doors and hardware schedule to be used in the project.
The attached Hardware schedule shall be used for the Vault Building.
PAIR 3’-0” X 7’-0” HM DOORS IN 2” HM FRAME
6 HINGE McKinley T4A3386 4 ½” x 4 ½” US32D NRP US32D
1 SURFACE BOLT Rockwood 580-12 US26D
1 EXIT DEVICE Sargent 43-MD8610 F US32D US32D
1 CORE VERIFY KEYING WITH OWNER
2 HOLD-OPEN Rixson 9-236 652 652
1 ASTRAGAL Pemko 355CP C
2 KICK PLATE Rockwood K1050 8” x 34” US32D US32D
1 RAIN DRIP Pemko 346C C
1 GASKETING Pemko 303CS C
1 THRESHOLD Pemko 2005AT A
11. Will the roof of the building require some kind of sealing?
Yes, : The roof is coated with a polyurethane methacrylate traffic coating as noted on the
drawings on Sheet A201 and in Specification Section 07 18 00- Traffic Coatings,
Pedestrian Traffic. Additionally the concrete mix requires a water resistant additive to be
used per Addendum No. 3. Basis of design product is Hycrete www.hycrete.com.
Accceptable alternate products include Penetron (www.pentron.com) or Xypex
(www.xypex.com) or another approved equal. Installation per maunfacturer’s
instructions.
12. Please indicate if you can use grass rolls instead of seeds.
Response: Sod is acceptable at no additional cost to the contract or extension of contract
time. Contractor is responsible for watering and fertilizing sod until it is established. If
used, Sod shall meet the requirement of standard FAA Specification T-904 which is
available on the FAA website and can be provided upon request
Addendum No. 3 BF-0
Bid Form Checklist
o Bid Form (BF-2)
o Sub-Contractors and Prime Contractors Work and Acknowledgement of Addenda (BF-3)
o Bid Price Form (BF-4 thru BF-10)
o Contract Time and Liquidated Damages (BF-11)
o Designation of Subcontractors (BF-12)
o Prime Contractor and Electrical Contractor Work (BF-13 and BF-13B)
o Bid Bond (BF-14 thru BF-15)
o Partnership Certificate (BF-16)
o Corporate Certificate (BF-17)
o Bidder Qualification Questionnaire (BF-18 thru BF-20)
o Disadvantaged Business Enterprise (BF-21)
o Disadvantaged Business Enterprise Assurance Form (BF-22)
o List of Proposed Disadvantaged Business Enterprise Sub-Contractors (BF-23)
o Letter of Intent to Perform as a Disadvantaged Business Enterprise Sub-Contractor (BF-24)
o Statement of Good Faith Efforts (BF-25 and BF-26)
o Notice of Requirement for Affirmative Action to Ensure Equal Employment Opportunity
(BF-27)
o Form of Non-Collusion Affidavit (BF-28)
o Certification of Offeror/Bidder Regarding Debarment (BF-29)
o Certification of Offeror/Bidder Regarding Tax Delinquency and Felony Convictions (BF-30)
o Certification Regarding Lobbying (BF-31)
o Equal Opportunity Clause and Report Statement (BF-32 and BF-33)
o Buy American Preference (BF-34 ad BF-35)
o Prohibition of Segregated Facilities (BF-36)
o Department of Planning and Natural Resources & U.S. Environmental Protection Agency
Construction Notices of Intent (BF-37)
Forms must be returned with each firm’s proposal.
Mark “N/A” if not applicable to your firm.
THIS PAGE MUST BE COMPLETED AND SUBMITTED WITH OFFER
Addendum No. 3 BF-5
ITEM # SPEC. NO. ITEM DESCRIPTION UNIT QTY UNIT PRICE TOTAL
1 C-105-1 MOBILIZATION LS 1
2 C-105-2 AIRLINE DELAY (PARTIAL DELAY, 1-2 HOURS) EA 5
3 C-105-3 AIRLINE DELAY (FULL NIGHT LOSS) EA 3
4 C-100-1 CONTRACTOR QUALITY CONTROL PROGRAM
(CQCP)
LS 1
5 C-102-1 TEMPORARY STORMWATER POLLUTION,
PREVENTION, EROSION AND SILTATION CONTROLLS
1
6 C-120-1SAFETY, SECURITY, AND MAINTENANCE OF
AIRFIELD TRAFFICLS 1
7 P-101-1 MISCELLANEOUS PAVEMENT REMOVAL AND
MINOR DEMOLITION
LS 1
8 P-152-1 UNCLASSIFIED EXCAVATION CY 14,050
9 P-152-2 EMBANKMENT IN PLACE (DOUBLE-HANDLING OF
EXISTING SOIL OBTAINED FROM UNCLASSIFIED
EXCAVATION)
CY 6,000
10 P-209-1 8" CRUSHED AGGREGATE BASE COURSE SY 56,000
11 P-403-1 ASPHALT MIXTURE SURFACE COURSE TN 9,000
12 P-602-1 EMULSIFIED ASPHALT PRIME COAT GAL 16,000
13 P-620-1 WHITE OR YELLOW REFLECTIVE RUNWAY
MARKING PAINT
SF 80,000
14 P-620-2 NON-REFLECTIVE BLACK RUNWAY MARKING
PAINT
SF 60,000
15 T-901-1 SEEDING AC 6.2
SCHEDULE A - RUNWAY SHOULDER CONSTRUCTION
TOTAL SCHEDULE A:
Provide, in the appropriate spaces of the Bid Price Form, the unit price(s) and lump sum price(s), based on the
description indicated for that item, the Total Amount of each item in numerical figures, and the Total amount bid for
the entire work.
PROCEED TO SCHEDULE B AND C UPON COMPLETION OF THIS BID SCHEDULE. ALL SCHEDULES OF
WORK MUST BE COMPLETELY FILLED IN TO BE CONSIDERED FOR AWARD
THIS PAGE MUST BE COMPLETED AND SUBMITTED WITH OFFER
Addendum No. 3 BF-10
ITEM # SPEC. NO. ITEM DESCRIPTION UNIT QTY UNIT PRICE TOTAL
2 P-152-1 UNCLASSIFIED EXCAVATION CY -7,000
3 P-152-2 EMBANKMENT IN PLACE CY -2,268
4 P-209-1 8" CRUSHED AGGREGATE BASE COURSE SY -27,150
5 P-403-1 ASPHALT MIXTURE SURFACE COURSE TN -4,300
6 P-602-1 EMULSIFIED ASPHALT PRIME COAT GAL -8,000
7 P-620-1 WHITE OR YELLOW REFLECTIVE RUNWAY
MARKING PAINT
SF -8,700
8 P-620-2 NON-REFLECTIVE BLACK RUNWAY MARKING
PAINT
SF -13,000
ITEM # SPEC. NO. ITEM DESCRIPTION UNIT QTY UNIT PRICE TOTAL
1 P-219-1 CRUSHED CONCRETE BASE (OWNER
SUPPLIED/CONTRACTOR CRUSHED AND
INSTALLED
SY 56,000
2 P-210-1 CALICHE BASE COURSE (CONTRACTOR
FURNISHED AND INSTALLED)
SY 56,000
TOTAL CONSTRUCTION 25-FT SHOULDERS (SCHEDULES A + B + C):
TOTAL CONSTRUCTION 12.5-FT SHOULDERS (SCHEDULES A + B + C - DEDUCTIVE ALTERNATE NO. 1 TOTAL):
DEDUCTIVE ALTERNATE 1 - REDUCE SHOULDER WIDTH TO 12.5-FT
TOTAL DEDUCTIVE ALTERNATE FOR 12.5-FT SHOULDERS
MATERIAL ALTERNATIVES (TO BE SUBSTITUTED FOR P-209 CRUSHED AGGREGATE BASE COURSE)
Material Alternatives. Selection of a pavement base course alternative is subject to verification that sufficient supply is available locally.
A determination of which base course is used will be determined after the opening of the bids. The contractor shall fill in their unit
prices for providing the two alternatives listed in the bid form. This is the full price to install the item. Should it be decided to utilize an
alternative base, this unit price will replace the unit price in the bid schedule for “P-209-1 Crushed Aggregate Base Course” for any or
all schedules of work.
Provide, in the appropriate spaces of the Bid Price Form, the unit price(s) and lump sum price(s), based on the
description indicated for that item, the Total Amount of each item in numerical figures, and the Total amount bid for
the entire work.
_____________________________________________ ______________________________________
Name of Bidder Signature of Officer
THIS PAGE MUST BE COMPLETED AND SUBMITTED WITH OFFER
Addendum No. 3 BF-13B
DESIGNATION OF
AIRFIELD ELECTRICAL CONTRACTOR
Project Name: RUNWAY 10-28 SHOULDER AND ELECTRICAL VAULT CONSTRUCTION
HENRY E. ROHLSEN AIRPORT
AIRFIELD LIGHTING COMPUTERIZED CONTROL SYSTEMS:
The Contractor shall designate a superintendent experienced as specified herein for the duration of this project. The superintendent shall be experienced in either similar airfield lighting computerized control systems or airport control systems and installation of airfield lighting vault equipment modifications in excess of $150,000. Information documenting the required experience shall be provided. Failure to provide this information that meets this requirement shall cause the Bidder to be considered non-responsive. Attach additional pages if necessary.
DATE WORK DESCRIPTION CONTRACT AMOUNT
GENERAL AIRFIELD ELECTRICAL:
The contractor shall have been in continuous business and a contractor for the last five (5) years. The general airfield electrical subcontractor shall provide electrical experience / projects reflecting airfield lighting projects that have included the installation of runway and taxiway lighting systems in accordance with FAA standards and specifications with a minimum value for electrical work of $500,000. Attach additional pages if necessary.
DATE WORK DESCRIPTION CONTRACT AMOUNT
Name of Authorized Individual
Authorized Signature
Date
Addendum No. 3 L-127-1
ITEM L-127 - AIRFIELD LIGHTING CONTROL SYSTEM PERFORMANCE
SPECIFICATIONS
INTRODUCTION
127-1.1 BACKGROUND
The Airfield Lighting Control and Monitoring Systems (ALCMS) shall combine state-of-the-art
programming intelligence with high quality, industrial strength components. The system should
represent the leading edge in aviation lighting technology with innovative touchscreen control
stations database storage and retrieval systems.
The ALCMS Manufacturer shall have experience in aviation ground lighting control and be listed
as an FAA approved manufacturer in FAA AC 150/5245-56B.
127-1.2 PROJECT SCOPE
The ALCMS Manufacturer/Contractor shall furnish, install, test and commission a complete and
functional computerized airfield lighting system, L-890BB, per FAA Advisory Circular 10/5345-
56 latest edition.
This project shall include all open architecture software, programming, industrial grade and
commercial computers, programmable logic controllers, touch-screen displays, monitoring devices
and interface hardware, network communication equipment, interconnecting cables, miscellaneous
hardware, cabinets, as-builts, manuals, factory testing, on-site commissioning, on-site testing, on-
site training and any other materials, supervision, labor, all equipment, tools and all incidentals to
provide a fully functional and complete system to the satisfaction of the Owner and Engineer.
Work with Owner and Engineer to develop the controls and touchscreen layouts that are Air Traffic
Controller acceptable to the airport.
Maintain a fully functional and operational airport lighting control system throughout the
installation and testing of the new system. Coordinate construction with the resident engineer to
avoid conflicts with airport operational requirements and to schedule required system outages.
Provide a one year maintenance warranty agreement which shall include the furnishing of key spare
parts along with technical support both remote and on site.
The ALCMS shall include the functionality to fully support basic control and monitoring
requirements. The system shall be configured and installed in such a manner as to facilitate and
minimize future upgrade process. The ALCMS, computer, HMI software and hardware shall be
supplied with the processing capacity, memory and other resources to support the potential growth
indicated in the specification.
127-1.3 QUALIFICATIONS
The ALCMS manufacturer shall be ISO 9001 certified and thus demonstrate a commitment to the
highest quality standards. The ALCMS manufacturer shall be listed in the FAA Approved
Equipment List, AC 150/5345-53 (current edition) and shall be a FAA approved supplier of L-
Addendum No. 3 L-127-2
890BB and shall meet FAA 150/5345-56 current edition for L-890BB Basic monitoring with
latching failsafe.
The Contractor shall designate a superintendent experienced as specified herein for the duration of this project. The superintendent shall be experienced in either similar airfield lighting computerized control systems or airport control systems and installation of airfield lighting vault equipment modifications in excess of $150,000 that has been completed in the last three (3) years. Information documenting the required experience shall be provided. Failure to provide this information that meets this requirement shall cause the Bidder to be considered non-responsive.
A complete detailed list of all proposed equipment and their specification must be submitted with the
bid package. Failure to provide the detailed list may cause the Bidder to be considered non-response.
The Owner and Engineer reserve the right to reject any proposal, which in their opinion does not
meet the system design and standards as specified herein.
127-1.4 PROJECT COORDINATION & CONDITIONS
This project is located on an active airport and work is subject to security and other restrictions.
The existing airport lighting control system shall remain operational during construction and testing
of the new system. The existing control system shall remain operational until the FAA and the
Owner accepts the new system.
The airport will be operational during construction and requires coordination and prior approval
from the Engineer for any planned power and systems outages. All work inside the airport security
fence shall be coordinated with the Engineer, FAA, and Owner.
ALCMS manufacturer shall provide an experienced and qualified Engineering, and Service staff to
support the airport throughout the installation and life of the system.
The project shall follow this basic cycle of events:
Milestone Description
1. Bid Specifications and
Drawings
ALCMS manufacturer reviews specifications and
drawings and prepares submittal
2. Bid Submittal ALCMS manufacturer submits 100% of
equipment and 30% preliminary system riser.
3. Shop Drawings Manufacturer will meet with Owner and
determine preliminary touchscreen layouts. The
manufacturer will send a DEMO CD of the
planned layouts of the touchscreens that will be
used for the control of the ALCMS system to the
FAA, Owner, and Engineer(s). After review, the
Manufacturer shall modify layouts to incorporate
changes made by the Owner/FAA.
4. Production Testing System is tested by ALCMS manufacturer’s
engineering.
5. Installation Contractor installs equipment and completes
external wiring
6. Commissioning ALCMS manufacturer arrives at installation site
to complete commissioning of system and verify
Contractor installation and wiring
Addendum No. 3 L-127-3
7. Initial Training,
Demonstration units in
Tower
Initial training on the system operation and the
Touchscreen is provided prior to system cut-over
8. System Cut-over ALCMS manufacturer and Contractor cut-over
the new system and bring it on-line with
approval of FAA and Owner.
9. Final Testing System is available for final testing witnessed by
FAA, Owner and Engineer(s)
10. Manuals and as-builts ALCMS manufacturer issues operator manuals,
maintenance manuals, ATC manuals and final
as-installed system prints
11. Final Training ALCMS manufacturer completes on-site training
of maintenance and ATC personnel
12. Final Owner Acceptance Upon completion of all contractual requirements,
system is accepted in writing by the FAA and
Owner.
13. Warranty and Support ALCMS manufacturer provides warranty and
support per the contractual requirements which
will be 12 month from the Final Acceptance
A work and staff matrix shall be established by the Contractor to clearly show all personnel
involved in the project and their designated responsibilities and authorities.
127-1.5 SYSTEM PROGRESS REVIEW
A minimum of two (2) trips by the ALCMS Manufacturer/Contractor to the airport shall be
included for progress review meetings with the airport, at no cost to the Owner.
Prior to the progress review meetings, the ALCMS Manufacturer/Contractor shall provide
prototype touchscreen layouts and functionality demonstrations that will allow Air Traffic Control
and the airport to review the screen layouts, colors etc. and provide development feedback.
127-1.6 PRODUCTION TESTING
Before shipment, the ALCMS system shall be assembled as an operating system at the ALCMS
manufacturer’s test facilities. All inputs shall be simulated by actual contact closures or
analog/digital input signals. All outputs shall be connected to simulated loads including visual
brightness level indications. The ALCMS manufacturer shall provide an indicating panel connected
to the each computer to indicate the CCR brightness levels commanded by the ALCMS. The panels
shall be used to determine if the proper outputs of the touch screen at the factory testing and in the
field.
127-1.7 CONTRACTOR INSTALLATION REQUIREMENTS
The installing Contractor/Manufacturer shall be responsible for the physical installation of all
associated ALCMS components. This includes fiber optic cable installation, programmable logic
controllers, monitoring devices and interface hardware, network communication equipment,
miscellaneous hardware, Computers, vault modifications, removal of the existing system, computer
enclosures, all equipment, wiring, and touchscreen control stations and for a complete operational
system in place.
Addendum No. 3 L-127-4
The Contractor shall furnish, install, relocate, connect and test all equipment, equipment
accessories, conduit, cables, wires, buses, grounds and support necessary to insure a complete and
operable electrical distribution facilities for the airport lighting system as specified herein the
submittal package.
The equipment installation and mounting shall comply with the requirements of the National
Electrical Code and local code agency having jurisdiction.
Wire and Connections
a. The Contractor/Manufacturer shall make all necessary electrical connections at
each location in accordance with the ALCMS manufacturer’s wiring diagrams
furnished.
b. All wires called out in the drawings associated with equipment that is to be
controlled or monitored should be pulled, terminated and dressed at the appropriate
terminal blocks and at the associated equipment.
c. In wiring to the terminal blocks, the Contractor shall leave sufficient extra length
on each control lead to make future changes in connections at the terminal block.
d. Contractor/Manufacturer shall provide and install all necessary wiring and
connections for a complete working system in place.
Marking and Labeling
a. All equipment, control wires, terminal blocks, etc., shall be tagged, marked or
labeled as specified below:
b. Wire Identification: The Contractor shall furnish and install self-sticking wire
labels or identifying tags on all control wires at the point where they connect to the
control equipment or to the terminal blocks.
c. Wire labels, if used, shall be of the self-sticking, pre-printed type and of the
manufacturer’s recommended size for the wire involved. Identification markings
designated in the approved shop drawings shall be followed.
d. Tags, if used, shall be nonferrous metal or plastic. Each tag shall be securely tied
to the proper wire by a nonmetallic cord or plastic wire tie.
Installation of Fiber Optic Communication Equipment
a. The Contractor shall install, terminate and test all fiber optic communications
required for the project. This includes all of the following components:
1. Fiber optic cable
2. Fiber optic patch panels
3. Fiber optic jumper cables
4. Fiber connectors / couplings
5. Fiber junction Boxes
Addendum No. 3 L-127-5
b. Installation of the fiber optic communication equipment shall be done by a trained
and qualified fiber optic specialist.
c. The qualifications of the company and specialist to install the fiber optic equipment
shall be submitted for approval.
d. All associated fiber optic equipment including fiber cables, splices, jumper cable
shall be tested upon completion of the fiber cable installation and termination of
connectors.
e. Tests shall include verification that the ‘dB loss versus the distance of the fiber
pull’ is within acceptable limits.
f. All test data shall be recorded and composed into a test report and shall be
submitted to the airport / owner for approval.
g. Commissioning of the system shall not begin until all test reports have been
submitted and approved.
Training Audio/Video Recording
a. All audio/video recording of all ALCMS related training sessions are the
responsibility of the Contractor/Manufacturer.
b. The ALCMS Contractor/Manufacturer shall schedule with a minimum of 48 hour
notice training dates with the FAA and Owner and shall provide all required video
recording personnel and video equipment necessary to record each training
session.
127-1.8 ALCMS CONTRACTOR/MANUFACTURER COMMISSIONING
ALCMS Contractor/Manufacturer shall perform the following commissioning tasks:
a. Verify all connections including power, control and monitoring.
b. Verify proper labeling of equipment.
c. Verify communications between all associated equipment.
d. Perform all hardware calibrations.
e. Perform system testing including control, monitoring and diagnostic.
f. Perform Final Acceptance Testing
127-1.9 INITIAL ON-SITE TRAINING: PRIOR TO CUT-OVER
The ALCMS Contractor/Manufacturer shall provide the FAA and maintenance staff a training
course syllabus and training schedule thirty (30) days before on-site training.
Any audio/video recordings of training classes described herein are the sole responsibility of the
Contractor/Manufacturer. Coordination of the video recording must be organized and approved by
the Engineer, FAA and Owner.
Addendum No. 3 L-127-6
Before system cut-over, the ALCMS Contractor/Manufacturer shall provide two (2), 8 hour (one-
day) training classes for Owner’s maintenance personnel. This “hands” on training will include
the following:
a. System block diagram
b. System assemblies and wiring diagrams
c. Graphical User Interface (GUI) Screens (Hands-on)
d. Touchscreen Operation
e. System maintenance
f. Maintenance and Troubleshooting (Hands-on)
g. Granting local control to the Vault
h. Power up and Power down sequences
i. Failsafe Operations
j. Reporting capabilities
k. Control and monitoring capabilities
Before system cut-over, the ALCMS manufacturer shall provide a minimum of four (4), 1 hour
training classes over the course of a one week time frame for FAA Air Traffic Control (ATC). This
training will include discussion and review of the following:
a. Touchscreen operations
b. Using the presets
c. Alarm and Warning messages
d. Failsafe conditions
e. Granting local control to the Vault
Training classes should be limited to a maximum of 10 people per class and should be scheduled
to coordinate with the different work shifts and personnel over the course of one week.
All training sessions will be held at Henry E. Rohlsen Airport. The ALCMS
Manufacturer/Contractor, shall coordinate with Air Traffic Control and Airport Maintenance to
setup and organizing on-site training for the Airport and FAA personnel. The
Manufacturer/Contractor shall provide tables, chairs, projection screen and all manuals and
drawings. The ALCMS Manufacturer/Contractor shall provide all required visual aids and
projectors. All training sessions shall be video recorded.
127-1.10 FINAL ACCEPTANCE TEST
Following the final installation, commissioning and calibration of the system, ALCMS
Manufacturer/Contractor shall perform a demonstration of the system performance to the
satisfaction/approval of the FAA, Owner and the Engineer. This demonstration shall include the
following:
a. Control functions
b. Alarm functions
c. Display functions
The ALCMS manufacturer shall develop a test plan in accordance with the specifications and issue
this to the Contractor for approval from the Engineer.
The final testing shall be witnessed by the FAA, Owner, and the Engineer.
Addendum No. 3 L-127-7
127-1.11 OPERATION AND MAINTENANCE MANUALS
ALCMS Manufacturer/Contractor shall provide four (4) operation and maintenance manuals that
are hard-covered and suitable for daily operation and maintenance of the system, see Specification
L-106 “Submittals, Record Documents and Maintenance Manuals”. The manuals shall include the
following information:
a. Operational overview and system description
b. Graphical User Interface Screen operation
c. User configuration tools instruction manual
d. Logic and System Block Diagrams
e. Detailed external wiring diagrams
f. Detailed assembly drawings and wiring diagrams
g. Original Equipment Manufacturer (OEM) Manuals
h. Input/Output terminal diagrams
ALCMS Contractor/Manufacturer shall provide four (4) operation manuals for the Air Traffic
Controllers (ATC) that are hard-covered and suitable for daily operation of the system, see
Specification L-106 “Submittals, Record Documents and Maintenance Manuals”. At a minimum,
the manuals shall include the following information:
a. Touchscreen operation (human machine interface)
b. Touchscreen maintenance (i.e. calibration)
The manuals shall be provided in hardbound 3-ring binders. The cover and spine-end of each
binder shall be labeled with all project-related information.
127-1.12 AS-BUILT DRAWINGS
ALCMS Contractor/Manufacturer shall provide four (4) sets of As-Built drawings after system
acceptance, see Specification L-106 “Submittals, Record Documents and Maintenance Manuals”.
The As-Built drawings shall include the following information:
a. System Block Diagram (1-line drawings)
b. System External Wiring Diagrams with all conductors identified
c. Assembly Drawings
d. Assembly Wiring Diagrams
The As-Built drawings shall be 11” X 17” in size and shall be spiral bound or supplied in 3-ring
binders. The cover of each binder shall be labeled with all project-related information.
127-1.13 FINAL ON-SITE TRAINING: CUT-OVER AND SAT COMPLETE
The ALCMS Contractor/Manufacturer shall provide the FAA and maintenance staff a training
course syllabus and training schedule thirty (30) days before on-site training.
Any audio/video recordings of training classes described herein are the sole responsibility of the
Contractor/Manufacturer. Coordination of the video recording must be organized and approved by
the Engineer, FAA and Owner.
Addendum No. 3 L-127-8
After the final acceptance test is complete, the ALCMS Contractor/Manufacturer shall provide two
(2), 8 hour (one-day) training classes for Owner’s maintenance personnel. This “hands” on training
will include the following::
a. System block diagram
b. System assemblies and wiring diagrams
c. Graphical User Interface (GUI) Screens (Hands-on)
d. Touchscreen Operation
e. System maintenance
f. Maintenance and Troubleshooting (Hands-on)
g. Granting local control to the Vault
h. Power up and Power down sequences
i. Failsafe Operations
j. Reporting capabilities
k. Control and monitoring capabilities
After the final acceptance test, the ALCMS manufacturer shall provide a minimum of ten (10), 1
hour training classes over the course of a one week time frame for FAA Air Traffic Control (ATC).
This training will include discussion and review of the following:
a. Touchscreen operations
b. Using the presets
c. Alarm and Warning messages
d. Failsafe conditions
e. Granting local control to the Vault
Training classes should be limited to a maximum of 10 people per class and should be scheduled
to coordinate with the different work shifts and personnel over the course of one week.
All training sessions will be held at Henry E. Rohlsen Airport. The ALCMS
Manufacturer/Contractor, shall coordinate with Air Traffic Control and Airport Maintenance to
setup and organizing on-site training for the Airport and FAA personnel. The
Manufacturer/Contractor shall provide tables, chairs, projection screen and all manuals and
drawings. The ALCMS Manufacturer/Contractor shall provide all required visual aids and
projectors. All training sessions shall be video recorded.
127-1.14 OWNER SYSTEM ACCEPTANCE
Upon successful completion of the final acceptance test, On-site training and any open ‘Punchlist
items’, the Owner shall issue the ALCMS Contractor/Manufacturer a written system acceptance
letter.
‘Punchlist items’ are defined as any remaining contractual requirements that have not been
completed to the satisfaction of the FAA, Owner and the Engineer.
The date of the acceptance letter represents the start of the warranty period.
127-1.15 SYSTEM WARRANTY
The complete system shall be guaranteed to meet or exceed the design and performance requirements
stated in this project specification. Installed equipment, software, and materials, which in the opinion of
Addendum No. 3 L-127-9
the resident engineer do not meet the design requirements, shall be replaced or modified by the ALCMS
Contractor/Manufacturer.
All equipment shall be warranted against defects in workmanship, hardware and software for a
period of twelve (12) months after final acceptance of the Owner. During this time period (12)
months the ALCMS Contractor/Manufacturer shall provide all parts, labor and technical support
with the following conditions:
a. The ALCMS system is guaranteed against mechanical, electrical and physical
defects (excluding lamps) for a period of one year from the date that the ALCMS
system has been formally accepted by the Owner.
b. The Contractor/Manufacturer shall correct by replacement, the equipment or parts
which fail because of mechanical, electrical or physical defects.
c. The Contractor/Manufacturer may examine any goods upon which a claim is made
in the same condition as when defect therein is discovered.
d. Any returns under this guarantee are to be the responsibility of the
Contractor/Manufacturer including transportation charges. For products not
manufactured by, but sold by the manufacturer, the Contractor/Manufacturer is
still responsible for all costs.
127-1.16 SYSTEM SUPPORT
The ALCMS Contractor/Manufacturer’s Service Department shall provide technical assistance and
support during the warranty period. It is required that the supplier of the equipment identify, by
name and telephone number, the person or persons who will be responsible for the proper
performance of the system during the one (1) year warranty period.
The Service Department shall provide 7 days a week / 24 hours a day support phone line. The
support phone number shall be specified in the submittal. The supplier shall have a dedicated phone
line, and shall provide free phone consultation and provide technical phone assistance with in two
(2) hours of the initial call. If requested, the supplier will have technical service at site with in
twelve (12) hours.
127-1.17 SPARE PARTS
A recommended spare parts list shall be included with the Submittal including part numbers and
pricing. These prices shall be valid for (12) months from date of system acceptance.
Provide the following spare parts:
Quantity Description
1 17” Touchscreen
1 Computer, Industrial, to match industrial
hardware supplied, pre-programmed
1 Video Extender
1 Fiber Converter
1 Ethernet Switch
1 Control and Monitoring Unit
Addendum No. 3 L-127-10
1 Current Sensor
1 Voltage Sensor
EQUIPMENT AND MATERIALS
127-2.1 GENERAL
The ALCMS system shall be based on a network ready system that operates within a Windows or
UNIX operating environment. The application, database, and graphic software shall be off the shelf
products, which have been developed to fit the needs of airports.
The database shall be object oriented and constructed by choosing elements from a foundation that
contains a wide range of airport related functional elements.
Friendly definition tools shall be used to modify system parameters, without the assistance of
computer specialists. Airport personnel shall be able to add CCRs and other control elements to the
system by simply installing a computer interface at the new CCR or control element, connecting it
to the local vault network, and adding its parameters to the system through a simple menu driven
interface. The Airport personnel shall have the full capability and software tools available to modify
touchscreen graphics to reflect any desired modifications to the airport visual aids and supporting
systems.
The ALCMS shall be PC-based system for control.
A dedicated fiber optic network shall be used for data transfer between the electrical vault and the
control tower.
The computerized airfield lighting control system shall be comprised of the following major
hardware components:
a. Touchscreen located in the existing tower cab consisting communication
equipment, and UPS.
b. Vault computer subsystem consisting of an industrial enclosure, primary industrial
computer, touch screen, printer, communication equipment, redundant UPSs and
a redundant industrial computer installed in the Airfield Electrical Vault.
The airport lighting control system shall be designed to revert to a fail-safe mode upon computer/plc
failure, communications failure, or loss of power. Under fail-safe conditions, airport lighting
equipment that is operating at the time of failure shall continue to operate at the same intensity
level. Airport lighting equipment not operating at the time of failure shall operate according to an
owner-established plan.
The computers located in the airfield vault shall monitor system operations, commands, operational
parameters and alarms. The ALCMS shall provide basic system level diagnostics and alarm
reporting. Shall at a minimum have the capacity to:
a. Annunciation of a computer malfunction to indicate system is unable to execute
lighting control commands.
Addendum No. 3 L-127-11
b. Annunciation of communication link warnings (1 link failure) and alarm (complete
loss of communication).
c. Annunciation that system is in “Failsafe” to indicate the system is unable to
execute remote lighting control commands and that lighting circuits have switched
to the systems failsafe state. Refer to Section for more detail on failsafe.
d. Annunciation of Vault control interface equipment failure to indicate the system is
unable to execute a lighting control command to a controlled element or group of
elements (i.e. the constant current regulators).
e. Annunciation of loss of system commercial power indicating system is operating
on emergency power.
f. Annunciation of UPS warnings and alarms to indicate possible faults with UPS
equipment (i.e. loss of input power, UPS on inverter, low battery).
g. Feedback that a controlled element (i.e. Runway & Taxiway Lighting) is on or off.
Current Transformers shall be used to provide positive feedback that a controlled
element turned on when it was commanded on and turned off when it was
commanded off and shall provide an analog signal corresponding to the output
current of the controlled element.
h. The system shall monitor the Regulators (CCR), including the true RMS output
current of the CCRs, the true RMS output voltage of the CCR available at the
computer and at the CCR Unit and position of local control switch.
127-2.2 COMMUNICATION NETWORK
The tower and electrical vault computer shall communicate with each other the following dedicated
communication networks:
Fiber Optic Cable
a. The fiber optic cables shall be multi-mode, 850nm/1300nm wavelength, 62.5/125
micron fiber cable. The fiber communication link shall be a minimum of 12 fibers.
b. All fiber optic cable shall be terminated at a Contractor supplied fiber optic patch
panel within each subsystem before being terminated at the communication
equipment.
c. Fiber optic jumper cables shall be provided from the fiber patch panel to the
computer equipment enclosures.
d. Fiber optic cable shall be terminated with ST style connectors at the fiber optic
transceivers located within the vault computer cabinet.
e. Fiber optic runs shall not exceed 2000 meters (6,600 feet) when using multi-mode
fiber optic cable.
f. Fiber optic runs shall be direct point-point runs with no splices.
Addendum No. 3 L-127-12
g. All spare fiber cables shall be pulled and terminated within the fiber optic patch
panel for future expansion.
h. Upon completion of fiber optic installation, the Contractor shall be perform optical
loss (attenuation) measurements and Optical Time Domain Reflectometer (OTDR)
tests on all fiber optic cabling. Provide all test reports to Owner.
i. If any fiber cable loss exceeds either the established optical loss for high speed
transmission or the manufacturer's standards, the Contractor shall correct and/or
replace as necessary.
j. Fiber optic cables shall be terminated in accordance with TIA/EIA -598 - Color
Coding of Fiber Optic Cables.
k. Fiber optic connectors in the accompanied fiber patch panels shall be either a
count of 6, 12 or 48 and accumulate as needed.
l. Fiber optic cable shall be rated by the manufacturer for use in a minimum of
Gigabit, high speed wide and local area network environments.
127-2.3 COMPUTERS
Technical Specifications
1. All the industrial-grade computers in the ALCMS system are identical and
have the following technical specifications:
Options Description
a. Type Industrial-grade computer
b. Processor Type Pentium
c. Processor Clock
Rate
2.83GHz or better
d. Memory Capacity 2 MB RAM minimum
e. Drives 1.44 MB, 3.5”
f. Hard Disk 1.2 GB or larger, IDE
g. Cache Memory 256 kB or better
h. CD-ROM 24X or faster
i. Video SVGA Card, support 1280X1040 or
better
Vault Computer
a. The vault computer shall be capable of independently carrying out the following
functions:
1. Decode all commands received and transfer them for execution.
2. Determine the status of the Constant Current Regulators (CCRs) and other
controllable items.
Addendum No. 3 L-127-13
3. Transfer the status of the CCRs and other controllable items to the control
tower computer, vault computer and all other specified computers on the
network.
4. Continuously check for proper operation of all the communication
networks connected to the computer.
5. Continuously check for proper operation of the vault distributed control
and monitoring network.
6. Duplicate the tower control and graphical displays for allowing authorized
control from the vault(s).
7. The tower touchscreen shall not be able to initiate lighting commands
unless the vault authorizes control to the tower.
127-2.5 TOUCHSCREEN CONTROL STATIONS
Touchscreen Technology Technical Specifications
a. The touchscreen technology shall be integrated into the display monitor(s) and
shall have the following technical specifications:
Options Description
a. Technology Resistive
b. Screen Resolution 1024 X 768 minimum
c. Accuracy Standard deviation of error is less than .080 in.
Equates to less than ±1% error on most displays.
d. Approvals FCC Class B and UL approved
e. Chemical Resistance The active area of the touchscreen is resistant to
all chemicals that do not affect glass.
f. Temperature /
Relative Humidity -20C to 40C at 90% RH, non-condensing
g. Electrostatic Meets Level 4 (15 kV air/8 kV contact
discharges).
h. Construction Surface durability is that of glass, Mohs’
hardness rating of 7
i. Face Plate Anti-glare: 6:1 minimum
j. Optical clarity 90% over visible light spectrum
k. Touch Contact
Requirement
3 ms, with less than 3 ounce touch activation
l. Conversion Speed 22 ms, 19.2kbps
m. Contaminants See Chemical Resistance
n. EMI Unaffected by EMI from other nearby touch
screens, CRT’s, and displays. Unaffected by
environmental EMI.
o. Optical Coating Not required, glass is anti-glare, See Face Plate.
p. Thickness N/A No external overlays or films required.
127-2.6 SUBSYSTEM EQUIPMENT
Touchscreen
a. The touchscreens shall be a 17” LCD monitor display.
Addendum No. 3 L-127-14
b. One touchscreen shall be mounted in the tower cab console and one touchscreen
in embedded in each of the ALCMS cabinet enclosures.
c. 120 VAC, uninterruptible power shall be supplied to each of the touchscreens as
shown on drawings.
d. Surge suppression shall be supplied with all touchscreens and computer systems.
Video / Serial Communication Extension equipment
a. Video / Serial Communication extension Receiver boxes shall be installed in
conjunction with the touchscreen display under the tower cab console.
b. 120VAC, uninterruptible power shall be supplied to the Receiver boxes.
c. Video / Serial Communication extension Transmitter boxes shall be installed in
conjunctions with the tower computer located in the tower junction level
equipment room.
d. A Video / Serial extension cable shall be installed between the Receiver and
Transmitter boxes.
e. The Video Extension equipment shall be manufactured by Cybex™ or approved
equal.
Audible Alarm assembly
a. An audible speaker shall be installed in conjunction with each touchscreen display.
b. An audio cable shall be installed between the audible speaker and the tower
computer/touchscreen.
c. The audible alarm assembly must be designed so that the tone can be disabled
(turned off) and the user can control the volume.
Uninterruptible Power System
a. The UPS shall be capable of supplying full load power for 20 minutes after loss of
main input power.
b. The UPS(s) shall be installed in the tower computer/PLC, vault computer/PLC and
tower cab.
Computer
a. The computers shall be industrial computers.
b. Please refer to the “Computers” section for more detailed information regarding
the technical specifications of the computer.
Addendum No. 3 L-127-15
Industrial Enclosures
a. Industrial enclosures shall be manufactured by Hoffman® or approved alternate.
b. A NEMA 12 industrial enclosure shall be provided for housing associated vault
and tower control equipment.
c. The enclosure shall be designed for indoor use to provide protection against dust,
dirt, dripping water, and external condensation of non-corrosive liquids.
d. The environmental conditions within the area of the enclosure installation shall not
exceed 104F (40C) or fall below 32F (0C).
e. 8”x8” filtered louvers shall be installed in the side of the enclosure
127-2.7 CONTROL EQUIPMENT
The control equipment shall be of a distributed nature and may be a PLC based system.
General
a. Each CCR and each controllable item shall be connected the computer/PLC.
b. The control modules should communicate back to the Vault computer
c. Removal of any control modules from the vault network shall not affect the
operations of the ALCMS system.
d. The control modules shall be a universal device that can be used on any type of
CCR and/or controlled element from any manufacturer.
e. Each control modules shall be identical and have interchangeable components.
f. The control modules unit shall be able to be replaced in the system without shutting
down the entire control system.
Overview of Operation
a. The control modules shall perform the following functions:
1. Brightness setting control of the CCR(s) or ON/OFF control as required
by the controlled element (i.e. generator may only require ON/OFF
control).
2. CCR status monitoring
3. Perform all failsafe functions.
Failsafe
Addendum No. 3 L-127-16
a. Each control module shall provide a self-contained failsafe feature that shall
perform the following functions:
1. Insure default operation of the airport lighting, even if the entire airport
lighting control system is not functioning.
2. Adaptable to each CCR regardless of internal or external control voltage.
3. Permits maintenance of portions of the control system, without changing
the operational status of the lighting system.
4. Upon a failsafe condition, the ALCMS controlled devices must remain on at the
same brightness level prior to failsafe condition.
5. The failsafe device must maintain last state (latched) condition.
6. The failsafe device must maintain last state even after complete loss of power,
including battery backup.
7. Software or firmware within the ALCMS must not be used to maintain last state
condition.
b. The system shall be designed for Passive Failsafe. The failsafe mode of each
control module shall be confirmed with the Owner and FAA during factor testing.
1. Passive Failsafe mode: This mode shall be executed as follows:
a) If the CCR was switched ON before the failure, it shall remain ON
at the same brightness level.
b) If the CCR was switched OFF before the failure, it shall remain off.
c. Technical Specifications
1. The failsafe system shall operate independently of the computer, providing
failsafe interfacing to the CCR and/or other controllable elements.
2. The failsafe system shall be based on electromechanical latching relays
with the following characteristics:
Specification Rating
Maximum switching
voltage
240VAC, 125VDC
Nominal switching
capacity
8A / 250VAC
5A / 30VDC
Rated current (resistive) 5A
Operational Life Mechanical 5X107
Electrical 105
Protection IP67 (protection against ingress of dust and
water in harmful quantities)
d. Mode of Operation
1. The commands executed to switch the CCR and/or controllable element
shall be momentary commands.
2. The control commands shall be mechanically latched upon execution.
3. Failure of the control module and/or loss of communication to the network
shall not change the status of the airport lighting.
Addendum No. 3 L-127-17
127-2.8 EXPANDABILITY
The ALCMS design shall be modular and scalable and provide the airport with a completely
expandable system. The hardware components represent the core of the ALCMS
Contractor/Manufacturer’s modular architecture. Additional Touchscreen Control Stations, Vault
Computers and Constant Current Regulator monitors are added to the system topology using a
simple and user-friendly configuration application.
The system proposed shall include all the necessary tools for easy future changes and additions.
The system must provide industry standard database programs and an object oriented graphic editor
running under a multitasking operating system. These tools will enable on site changes to be made
to the system by airport personnel. The system software shall be re-configurable in the field.
Systems requiring supplier assistance or an off-site computer for routine reconfiguration shall not
be acceptable.
HUMAN-MACHINE INTERFACE OPERATIONAL REQUIREMENTS
127-3.1 GENERAL
The touchscreen display(s) shall control the airfield lighting system. The display shall show real-
time information on the operational status of the airfield lighting systems.
The Touchscreens shall at a minimum include the following in design:
a. A clean screen button to prevent accidental actuation of circuits while cleaning the
screen.
b. Touch buttons or touch sensitive areas must be a minimum of 5/8 inch wide by 1/2
inch high.
c. Separation between touch buttons or touch sensitive areas must be a minimum of
1/8 inch between button/area edges.
d. The system must provide the user with the ability to calibrate the touchscreen.
e. The touchscreen control stations shall consist of multiple touchscreen ‘pages’ each
with a specific function. These touchscreen ‘pages’ shall be defined by the
airport/owner in conjunction with Air Traffic Control requirements. Typical
touchscreen ‘pages’ include the following:
- Preset Page: Consists of pre-defined preset buttons used to simplify
airfield lighting control commands.
- Runway Page: Consists of runway control touch buttons used to
individually control runway circuits. Multiple runway pages may be
necessary for airports with several runways.
Addendum No. 3 L-127-18
- Taxiway Page: Consists of taxiway control touch buttons used to
individually control taxiway circuits. Multiple taxiway pages may be
necessary for airports with several runways.
- Utility Page: Consists of miscellaneous functions for calibrating the
touchscreen, granting lighting control to other locations, setting date and
time etc.
All preset and control configurations shall be defined by the airport/owner in conjunction with Air
Traffic Control requirements. The ALCMS Contractor/Manufacturer shall provide preset tables to
be used by the Owner to define the configuration settings. Changes in the preset tables shall be
allowed during the approval process.
127-3.2 OVERVIEW OF OPERATION
Airfield lighting control commands are entered into the system by touching the corresponding touch
button on the touchscreen video display. When a command is entered, the touchscreen shall
respond by graphically displaying the button as being depressed and change the button color.
The tower touchscreen shall register the command, generate a data instruction and transmit the
command to the vault computer(s) for implementation. The command is also simultaneously
transmitted to all other computer connected to the network.
The tower touchscreen shall receive confirmation from the vault(s) that the corresponding
equipment has responded to the control command and display the current system status on the
touchscreen display.
A “CONFIRM” or “ACCEPT” button to prevent unintentional actuation of circuits and to allow an
operator to authenticate a control action.
A “REJECT” or “CANCEL” button to abort a control action.
The color red must be used for alarm annunciation of circuit graphics and touch buttons.
The color orange must be used for maintenance lockout.
A color legend must be able to be displayed to indicate color representation.
Various colors must be able to be used to indicate the change of runway and taxiway lighting brightness
steps.
Brightness step settings must be indicated by text on the associated circuit button.
In the event that communications is lost between the tower and vault(s), an alarm shall be indicated
at each computer location.
The equipment furnished as part of the control and monitoring system must be suitable for the
environment that it will be operated in. All equipment must be rated to operate in ambient
temperature between 32°/+104°F (0°C/+40°C) at 0-90% relative humidity. The ALCMS
components must be housed in an enclosure (minimum NEMA 12) in accordance with applicable
NEC requirements for the environmental conditions. Additional climate control of the ALCMS
Addendum No. 3 L-127-19
component enclosures may be required based on site conditions. The ALCMS must cause minimal
radiated or conducted electromagnetic interference to other equipment such as computers, radars,
instrument landing systems, radio receivers, very high frequency omni directional radio ranges,
etc., that may be located on or near an airport, or that may use the same power supply.
System shall have sunrise and sunset notification which shall have a visual pop up and be
annunciated at ATC HMI interfaces.
The ALCMS must have provisions for a two photocell and/or air-to-ground radio/pilot controlled
lighting.
127-3.3 USER SOFTWARE CONFIGURATION
The ALCMS shall provide for easy end-user configuration of the airfield lighting control and
monitoring system.
The ALCMS configuration tools shall enable trained personnel to modify their existing system
from any computer on the network.
The ALCMS configuration tools shall allow the following modifications to be implemented to the
system:
a. Install a new control module.
b. Change Touchscreen graphics.
c. Change lighting control methodology.
d. Change lighting preset conditions.
e. Add Touchscreen control circuits / buttons.
f. Add Touchscreen graphics.
g. Add new control and preset methodology.
The ALCMS configuration tools shall function in the following manner to add a new Constant
Current Regulator (CCR) and interface it to a new control module:
a. Open the configuration tools and add a new CCR object
b. Select the new CCR object and set its address and configuration parameters for the
new control module
c. Add a new circuit object.
d. Select the new circuit object and set its configuration parameters.
e. Select CCR object to be controlled by the circuit and inserting the new CCR object
into the new circuit object's control list.
f. Switch the configuration tools to the graphic editor and draw the lines and arcs that
compose the new lighting area on the airfield.
g. Define the newly drawn lines and arcs as a lighting group by selecting them all
with the grouping aid and associate the new group with the new circuit object by
choosing it from the presented list of circuit objects.
Addendum No. 3 L-127-20
h. Create a new touchscreen button by dragging it from the control palette and
dropping it onto the graphical canvas in the desired location.
i. Associate the new button with the new circuit object by choosing it from the
presented list of circuit objects as done previously with the lighting group.
j. Save and distribute the new configuration change by selecting the distribute
configuration option in the main menu of the configuration tools.
The graphic editor shall have the following features:
a. All drawing aids necessary to design any graphical detail required.
b. Integrate dynamic symbols into the graphics map (screen) by selecting an object
from the symbols library.
c. Capable of importing an AutoCAD® or standard drawing exchange format (DXF)
file into the graphic map and make modifications.
d. All definitions and linking of completed graphic objects is performed outside the
graphic editor within the configuration tools application (see section above).
1.7-3.4 SOFTWARE VERSION CONTROL
The ALCMS software includes but is not limited to the software source code, compiled programs,
executable files and PLC ladder logic. All software associated with the ALCMS must be kept under
appropriate version control by the ALCMS manufacturer. Software version control must meet the
following minimum requirements:
a. ALCMS manufacturer must have established ISO certified (current edition)
software control procedures.
b. Proper software coding techniques must be practiced including software remarks
when appropriate.
c. All ALCMS software must be version controlled utilizing a software version
control system.
d. Software versions must be date stamped with the ability to track software changes.
e. All ALCMS software must be stored electronically (i.e. on a network).
f. The network must be backed up with back-up copies stored off site.
127-3.5 ALCMS ALARM FUNCTIONS
Events
a. Events must be annunciated as specified by the airport sponsor and the ATCT to
any part of the HMI system.
Addendum No. 3 L-127-21
b. Events must be logged to a database.
c. Events must be date stamped with date and time of occurrence. This allows for
possible reconstruction of sequences of events within the ALCMS.
d. Events that must be recorded include but are not limited to the following:
- Changes in airport lighting brightness steps
- Changes in states of the computers (start-up, shut-down)
- Changes in states of the communication links (link up, link down)
- Changes in control authorizations (Tower control, Vault control)
- Changes in warning and alarm states.
Warnings
a. The system must provide the ability to classify events as warnings.
b. Warnings must be annunciated at vault HMI interfaces.
c. Warnings must not be annunciated (filtered) at the ATC HMI interfaces.
d. Warnings must be logged to a database.
e. Warnings must be date stamped with date and time of occurrence. This allows for
possible reconstruction of sequences of events within the ALCMS.
f. Warnings that must be recorded include but are not limited to the following:
- Changes in states of the communication links (link up, link down)
- Loss or change in utility status.
Alarms
a. Alarms must be annunciated at maintenance HMI interfaces.
b. Alarms must be annunciated at the ATC HMI interfaces.
c. Alarms must be logged to a file.
d. Alarms must be date stamped with date and time of occurrence. This allows for
possible reconstruction of sequences of events within the ALCMS.
e. Alarms that must be recorded include but are not limited to the following:
- Protective Shutdown of a CCR
- Failure of a controlled element to respond to commanded step
- Loss of communication links (all links down)
- System in “failsafe”
- Loss or change in utility status.
Audible Alarm: The touchscreen audible alarm will function as follows.
Addendum No. 3 L-127-22
a. The audible alarm will sound at each touchscreen display when an alarm condition
occurs. In addition, the ‘ALARM ACK’ button will flash and the associated
graphics will change to red.
b. The audible alarm will stop automatically after three (3) seconds unless the
‘ALARM ACK’ button is pressed.
c. If the alarm is not acknowledged, the audible will cease for sixty (60) seconds
while the ‘ALARM ACK’ continues to flash. If the ‘ALARM ACK’ is still not
pressed after the sixty (60) seconds, the audible will sound again for three (3)
seconds.
d. This sequence will repeat indefinitely until the alarm is acknowledged.
Communication Alarm: Communications monitoring will function as follows:
a. The communications status will be displayed at each touchscreen display and
indicate the current status of the communication links of the ALCMS.
b. ‘Green’ indicates that communications is OK and ‘Red’ indicates that there has
been a communication failure. Detail of the communication failure can be viewed
on the ‘ALARM DISPLAY’ Page.
127-3.6 EVENT MESSAGE HANDLING
The ALCMS shall provide alarming capabilities for each of the monitored data points. Maintenance
personnel shall have the ability to filter each alarm independently by circuit for display at the vault or
ATC locations. Maintenance personnel shall also have the ability to independently specify all alarm
thresholds for each circuit The ALCMS shall have an events storage database for storing and retrieving
events and alarms that must meet the following minimum criteria:
a. Viewing – Events, including warnings and alarms, must be able to be viewed via
a user HMI interface.
b. Subset Viewing - Subset of events, including warnings and alarms, must be able
to be viewed via a subset HMI interface that allows the user to specify a date and
time range to view.
c. Logging – All active and cleared events must be stored to a database designed for
optimal retrieval performance.
d. Date/Time Stamp – Stored events must be stamped with the date and time of
occurrence.
e. Archiving – Events must be stored for a predefined amount of time. Storage time
must be defined by the airport and must be configurable from 1 day to 1 year.
f. Back-up – The ALCMS must provide a method (via HMI interface) for backing
up event database to external media (floppy, CD-ROM, tape or other media).
Addendum No. 3 L-127-23
g. Purging – The ALCMS must provide a method (automatic or manual) for erasing
the events database to allow for hard disk space recovery.
127-3.8 SECURITY ADMINISTRATION
The ALCMS must provide system-wide security administration capabilities. The system must allow a
system administrator to establish user accounts and passwords for end-users and determine each user’s
level of system authorization.
The security feature must be able to record user’s who logon to the system and record events that occur
during the user’s logon period. User accounts are typically set up to be simple, yet allow only those that
have been trained in certain aspects of the system to gain access to these features.
127-3.9 STANDARD REPORTING
Menu selected screens shall be provided to display all the activities and malfunctions which occurred
during a defined time period. At a minimum, the ALCMS must provide the ability to create the following
reports:
a. Events Report – Events, including warnings and alarms, must be able to be saved
to external media or printed to a printer.
b. Subset Events Report - Subset of events, including warnings and alarms, must be
able to be saved to external media or printed to a printer.
c. Constant Current Regulator Report – Current status of all CCR and other
controlled elements including monitoring status must be able to be saved to
external media or printed to a printer.
d. Monitoring Report – Current status of all CCR and other controlled elements
including monitoring status must be able to be saved to external media or printed
to a printer.
e. Operations Report - Record all lighting operations for the system.
f. Coordinate with owner for format of up to (4) additional custom reports.
127-3.10 SYSTEM SOFTWARE RECOVERY
The ALCMS System must provide the ability for complete recovery from system hard drive crashes or
computer malfunction. The system must be provided with backup software that would allow the end-
user to rebuild a computer hard drive for any of the ALCMS computers (Tower or Vault). ALCMS shall
utilize Norton Ghost as recovery software per Airport requirements.
127-3.11 TOUCHSCREEN COMMAND SEQUENCES
The touchscreen control station shall allow the airfield lighting circuits to be controlled individually
(i.e. RWY Edge) or as a group based on preset tables (See following section).
Addendum No. 3 L-127-24
Each control command shall require two distinct operator actions in order for the command to
initiate any state changes of the airfield lighting. The command sequence shall be as follows:
a. Select circuit: Operator selects the desired circuit to be changed.
b. Select intensity: Operator selects the desired brightness step that the circuit is to be
changed to.
c. Confirm/Reject: Operator selects the ‘OK’ button to confirm the selection and
initiate the lighting change. Operator selects the ‘CANCEL’ button to reject the
selections and make another selection.
127-3.12 TOUCHSCREEN PRESET SEQUENCES
The touchscreen control station will allow for simultaneous airfield lighting circuits changes that
will be accomplished with preset lighting sequences. The ALCMS must be able to override preset
lighting configurations as needed using the individual device buttons.
The preset lighting sequences will be defined by the airport in airfield lighting preset tables The
preset settings are established in accordance with FAA Order 7110.65, Air Traffic Control
Handbook, latest revision.
Each preset lighting change shall be based on the following operator inputs:
a. Airport Land & Take Off Operation Selection: Operator selects the East or West
flow direction (i.e. east for runways 8 and 13 or west for runways 26 and 31)
b. Day/Night Setting: Operator selects the day/night setting. The day/night setting
will affect the intensity of the circuits.
c. Visibility: Operator selects a single visibility setting that will be based upon the
Runway Visual Range (RVR) options of the airport.
d. Confirm/Reject: Operator selects the ‘OK’ button to confirm the preset selections
and initiate the lighting change. Operator selects the ‘CANCEL’ button to reject
the selections and make another preset selection.
Upon confirmation of the preset selections, the intensity of all the circuits associated with the preset
condition shall automatically change to match the visibility requirement.
127-3.13 CONTROL METHODOLOGY
The touchscreens control methodology will function based on the following tables. These tables
outline each touchscreen button and the associated CCRs, circuits and other airfield equipment that
is controlled by the button.
The visibility settings of the Regulators shall be based on the following tables that were taken from
FAA document 7110.65.
Addendum No. 3 L-127-25
Table 1: HIRL 5-step Regulators
Visibility Day
(Brightness step)
Night
(Brightness
step)
Less than 1 mile 3 3
1 to but not including 2
miles 3 2
2 to 3 miles 2 2
More than 3 miles 0 1
Table 2: 3-step MIRL Regulators
Visibility Day
(Brightness step)
Night
(Brightness
step)
Less than 1 mile 3 2
1 mile or more 0 1
Table 2: 3-step Taxiway Regulators
Visibility Day
(Brightness step)
Night
(Brightness
step)
Less than 1 mile 1 1
1 mile or more 0 1
Table 3: 1-step Equipment
127-3.14 CONTROL METHODOLOGY
The touchscreen control methodology will function based on the following tables. These tables
outline each touchscreen button and the associated CCRs, circuits and other airfield equipment that
is controlled by the button.
Touchscreen Button Circuits Activated
ALL CCR R/W R10A
CCR R/W R10B
CCR R/W R10S
CCR T/W AW
CCR T/W AE
WINDCONE
Visibility Day (Brightness
step)
Night
(Brightness
step)
Less than 1 mile 5 4
1 to but not including 2
miles
4 3
2 to but not including 3
miles
3 3
3 to 5 miles inclusive 0 2
More than 5 miles 0 1
Addendum No. 3 L-127-26
Table 5: Airfield Preset Page
Touchscreen Button Circuits Activated
RW 10-28 CCR R/W R10A
CCR R/W R10B
CCR R/W R10S
Table 6: Runway Lights Page
Touchscreen Button Circuits Activated
TW A CCR T/W AW
CCR T/W AE
WINDCONE WINDCONE
Table 7: Taxiway Lights Page
Touchscreen Button Circuits Activated
GEN STATUS GENERATOR
UTILITY STATUS UTILITY
Table 8: Utility Page
127-3.15 GRAPHICAL AIRPORT PICTORIAL
The ALCMS display screens will display a graphical pictorial representation of the airport runways,
taxiways and other requested airport features.
When there is a change in a lighting system status, the appropriate detail of the graphic will indicate
the status by changing color.
The circuit intensity display colors will be represented as seen in the legend as follows. Due to the
limitations of the color printer, the printed colors you see will not match the actual colors as they
will appear on the touchscreen(s):
The status monitoring display colors will be represented as seen in the legend as follows. This
includes ATS monitoring, Generator monitoring and communications monitoring:
STEP 0
STEP 1
STEP 2
STEP 3
STEP 4
STEP 5
COLOR LEGEND
STEP 1
STEP 2
STEP 3
STEP 0DARK GRAY
DARK BLUE
DARK GRN
MAGENTA
LIGHT GRN
CYAN
Addendum No. 3 L-127-27
127-3.16 PRESETS
Presets shall be inclusive but not limited to the following inputs:
Runway Operations (across) Step 10 28
Circuit Descriptions (below)
Runway Edge R10A 5 1 1
Runway Edge R10B 5 1 1
Runway Sign R10S 3 1 1
T/W AW 3 1 1
T/W AE 3 1 1
Windcone 1 1 1
Preset Table: Night > 5 miles
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 0 0
Runway Edge R10B 5 0 0
Runway Sign R10S 3 0 0
T/W AW 3 0 0
T/W AE 3 0 0
Windcone 1 0 0
Preset Table : Day > 5 miles
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 2 2
Runway Edge R10B 5 2 2
Runway Sign R10S 3 1 1
T/W AW 3 1 1
T/W AE 3 1 1
Windcone 1 1 1
Preset Table: Night 3 to 5 miles
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 0 0
Runway Edge R10B 5 0 0
OFF
ALARM
EMERGENCY
NORMAL
COLOR LEGEND
DARK BLUE
DARK GRN
RED
YELLOW
GREEN
Addendum No. 3 L-127-28
Runway Sign R10S 3 0 0
T/W AW 3 0 0
T/W AE 3 0 0
Windcone 1 0 0
Preset Table: Day 3-5 miles
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 3 3
Runway Edge R10B 5 3 3
Runway Sign R10S 3 1 1
T/W AW 3 1 1
T/W AE 3 1 1
Windcone 1 2 2
Preset Table: Night 2-3 miles
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 3 3
Runway Edge R10B 5 3 3
Runway Sign R10S 3 1 1
T/W AW 3 0 0
T/W AE 3 0 0
Windcone 1 1 1
Preset Table: Day 2-3 miles
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 3 3
Runway Edge R10B 5 3 3
Runway Sign R10S 3 1 1
T/W AW 3 1 1
T/W AE 3 1 1
Windcone 1 1 1
Preset Table: Night 1-2 miles
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 4 4
Runway Edge R10B 5 4 4
Runway Sign R10S 3 1 1
T/W AW 3 0 0
T/W AE 3 0 0
Windcone 1 1 1
Preset Table: Day 1-2 miles
Addendum No. 3 L-127-29
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 4 4
Runway Edge R10B 5 4 4
Runway Sign R10S 3 1 1
T/W AW 3 2 2
T/W AE 3 2 2
Windcone 1 1 1
Preset Table: Night <1 mile
Runway Operations (across) 10 28
Circuit Descriptions (below) Step
Runway Edge R10A 5 5 5
Runway Edge R10B 5 5 5
Runway Sign R10S 3 1 1
T/W AW 3 3 3
T/W AE 3 3 3
Windcone 1 1 1
Preset Table: Day <1 mile
RADIO PILOT CONTROL
Runway Operations (across) Step 10 28
Circuit Descriptions (below)
Runway Edge R10A 5 1 1
Runway Edge R10B 5 1 1
Runway Sign R10S 3 1 1
T/W AW 3 1 1
T/W AE 3 1 1
Windcone 1 1 1
Preset Table Night 3 click
Runway Operations (across) Step 10 28
Circuit Descriptions (below)
Runway Edge R10A 5 3 3
Runway Edge R10B 5 3 3
Runway Sign R10S 3 1 1
T/W AW 3 2 2
T/W AE 3 2 2
Windcone 1 1 1
Preset Table Night 5 click
Runway Operations (across) Step 10 28
Circuit Descriptions (below)
Runway Edge R10A 5 5 5
Runway Edge R10B 5 5 5
Runway Sign R10S 3 1 1
T/W AW 3 3 3
Addendum No. 3 L-127-30
T/W AE 3 3 3
Windcone 1 1 1
Preset Table Night 7 click
METHOD OF MEASUREMENT
Payment will be made at the contract unit price for each completed and accepted vault equipment
installation. This price shall be full compensation for furnishing all materials and for all preparation,
assembly, and installation of these materials, and for all labor, equipment, tools, and incidentals
necessary to complete the item.
BASIS OF PAYMENT
No direct payment shall be made for the work described in this section. The work described in this
section is incidental to bid items in section L-109 and shall be paid for in the respective bid item of
which it is a component part.
END OF ITEM L-127
Addendum No. 3 263200 - 1
SECTION 26 32 00 – PACKAGED GENERATOR ASSEMBLIES
PART 1 GENERAL
1.01 RELATED REQUIREMENTS
A. The General Provisions, Supplemental General Provisions, Special Provisions and Division 1
Specification Sections apply to Work covered by this Section.
B. Comply with other Division 26 Sections, as applicable and as noted herein. Refer to other Divisions
for coordination of the Work.
C. Automatic electrical transfer equipment: furnished separately under section 26 36 00.
1.02 SCOPE OF WORK
A. Provide labor, materials, equipment, tools and services, and perform operations required for, and
reasonably incidental to the providing of a UL2200 Listed standby engine-generator (EG) system
with an outdoor weather protective enclosure mounted on top of a sub base diesel fuel tank, for
automatic and manual operation for the transfer of electrical power to the connected Facility loads,
including all stairs and platforms, related systems and accessories for a complete working installation
in place. The furnished generator set shall meet all applicable Tier level emission and certification
requirements of United States Environmental Protection Agency’s (U.S. EPA) standards and
regulations.
B. It is the intent of these Specifications that there is a single source of supply and responsibility for the
entire specified EG system to include the new engine generator set and accessory equipment. Due to
the coordination required between the related systems, the engine generator supplier (EG vendor)
shall be the responsible party, through the Installing CONTRACTOR, and supply the entire system as
a unit, less installation materials and installation to be furnished by the Installing CONTRACTOR.
The EG vendor shall coordinate with the Installing CONTRACTOR for installation requirements and
actual equipment dimensions for foundation installation and all mechanical and electrical interface
requirements.
C. The work covered by this Specification consists of the supply and testing of a standby power duty
rated diesel electric generator set with standby ratings as indicated herein. The entire engine-
generator system (EG) shall be furnished by the EG vendor which shall include, but not necessarily
be limited to, the following basic components:
1. Diesel engine.
2. Generator.
3. Generator mounted AC main power circuit breakers.
4. Engine-mounted radiator closed loop-cooling system.
5. Weather protected enclosure and appurtenances.
6. Exhaust system with high degree sound attenuating silencer as specified herein.
Addendum No. 3 263200 - 2
7. Generator starting / control battery and automatic battery charger.
8. Generator set spring vibration isolators.
9. Engine-generator set system accessory equipment items.
10. Generator system status annunciation signals.
11. Generator Remote Annunciator Panel (for mounting in building)
12. Fuel Monitoring Panel
13. Access stairs with handrails at all access doors.
1.03 SYSTEM DESCRIPTION
A. System Operation
1. The standby engine-generator (EG) system shall be the manufacturer’s standard production
model nameplate rated to have a minimum rating and site capability of 200KW, 250KVA
Standby Power, at 0.80 power factor, 277/480 volt AC, 3-phase, 4-wire, 60 hertz. The generator
set shall be capable of properly transferring electrical power to the connected Facility’s electrical
loads. The generator set system, including equipment and operation, shall, in its entirety, be
designed, manufactured, and installed so as to comply with NFPA 110, Level 1, type 10
requirements and in accordance with all other applicable Codes, including those indicated herein.
B. System Function
1. The EG system shall include the capability of the generator set being automatically controlled for
start, run, and stop by the generator set automatic transfer switch equipment controls. Provide
selectable manual generator set start and stop controls. Upon engine crank initiation, the new
generator set shall start, attain rated speed and voltage, and be able to accept rated electrical load
within ten (10) seconds from the issue of generator set start initiation. The engine mounted speed
governor shall automatically control generator set speed, while the generator mounted automatic
voltage regulator shall control generator output voltage regulation. Manual adjustment of
generator speed and voltage shall also be provided with the generator-mounted controls.
C. Site Conditions
1. The operating environment of the standby engine-generator system shall be:
Altitude: ....................................................................................................... maximum of 100 ft
Outdoor temperature: maximum of .................................................................................. 110 °F
Outdoor temperature: minimum of ................................................................................... 30 °F
Engine jacket water/glycol: ......................................................................................... 50%/50%
Installation type: ........................... Inside an outdoor non-walk-in weather protective enclosure
Fuel type: .......................................................................................Standard No. 2 diesel fuel oil
Addendum No. 3 263200 - 3
Cooling system type: .................... Generator set mounted closed loop radiator with blower fan
Exhaust system: ............................................... inside of the of the generator outdoor enclosure
D. System Performance
1. The standby engine-generator system shall conform to the following general performance
criteria:
a. Rating - Engine brake horsepower shall be sufficient to deliver full rated engine-generator
set KW / KVA when operated at rated rpm and equipped with all engine-mounted parasitic
and external loads as installed within the generator outdoor enclosure within the site
condition parameters.
b. Conditions - the rating shall be based on ISO-3046/1 conditions of 29.53 in Hg and 27°C
(81°F).
c. Fuel - Diesel engines shall be able to deliver rated power when operating on standard No. 2
diesel fuel having 35 degree API (16°C or 60°F) specific gravity.
d. Fuel Consumption - Diesel fuel rates shall be based on fuel having a low heating value
(LHV) of 18,390 Btu / lb when used at 29°C (85°F) and weighing 7.001 lb / U.S. gal.
e. Start Time and Load Acceptance – Generator set shall start, achieve rated voltage and
frequency, and be capable of accepting load within 10 seconds from start initiation when
properly equipped and maintained with all installed and specified parasitic loads.
f. Block Load Acceptance - Transient response shall conform to ISO 8528 requirements.
1.04 REFERENCE STANDARDS
A. The standby engine-generator set system equipment shall be designed, manufactured,and tested in
strict accordance with the latest edition of the specific component manufacturers’ governing
standards. The design, manufacture, assembly, installation, and operation of all elements of the
engine generator system herein specified shall be in accordance with, but limited to, published
standards, guidelines, and requirements of the following as applicable:
1. American Society of Mechanical Engineers (ASME).
2. Diesel Engine Manufacturers Association (DEMA).
3. Electrical Generating Systems Association (EGSA).
4. International Standards Organization (ISO).
5. Institute of Electrical and Electronics Engineers (IEEE).
6. National Electrical Code (NEC).
7. National Electric Manufacturers Association (NEMA).
8. National Fire Protection Association (NFPA).
Addendum No. 3 263200 - 4
9. Occupational Safety and Health Administration (OSHA).
10. Society of Automotive Engineers (SAE).
11. Underwriters Laboratories (UL), including UL2200
12. Department of Environmental Protection (DEP).
13. American National Standards Institute (ANSI).
14. American Welding Society (AWS).
15. International Building Code (IBC).
16. United States Environmental Protection Agency (US EPA) – New Source Performance Standard
(NSPS).
17. Local Authorities Having Jurisdiction (AHJ) and any local Code and regulation requirements.
B. The generator set to be furnished shall not be released for manufacture until the ENGINEER has
reviewed and approved the generator equipment Shop Drawings, no exceptions. The generator set
shall be Manufacturer designed, built, and certified to meet the applicable Tier level emissions
requirements of the United States Environmental Protection Agency’s (U.S. EPA) New Source
Performance Standard for Stationary Reciprocating Compression Ignition Engines (NSPS) rules and
regulations in affect at the time of generator manufacture and shipment.
1.05 QUALITY ASSURANCE
A. The complete engine generator set, and all related systems, accessories and equipment shall be
furnished by one (1) supplier (EG vendor), thus ensuring that the responsibility for performance to
this Specification shall not be divided among individual suppliers and thereby assuring high standards
of quality, coordination, reliability, and service for the EG system. The complete provision and
performance responsibility for all of the furnished generator equipment shall be assumed solely by
one primary vendor who shall directly deliver, service, test, and commission all of the furnished
generator set and accessory generator system equipment. The EG vendor shall be the engine
generator manufacturer’s factory authorized direct distributor, who maintains complete local sales,
parts, and service facilities and provision in the field of electric power generation on direct behalf of
the manufacturer of the engine generator set to be furnished, including factory trained mechanics and
technicians and engine generator replacement parts for the unit supplied. Second level manufacturer’s
sub-dealers or redistribution suppliers do not comply with this requirement and shall not be accepted.
B. The complete generator set, including engine, generator, base, and radiator shall be designed, built,
and assembled as a complete unit by the engine manufacturer, shall be complete in all respects and
shall include all equipment and controls necessary for a fully operational alternative electric power
supply. All system components shall have been designed and built to achieve optimum physical and
performance compatibility and prototype tested to prove integrated design and operational capability.
C. All materials, generator equipment, and parts provided shall be new and unused of current design and
of the highest grade. The generator set package shall be manufactured and assembled at the engine
generator set Factory and shipped by the manufacturer only after the generator set equipment Shop
Drawings have been reviewed and approved by the ENGINEER, no exceptions.
Addendum No. 3 263200 - 5
D. The EG vendor must be the engine generator manufacturer’s factory authorized direct distributor and
must maintain service facilities with service and parts personnel available to the OWNER on a 24-
hour / 365 day basis. Proof of this requirement shall be provided by the EG vendor and included in
the Shop drawing submittals. Inspection of the EG vendor’s facility may be made by the ENGINEER
in order to substantiate this requirement.
1.06 SUBMITTALS
A. Submit eight (8) bound copies Shop Drawing Submittals to include EG system product data,
technical information, and detailed mechanical, electrical and structural drawings indicating
compliance for all engine generator equipment, products, operations, performances, interfaces, and
services as specified herein.
B. The following information shall be provided for all furnished equipment:
1. A copy of this Specification Section, with all related Project Addendum updates included, and all
referenced and applicable Sections, with Addendum updates included, with each paragraph
check-marked to indicate Specification compliance or marked to indicate requested deviations
from Specification requirements. Check marks () shall denote full compliance with a paragraph
as a whole. If deviations from the Specifications are indicated, and therefore requested by the
CONTRACTOR, each deviation shall be underlined and denoted by a number in the margin to
the right of the identified paragraph. The remaining portions of the paragraph not underlined
shall signify compliance on the part of the CONTRACTOR with the Specifications. The
submittal shall be accompanied by a detailed written explanation and justification for each
requested deviation.
C. Engine-Generator Set
2. Component List – Provide a detailed breakdown by manufacturer and specific part number
including associated technical data of all components and options to be provided.
3. Technical Data - Manufacturer's specifications and data sheets identifying make and model of
engine and generator, and including relevant component design and performance data as
determined from Factory prototype testing of the specific engine generator set package proposed
to be furnished. All Prototype testing shall not be performed on the specific generator set
equipment to be furnished for this project.
4. Major System Equipment :
a. Dimensions:
1) Length.
2) Width.
3) Height.
b. Weight:
1) Dry.
2) Wet.
Addendum No. 3 263200 - 6
5. Engine:
a. Type, aspiration, compression ratio, and combustion cycle
b. Bore, stroke, displacement, number of cylinders, and operational speed in RPM
6. Generator:
a. Insulation class.
b. Number of leads.
c. Excitation type.
d. Temperature rise rating.
e. Insulation type and method.
f. Harmonic, SCR loading capability.
g. Generator set at rated load, voltage, and power factor.
h. Efficiency at 0.80 PF for: 50 % load, 75 % load, 100% load.
i. Time constants, short circuit transient (T'D).
j. Time constants, armature short circuit (TA).
k. Reactance, sub-transient - direct axis (X"D).
l. Reactance, transient - saturated (X'D).
m. Reactance, synchronous - direct axis (XD).
n. Reactance, negative sequence (X2).
o. Reactance, zero sequence (X0).
p. Fault current, 3-phase symmetrical.
q. Damage and Decrement curve.
r. Short circuit ratio.
s. Stator winding coil pitch.
7. Provide the following Manufacturer’s engine generator set package prototype technical data for
the following minimum operating loads: 1/4, 1/2, 3/4, and at full load:
a. Engine horsepower rating (BHP) at 0.8 power factor.
b. Generator set electrical KW output at standby rating.
Addendum No. 3 263200 - 7
c. Standard condition fuel consumption.
d. Combustion air inlet flow rate.
e. Radiator airflow.
f. Maximum radiator / ventilation airflow restriction.
g. Exhaust gas flow rate.
h. Exhaust stack temperature.
i. Exhaust system backpressure restriction (maximum).
j. Exhaust emissions data at varying loads.
k. Heat rejection to atmosphere from generator.
l. Heat rejection to atmosphere from engine.
m. Mechanical sound data (Overall and at different frequencies and varying distances).
n. Exhaust sound data (Overall and at different frequencies and varying distances).
8. Provide engine generator set manufacturer’s transient analysis graphs indicating generator set
maximum and minimum instantaneous transient response of both frequency and voltage, relative
to time, for the generator set when imposing the following electrical single step block load
changes on the generator set at rated power factor:
a. 0 to 25% to 0%.
b. 0 to 50% to 0%.
c. 0 to 75% to 0%.
d. 0 to 100% to 0%.
9. Auxiliary Equipment - Specifications and data sheets and drawings, including, but not
necessarily limited to: vibration isolators; governor; voltage regulator; generator circuit breaker;
battery charger; generator starting/control battery; jacket water heaters; exhaust muffler; exhaust
flex; exhaust system components, outdoor weather protective enclosure, stairs, handrails and
platforms, and sub base tank, etc.
10. Drawings – Provide detailed dimensional drawings showing overall engine-generator set;
generator circuit breaker and muffler measurements. Include mounting locations and
interconnecting wiring and terminations for AC power load leads, customer interface points, AC
service and all AC / DC control interfaces. Include fuel, exhaust, and cooling systems piping
arrangements and interfaces, and oil drain lines.
11. Wiring Diagrams – Provide electrical wiring diagrams, schematic diagrams, and control panel
outline drawings published by the manufacturer for engine-generator set controls and for the
associated electrical accessory equipment items including all interconnections for remote
Addendum No. 3 263200 - 8
automatic control, transfer, and communication. Show, and properly identify, point-to-point
electrical interconnections and logic diagrams of the entire engine generator assembly for
ENGINEER review and for applicable wiring interface information for use by the Installing
CONTRACTOR.
12. Warranty Statements – Provide details of the engine generator vendor’s furnished warranty
coverage to the OWNER including warranty information as published by the respective
manufacturers of the furnished component equipment. In no case shall the warranty coverage and
warranty period for the complete furnished EG system be less than specified herein.
13. Service – Provide details of location and description of EG vendor's parts and service facility and
number of qualified generator set service personnel.
14. Maintenance Contract – Provide detailed outline and description of the EG vendor’s service
maintenance contract to be furnished for the generator set equipment as specified herein. Include
details of the items and services covered within the maintenance service contract.
15. Engine Oil Sampling Service – Provide description of service provided, recommended frequency
of analysis service, and details of procedures.
1.07 SERVICE AND WARRANTY
A. The EG vendor shall be directly capable, without subcontracting, of providing factory trained
servicemen, the required stock of replacement parts, technical assistance, and complete equipment
warranty administration.
B. Warranty Administration
1. The EG vendor shall be capable of, and solely responsible for the direct implementation and
administering of the engine, generator, and all other components manufacturer's warranties.
Subcontracting or rerouting of these services to other service organizations by the EG vendor is
not acceptable.
C. Warranty Terms
1. All of the generator system equipment furnished under this Section shall be guaranteed against
defects in material, parts, and workmanship. The generator system equipment warranty and
associated coverage shall be for a period of five (5) years (60 months). The warranty shall be
comprehensive covering all EG vendor furnished generator system equipment including proper
operation. All generator system equipment, including, but not limited to all generator system
accessory items furnished by the EG vendor shall be covered by this comprehensive 5 year
warranty. There shall be no warranty related charge deductibles or associated service fees
applicable to the OWNER for EG vendor furnished warranty services for the entire duration of
the specified warranty period. The generator equipment warranty coverage shall commence after
satisfactory EG vendor startup of the generator set either on the date of beneficial use of the
generator set or on the date of acceptance by the OWNER, whichever occurs first, and shall
include all EG vendor furnished labor, parts, travel time, expenses, and generator equipment
expendable items (lubricating oil, coolant, filters, gaskets, and other serviceable items made
unusable or required to be replaced by the warrantable defect) necessary for implementation and
completion of all warrantable equipment repairs or corrective actions furnished by the generator
supplier at the job site or elsewhere. Provided the generator system is operated properly within
Addendum No. 3 263200 - 9
the standby generator set application as specified herein, generator set running hours shall not be
a limiting factor for the generator system equipment warranty provision, either by the
manufacturer or by the generator equipment supplier. The furnished generator set battery is
considered a consumable item and shall be 100% warranted by the EG vendor for a period of two
(2) years from the date of generator set startup.
2. The EG system Shop Drawing Submittals and furnished generator system parts, operation and
maintenance manuals must include written warranties and supporting documentation clearly
indicating and certifying complete compliance to these specified warranty requirements for all
generator system equipment furnished by the EG vendor, no exceptions. Failure of the generator
equipment Supplier to provide the OWNER with the specified warranties and associated
warranty services shall be sufficient cause for rejection of the equipment and the EG vendor.
3. The EG vendor must maintain and be able to provide factory trained and qualified service
personnel, the specified local stock and availability of replacement or repair parts, technical
support assistance, and complete warranty administration on direct authorized behalf of the
furnished generator equipment Manufacturers. These warranty services shall be available to the
OWNER from the EG vendor on a 365 day / 24 hour basis. Subcontracting or rerouting of any of
these warranty related services by the EG vendor to other repair or service providers is not
acceptable.
4. Warranty Nameplate A warranty nameplate shall affixed to the generator set with the following
data:
a. Warranty coverage period:
b. Start-up date:
c. Termination date:
d. Engine and generator serial number information:
e. Engine and generator arrangement information:
f. EG vendor name:
g. EG vendor address:
h. EG vendor normal business telephone number:
i. EG vendor 24-Hour emergency telephone number:
j. Warranty service contact information:
k. Preventive maintenance to be performed by:
D. The EG vendor shall guarantee 100% parts availability within 48 hours from the time of any service
repair request or when an order is entered with the EG vendor.
E. Service Maintenance Contract
Addendum No. 3 263200 - 10
1. The engine-generator set supplier shall provide a five (5) full year service maintenance contract
for the furnished generator set, including annual engine oil change and proper disposal of
removed engine oil for the new generator set. It shall include four (4) routine scheduled
maintenance service visits per each year with a complete engine oil change on the fourth visit
each year. The service maintenance contract shall commence on the date of acceptance by the
OWNER. The EG vendor shall maintain 24 hour / 365 day emergency access to an EG vendor
account manager to expedite emergency repairs including service labor scheduling and parts
replacements. The EG vendor must furnish this contract and associated services directly to the
OWNER, not through an alternate company, supplier or service provider.
2. The generator set service maintenance contract furnished shall protect the OWNER from any
parts or labor price increases. The EG vendor’s service maintenance agreement contract shall be
optionally available for purchase extension by the OWNER at the end of the specified five (5)
year service maintenance agreement. The EG vendor shall maintain the following for the entire
duration of the specified generator set five (5) year warranty period.
a. Qualified mechanics, technicians, and service / repair equipment.
b. The EG vendor shall have factory trained service representatives and all tooling necessary
to test, maintain, and repair all provided equipment as necessary.
c. Specified generator set parts availability must be maintained by the EG vendor for a
minimum of fifteen (15) years from date of generator equipment startup.
d. The EG vendor shall have locally available at all times parts inventory stock of not less than
90% of all engine replacement parts and must maintain generator equipment service and
parts availability on a 365 day / 24 hour basis. Proof of this requirement shall be provided
by the EG vendor and inspection of the EG vendors local facility may be made by the
ENGINEER in order to substantiate this requirement.
F. The EG vendor shall guarantee 100% parts availability within 48 hours from the time of any service
repair request or when an order is entered with the EG vendor.
G. Oil sampling analysis service
1. The EG vendor shall be capable of performing and shall provide a scheduled oil sampling service
to monitor engine oil condition on an ongoing basis. The sampling method shall be of the atomic
absorption spectrophotometry method as opposed to the spectrographic analysis method and shall
be accurate to within a fraction of one part per million for the following elements.
a. Iron
b. Chromium
c. Copper
d. Aluminum
e. Silicon
f. Lead
Addendum No. 3 263200 - 11
g. Water
h. Fuel
i. Antifreeze
2. In order to provide oil sampling analysis service for the End User for the duration of the Five (5)
year extended warranty period, the EG vendor shall provide One (1) scheduled oil sample kit
consisting of two (2) oil extraction pumps, twenty (20) oil sample plastic bottles twenty (20)
prepaid mailing containers and written instructions. The mailed oil samples shall be analyzed at
the EG vendor's local facility by factory trained and certified personnel. Immediate notification
of the analysis results of each analysis shall be provided to the OWNER in written report format
with written advisement of any remedial action requirements and recommendations. The
scheduled oil sampling analysis program shall be optionally available to the OWNER by the EG
vendor beyond the specified five year warranty period.
PART 2 PRODUCTS
2.01 ACCEPTABLE GENERATOR SET MANUFACTURERS
A. Cummins: Cummins Power South, LLC
B. Caterpillar, Inc.: Pantropic Power, Inc.
C. Or approved alternate.
2.02 ENGINE-GENERATOR SET
A. Engine
1. The engine shall be a stationary, diesel cycle, compression ignition; liquid cooled, 1800-RPM,
four-stroke design, inline or V-type, with dry exhaust manifolds. Two stroke engines are not
acceptable.
2. The engine generator set package shall be capable of one step load acceptance of 100% rating
with voltage dip not to exceed 25% of rated voltage and stabilized recovery within 7.5 seconds.
Generator set Manufacturer’s confirmation documentation of this transient loading capability
shall be included in the generator system Shop Drawing Submittals.
3. The engine shall be equipped with air filters, engine driven fuel pump, fuel filters, fuel pressure
gauge, engine driven lubricating oil pump and cooler, lubricating oil filters, oil pressure gauge,
engine driven water pump, coolant temperature gauge, service hour meter, flywheel and housing,
and any other items required to provide proper engine generator set operation.
4. The design of the basic engine shall provide for maximum structural integrity to extend service
life. Engines using multiple engine crankshafts are not acceptable. All materials used in the
engine shall incorporate the highest level of current proven metallurgical and manufacturing
technology.
B. Lubrication System
Addendum No. 3 263200 - 12
1. The lubrication system shall include an engine driven mechanical positive displacement oil
pump, full flow filtration with replaceable elements and a bypass valve to continue lubrication in
the event of filter clogging, flexible oil lines and oil cooler. The bypass valve shall be integral
with the engine filter base or receptacle.
2. The engine shall be furnished with flexible hoses sufficiently long enough to route and direct the
engine’s crankcase ventilation fumes to the inside of the radiator discharge airflow plenum.
3. Provide a flexibly connected engine lubricating oil sump drain line terminated with a stainless
steel N.P.T. threaded cap. Furnish a removable handle isolation shutoff valve in the oil drain line
extended from the engine sump drain. The engine oil sump drain line beyond the valve shall be
flexible and terminated on the outside of the generator set outdoor weather protective enclosure
with a stainless steel N.P.T fitting and a threaded stainless steel cap. Provide a permanently
installed “Engine Oil Drain” nameplate secured to the enclosure wall next to the drain fitting.
C. Fuel System
1. The generator set fuel system shall be integral with the engine. It shall consist of a fuel filtration
system, engine mounted mechanically driven transfer pump, injection pumps or electronic fuel
control and delivery system, and flexible supply and return fuel lines. The transfer pump shall be
engine driven and shall deliver fuel under low pressure to the engine’s fuel injection system.
The system shall be capable of delivering fuel flow from the sub base fuel tank to the engine fuel
inlets or nozzles, sufficient for full rated operation of the engine under all ambient temperature
conditions and shall return any unused fuel to the sub base fuel tank. The engine’s air intake,
turbo charger and governor and fuel control systems shall properly operate to deliver fuel to the
engine at rated engine horsepower and full rated generator output when operating on diesel fuel
oil. No overheating of any engine component or system shall occur when operating at full rated
load on diesel fuel as installed inside of the furnished weather protective enclosure within the
atmospheric parameters as specified herein.
2. Unit fuel injectors or electronic fuel injection systems shall be designed for optimal and efficient
fuel combustion and engine performance at the rated engine horsepower while complying with
the US EPS and local Authority Having Jurisdiction engine emissions standards and
requirements.
3. Provide a fuel supply fuel filter / water separator system installed on the engine. The filter shall
have a clear sediment containment bowl and drain valve. The engine fuel return shall be flexibly
connected to the sub base tank fuel return. The fuel filter shall be Racor model 500 FGSS as
manufactured by Parker Hannifin Corp., Modesto, California.
4. For engines utilizing the fuel system as a portion means of cooling the engine during operation,
or where a large amount of heat is transmitted to the engine’s unused return fuel, the fuel shall be
piped with flexible connections from the filter/water separator system to the intake of the engine
fuel pump and then from the engine’s fuel return through a generator manufacturer furnished
radiator mounted diesel fuel oil cooler for return of cooled fuel to the sub base tank. The fuel
cooler shall not be electrically operated and must be rated and capable of exchanging engine
frictional heat rejected to the fuel at full load with the engine’s cooling system radiator airflow
including a 10% cooling capacity reserve to accommodate operational fouling.
5. Provide installed diesel fuel oil impervious flexible fuel lines on the engine fuel supply and
return connections. Flexible fuel line connections shall be N.P.T. Provide and install properly
Addendum No. 3 263200 - 13
routed schedule 40 carbon steel fuel extension piping, as required, for final connections to the
fuel supply and return piping between the engine flexible connections and the sub base fuel tank
engine supply and return connections.
6. Fuel shall be piped with flexible connections from the filter/water separator system to the intake
of the engine fuel pump and then from the engine’s fuel return to fuel oil sub base tank.
D. Diesel Fuel Oil Sub-base Tank
1. EG vendor shall supply one (1) UL2085 Listed above ground steel double wall steel secondary
containment construction generator diesel fuel oil storage sub base tank for stationary
installation. The sub base tank shall be designed and constructed by a manufacturer officially
approved by the Dept. of Environmental Protection Agency (DEP). The sub base tank shall be
designed, manufactured, and installed so as to meet all of the applicable guidelines and
requirements of the International Building Code, Dept. of Environmental Protection Agency
(DEP), NFPA 30, NFPA 30A, NFPA 37, and NFPA 110 when used with the specified EG
system at full standby generator set rating as installed on the Project site. The sub base tank shall
be clearly labeled with a permanent label indicating the type of product, the volume capacity, the
top loading capacity, the manufacturer, and UL Listing.
2. The generator set, engine exhaust system, and generator weather protective enclosure are to be
installed and appropriately secured on top of the sub base tank by the enclosure manufacturer.
The Installing Contractor shall install the complete sub base tank and generator set / enclosure
assembly on the site in accordance with all referenced and applicable Standards, Codes,
Regulations, Ordinances, and as required by the local Authorities Having Jurisdiction.
3. Diesel fuel oil generator set sub base fuel oil tank construction.
a. Furnish one (1) generator set double wall sub base diesel fuel oil tank, designed,
constructed and listed as UL2085 Special Purpose, Secondarily Contained & Protected
Generator Set Base Tank. The sub base tank shall be manufacturer designed and tested for
projectile, ballistic and vehicle impact resistance, and be two (2) hour fire rated. The sub
base tank shall be designed and constructed to support the total weight of the generator set,
enclosure, all accessory equipment items installed on the sub base tank, and tank full fuel
weight. It shall be double wall construction for a minimum of 110% secondary fuel
containment. The primary fuel tank shall be sized and constructed so as to be a minimum of
2300 gallon capacity rated and labeled.
b. Both the primary inner and the secondary outer containment tanks shall be fabricated from a
minimum of 3/16 inch thick steel. The tank top shall be a minimum of 1/4 inch thick steel.
Each tank shall be built to UL142 standards and pressure tested by the manufacturer to a
minimum of 3-5 PSI as outlined in UL142. The tank shall be internally vaulted with a
minimum of six (6) inches of light weight concrete. The tank shall incorporate suitable
internal stiffeners to create a smooth tank top surface and to limit the accumulation of
water. The outer tank shall be abrasive blast cleaned per SSPC-SP10 (White Metal Blast)
and shall be properly surface prepared and coated with one coat of a high build polyester
glass flake to a minimum of 12-15 mils (DFT) thickness, and a top finish coat of UV
resistant aliphatic polyurethane enamel with a minimum of 2-3 mils (DFT).The tank shall
be constructed with no sharp edges to insure uniform coating coverage on all surfaces. No
external sub base tank generator set support beams shall be permitted on top of the tank.
Provide drillings for ground device / cable attachments.
Addendum No. 3 263200 - 14
c. The manufactured sub base tank shall be designed and constructed to support the total wet
weight of the generator set, enclosure, all installed accessory equipment, and tank full fuel
weight, and be able to withstand a minimum of 180 MPH constant wind velocity with the
sub base tank empty of fuel. Provide mounting means and hardware on the top of the sub
base tank top to install all generator set spring vibration isolators and generator set
mounting base frame to be furnished by the EG vendor. The tank shall incorporate
foundation tie down construction and six (6) lifting points, approved by UL with a 4 to 1
safety factor consisting of minimum of 0.50 inch thick (nominal) steel plates welded into
the tank base perimeter, each with eyelets designed and installed so as to allow single point
spreader bar lifting of the empty sub base tank with the generator set, accessory equipment,
and enclosure installed on top of the sub base tank.
d. The tank shall be provided with appropriate quantity of earthquake/hurricane resistant tie
down restraint points, minimum of 1 / 4 inch thick, 2 inch high cross support channels
installed on the tank assembly by the tank manufacturer across the width of the bottom of
the sub base tank in adequate locations as required to support the fuel filled sub base tank,
generator set, and enclosure as an assembled package, to control moisture accumulation
under the sub base tank, and to allow visual fuel leakage inspection underneath the sub base
tank. Each cross support channel shall include foundation mounting holes on both ends to
allow for adequate securing of the sub base tank on the site’s mounting foundation. Provide
a drawing indicating dimensional locations for each of the foundation mounting securing
points for the sub base tank. The sub base tank manufacturer shall also provide 3/8” thick
by 6” wide full-length neoprene pads for isolation of all tank channel supports to be
installed between the bottom of the tank support channels and the site foundation during site
installation.
e. The sub base manufacturer shall provide in the Shop Drawing Submittals detailed sub base
tank windload and floatation uplift calculations and recommendations for foundation
anchoring means. The calculations will be based on the specific generator set and enclosure
to be installed on top of the fuel empty sub base tank. A copy of these calculations and
recommendations shall also be included in the sub base tank manufacturer’s operation and
maintenance manuals furnished to the ENGINEER and to the OWNER. The Installing
CONTRACTOR shall be responsible to install the sub base tank on the site. The Installing
CONTRACTOR shall furnish all required sub base tank foundation mounting hardware and
installation services to properly install and secure the sub base tank on the site’s concrete
foundation. Sub base tank foundation securement means shall be verified to withstand 180
MPH wind loading on the generator set /sub base / enclosure assembly with the sub base
tank empty of fuel.
f. The tank shall be provided with the following minimum N.P.T. connections and
appurtenances: generator supply and return ports, fuel fill port, required fuel level sensor
ports, fuel level gage, required primary and secondary tank normal and emergency vents,
specified fuel level and leakage sensors, primary and secondary tank drain ports, and spare
primary tank connection fittings with threaded plugs. All tank fittings, with the exception of
drain fittings are to be N.P.T. threaded # 304L schedule 40 stainless steel, and shall exit the
top of the tank only.
g. The sub base tank shall include inner and outer tank standard and emergency updraft
venting, pipe risers, and UL142 vent caps and shall be installed in compliance with all
applicable NFPA, and applicable local code and permitting approval requirements. The
Addendum No. 3 263200 - 15
emergency vent capacity shall be calculated by the tank manufacturer in accordance with
NFPA 30 & UL142. Primary and secondary emergency vent caps shall be Morrison Bros.
#244 or approved equal. The sub base tank vent locations shall be located so as to allow
direct vertical pipe routing, with the generator set and enclosure installed on the tank. The
standard fuel tank vent and any other tank vents as applicable must be extended from the
top of the sub base tank vertically through the roof of the enclosure and terminated with the
vent cap. Furnish a removable double poppet foot valve in the bottom of the engine supply
drop tube piping. The enclosure manufacturer shall furnish and install removable aluminum
or stainless steel construction rain collars and shields in the enclosure roof penetration
points for all tank vent extension piping exiting the enclosure roof.
h. The tank shall be furnished with low fuel level, high fuel level, critical low fuel level, and
fuel leak sensors/ switches and alarm level activation points. The switches and any required
auxiliary relay contacts shall be wired to the enclosure installed fuel level monitoring alarm
panel specified herein and to the generator control panel for local alarm and to the enclosure
installed DC junction box for remote annunciation use. Provide one (1) spare 3 in. N.P.T.
opening / fitting with galvanized threaded steel plug installed in the top of the tank for
additional future sub base primary tank fuel level monitoring purposes.
i. Provide and install a DEP approved, fuel fill / overspill box with a minimum of seven (7)
gallon capacity positive fuel containment box installed on top of the sub base tank. The box
shall be stainless steel construction with a stainless steel hinged pad lockable top cover with
a UL approved vent cap installed on the top of the box. Sub base tank fuel fill opening shall
be a minimum of four (4) inch N.P.T. and provided with a DEP approved anti-siphon valve
and mechanical fuel fill limiter. The fuel containment box shall have a tight fill connection
inside to shut off the flow of filling fuel at 95 % of tank capacity. Provide a UL Listed
spring loaded drain pull to allow fuel contained within the fill box to be returned directly
into the primary fuel tank.
j. Provide and install a mechanical water tight tank fuel level gage to monitor fuel tank level
from empty to full and locate on top of the tank inside of the sub base tank fuel fill box.
Provide and install for the sub base tank an additional tank manual withdrawal type fuel
level dipstick graduated and permanently marked in 100 gallon increments. Dipstick port
location shall be inside of the generator enclosure.
k. All fuel system piping shall be schedule 40 black iron, internally cleaned and pressure
tested, be sandblasted, primer coated, and finish painted with diesel fuel impervious black
colored enamel. Provide a sub base tank fuel inlet installed DEP approved and UL Listed
three (3) inch N.P.T. overfill prevention valve to automatically shut off the flow of filling
fuel at 95 % of tank capacity.
l. The enclosure manufacturer shall wire the sub base tank’s critical low fuel level generator
shutdown switch to the generator shutdown / annunciation controls. Activation of the
critical low fuel level switch shall cause the generator set to immediately shutdown while
simultaneously shunt trip open the generator mounted main circuit breaker.
m. Provide a UL approved NEMA 4X hinged door lockable fuel level monitoring alarm panel
with individual visual and common audible alarm indications for sub base tank low fuel
level, high fuel level, and fuel tank leakage conditions, and with relay dry contacts
(minimum of 3 Amp at 30 VDC) for each alarm wired to terminal points in the generator
mounted DC control interconnection junction box for remote annunciation use. The panel
Addendum No. 3 263200 - 16
shall include alarm press to test and alarm horn silence pushbuttons and shall be located and
securely installed on the exterior of the generator outdoor enclosure within near and ready
eyesight view of the sub base tank’s fuel fill box. AC service power for the alarm panel
shall b e provided by the Installing CONTRACTOR All level and alarm signal wiring
between the installed monitor panel, the generator set, and the sub base tank shall be in
EMT conduit with compression fittings and shall be provided by the sub base tank and
enclosure manufacturer. All wiring connections to the generator set shall be flexible. The
fuel alarm panel shall be current model no. LC-1003 as manufactured by Pneumercator, Inc.
n. The fuel monitoring panel is to be wired to the sub base tank installed fuel level probes and
sensors, generator control panel, and enclosure exterior wiring interface junction box by the
enclosure manufacturer. All fuel system electrical installations, including the fuel system
monitoring panel and controls shall be wired within the generator enclosure by the
enclosure manufacturer in accordance with all NEC requirements. Complete fuel system
control and power wiring diagrams shall be proved in the Shop Drawing submittals. All
level and alarm signal wiring between the enclosure installed fuel system panel, the
generator set, and the sub base tank shall be in EMT conduit with compression fittings and
shall be provided by the enclosure manufacturer. All wiring connections to the generator set
shall be flexible.
o. The sub base tank shall be furnished with a suitably sized rectangular shaped opening
conduit stub up area within the sub base tank’s primary and secondary tanks. The opening
shall be located and properly sized to be directly under the enclosure / sub base tank
installed generator mounted main AC power connection junction box for proper bottom
entry pass through of the AC power and control stub up conduits and conductors. The
Installing CONTRACTOR shall be responsible to coordinate foundation stub up locations,
all interface AC power, monitoring and control signal conduits and wiring connections for
the entire EG system. After installation of the generator AC power cables and conduits are
completed, provide a removable steel plate cover assembly for the stub up opening inside of
the enclosure to positively prevent accidental personnel entry into the opening. The plate
cover shall be secured so as to prevent excessive physical movement of the cover during
generator set operation.
p. The sub base tank’s critical low fuel level sensor / switch shall be connected to the
generator automatic shutdown circuitry. Activation of the critical low fuel level switch shall
cause the generator set to immediately shutdown while simultaneously shunt trip open the
generator mounted main power circuit breaker and annunciate a visual “Critical Low Fuel
level” alarm on the generator control panel..
q. Provide and install all required generator set /sub base tank fuel system interconnection
piping and make all connections between the sub base tank and the generator set fuel supply
and return, including all required vent piping. All fuel piping shall be properly cleaned of
debris and corrosion, and pressure tested to confirm no leakage prior to any fueling of the
tank. All fuel system interface wiring for remote monitoring and annunciation shall be
furnished and installed by the Installing CONTRACTOR.
r. The Installing CONTRACTOR shall be responsible to furnish diesel fuel to fill the
generator sub base tank to 75% full with new diesel fuel oil as recommended by the EG
Vendor for use with the furnished generator set prior to generator system startup and
testing. Upon satisfactory completion of all of the EG system testing and ENGINEER
Addendum No. 3 263200 - 17
final acceptance of the complete EG system, the Installing CONTRACTOR shall be
responsible to provide additional fuel to refill the sub base tank to 100% full fuel level with
new diesel fuel oil as recommended by the EG Manufacturer.
s. The sub base tank shall be manufactured only after the ENGINEER has reviewed and
approved the EG vendor’s equipment Shop Drawing Submittals.
t. Provide sub base tank manufacturer’s thirty (30) year warranty against defects in material
and workmanship, including structural failures for the furnished sub base tank
u. The generator sub base tank shall be furnished by the EG vendor as designed and
manufactured by Advanced Manufacturing & Power Systems, Inc., Deland, Florida or
approved equal. Detailed documentation and certifications by the enclosure manufacturer
and EG vendor indicating complete compliance with these Specifications and the Drawings
are to be included in the EG vendor’s submitted Shop Drawing Submittals.
E. Governor
1. The engine governor shall be an electronic isochronous speed controller. Speed droop shall be
externally adjustable from 0 to 10% from no load to full rated load and shall automatically adjust
generator frequency from within a maximum of 0.25% of rated frequency under steady state
operating no load and loaded conditions. Speed shall be sensed by a magnetic pickup off the
engine flywheel ring gear. A provision for remote speed adjustment shall be included. The
governor shall incorporate provisions for limiting fuel during start-up, and included capability for
r compensation adjustment. The use an of electronic engine control system to perform the
governor functions of controlling fuel and engine speed is acceptable.
F. Cooling System
1. The engine jacket water-cooling system shall be a pressurized closed circuit design with
provision for manual filling, thermal expansion, and coolant de-aeration. The radiator blower fan
and engine cooling water centrifugal type transfer pump shall be driven by the engine and
circulate the engine jacket water through the entire engine cooling water system including the
radiator. Any auxiliary coolant transfer pumps required for separate circuit after cooling of the
engine through the radiator must also be engine driven. Air to air aftercooled engines shall be
sufficiently cooled as required by the furnished radiator system. The radiator shall be of
sufficient capacity to allow continuous generator set full rated operation within a 110 degrees F
outside ambient air temperature. The radiator shall be furnished and installed on the generator set
by the generator set manufacturer prior to shipment.
2. The radiator shall be furnished with a duct flange for use with a radiator air discharge duct or
shroud as required to be installed by the enclosure manufacturer between the radiator and the
enclosure’s radiator air discharge opening. The radiator shall be furnished with a painted
perforated metal grill to protect the radiator core.
3. Heat rejected to the engine jacket water and after cooler shall be radiator driven air discharged to
the atmosphere through a close-coupled radiator. The radiator shall properly cool the engine
jacket water and after cooler water while the engine is operating at full load capacity within the
generator room at maximum specified site temperature.
Addendum No. 3 263200 - 18
4. The radiator fan, fan drive, and fan belts shall be totally enclosed and covered with 14 gauge
punched steel mesh guarding for personnel protection and shall be OSHA approved.
5. The radiator-cooling fan shall be a blower type and be mechanically direct driven from the
engine. Air shall be drawn from the engine sides and top and exhausted through the radiator core
to the radiator air discharge plenum.
6. Coolant lines shall be high temperature, strength reinforced and with flexible connections.
Provide a removable radiator pressure cap and radiator overflow line installed on the radiator.
7. Provide a flexibly connected coolant water drain line with stainless steel construction manual
shutoff valve terminated on the outside of the generator set outdoor weather protective enclosure
with a stainless steel N.P.T fitting and a threaded stainless steel cap. Provide a permanently
installed “Radiator Drain” nameplate secured to the enclosure wall next to the drain fitting.
8. An electronic coolant level sensor / alarm switch shall be furnished and installed in the radiator
by the engine manufacturer for coolant level monitoring of coolant level within the radiator and
interfaced with the generator set control circuitry to automatically shutdown the generator set in
the event of a critical low coolant level condition..
9. UL recognized engine coolant electric Jacket water heater(s) shall be provided and installed on
the engine by the EG manufacturer. The heater(s) shall be complete with automatic thermostatic
control suitable sized so as to maintain uniform engine coolant temperature of adjustable (90 -
175°F) while the engine is idle. The heater(s) shall be 120 volt AC single-phase controlled for
automatic on/off operation by the heater thermostats and shall be connected to a heater contactor,
installed and wired by generator set manufacturer. The heater(s) shall be automatically de-
energized by the generator set controls anytime that the engine runs. The engine manufacturer
shall install the heater with manual isolation shutoff valves at each heater hose connection at the
engine in order to facilitate heater/heater hose maintenance without having to drain the engine
coolant water.
10. Provide the engine / radiator closed loop type cooling system with a water/ethylene glycol based
coolant mixture as per the engine manufacturer's recommendations.
G. Combustion Air System
1. The engine intake air system shall include engine mounted, dry element, intake air filters with an
installed air filter restriction indicator for each filter.
H. Exhaust System
1. The engine exhaust system shall be installed to discharge combustion gases quickly and silently
with minimum restriction. The exhaust system including the generator exhaust silencer shall be
designed for minimum restriction, and in no case shall the total exhaust system backpressure
restriction imposed on the engine at full operating load exceed the engine manufacturer’s
maximum allowable exhaust backpressure limits.
2. All exhaust piping shall be Schedule 40 steel piping. The exhaust silencer and the exhaust piping
shall be covered with appropriate high temperature insulation and shielding inside of the
generator enclosure.
Addendum No. 3 263200 - 19
3. The generator exhaust silencer is to be installed inside of the generator outdoor weather
protective enclosure. The generator exhaust silencer exhaust outlet piping shall be terminated
vertically outside of the enclosure roof with an installed aluminum or stainless steel rain skirt and
terminated with a counter weighted aluminum construction exhaust rain cap. The exhaust
silencer and associated piping shall be installation supported and braced to prevent weight or
thermal growth from being transferred to the engine. Flexible expansion fittings shall be provided
to accommodate thermal growth. Support dampers and springs shall be included where
necessary to isolate damaging vibrations. All exhaust system piping, insulation materials, and the
complete installation of the entire exhaust system shall be provided by the enclosure
manufacturer / EG vendor.
4. The silencer shall be furnished with inlet and outlet weld on type ANSI companion flanges,
gaskets and bolts / nuts, and an appropriately sized stainless steel bellows type engine expansion
flex connector for connection to the engine. The silencer shall be furnished with a NPT drain
fitting. Suitable rated high temperature resistant gaskets shall be utilized for all exhaust system
flanged connections.
5. The silencer body shall be furnished with a N.P.T. drain fitting and shall be piped to the outside
of the generator outdoor enclosure with a stainless steel construction manual shutoff isolation
valve installed inside of the generator enclosure. The muffler water drain line shall be flexibly
terminated on the outside of the generator enclosure with a stainless steel N.P.T fitting and
stainless steel threaded cap. Provide a “Muffler Drain” nameplate permanently installed on the
enclosure exterior next to the silencer drain fitting.
I. Starting System
1. The engine shall be equipped with a 24 VDC electric starting motor system which shall include
one (1) solenoid shift positive engagement starting motors, starter relay, battery charging
alternator, starting / control batteries, an automatic battery charger and automatic reset circuit
breaker to protect against butt engagement. The starting motor shall be capable of providing
engine cranking for 90 consecutive second without damage to any component of the engine
starting system or engine. The system shall be capable of crank starting a properly equipped
engine so as to allow crank/rest termination to occur as necessary for the generator set to
consistently achieve proper rated operating speed within 10 seconds minimum at maximum site
ambient temperatures. Automatic adjustable crank cycle and termination control logic and
circuitry shall be furnished on the engine.
2. Furnish an engine manufacturer installed 24 VDC, 45 ampere, battery charging alternator with a
transistorized voltage regulator. The engine mounted battery-charging alternator and belt
assembly is to be furnished with installed OSHA approved metal guards.
3. Batteries for starting and control shall be a heavy duty, low-maintenance, lead acid type, and
housed in a hard rubber or polypropylene case with provisions for venting. Starting batteries shall
be rated 24 volt DC, minimum of 140 AH, and sized as based on specific application
requirements of engine oil viscosity, minimum ambient starting temperature, control voltage,
overcharging and vibration. Battery capacity shall be sufficient for cranking the engine for a
minimum of 15 seconds per each specified cranking cycle to achieve engine-firing speed with
ambient temperature of 32 degrees F. The furnished batteries shall also have sufficient engine
starting cranking amperage capacity for a minimum of ninety (90) seconds of continuous
cranking with an ambient temperature range of 32 to 110 degrees F.
Addendum No. 3 263200 - 20
4. Batteries shall be located as close to the starting motor as practical, away from spark sources, in a
relatively cool location, and permit easy inspection and maintenance. Non metallic, polyethylene
type battery electrolyte impervious battery cases with matching covers allowing full flow air
ventilation shall be provided for the batteries and shall provide positive electrolyte containment.
Required insulated battery cables shall be provided and sized to satisfy engine generator set
starting and control circuit requirements.
5. An engine mounted key operated starting / control battery disconnect switch shall be furnished.
Provide an alarm light on the generator set control panel to activate when the battery disconnect
switch is in the “off battery” position.
6. A solid state, constant voltage automatic battery charger, UL1564 Listed, designed for use with
lead acid batteries shall be provided of the current limiting type, designed for float charging, with
an automatic and manual digital equalize charge timer adjustable from 1 to 144 hours with
selectable timing modes. It shall accept 120 volt AC, single-phase input power to provide 24 volt
DC, minimum of 10-Ampere output and shall provide 100 % battery recharge per NFPA 110,
Level 1 requirements. The Installing CONTRACTOR shall connect AC service to the charger
and the enclosure manufacturer shall wire the charger DC power output and alarms to the
generator set in EMT conduit with compression fittings. It shall be fused on the AC input and DC
output, and incorporates current limiting circuitry. A power switch shall be mounted on the face
of the charger and shielded from accidental switching. The charger shall include an AC power
monitor with light, a digital 1% accuracy DC ammeter to monitor the battery charging current, a
digital 1% accuracy DC voltmeter with selector switch. The charger shall be furnished with
alarms for input AC failure, charger failure/malfunction, low battery voltage, high battery
voltage, low DC amperage, critical low DC voltage, and combined summary alarm monitoring
with individual local alarm light indications and dry alarm contacts for each alarm wired to the
generator DC control interconnection junction box for remote annunciation use. The charger
shall be housed in a NEMA 1 enclosure suitable for wall mounting. The battery charger shall
comply with all of the requirements of NFPA 110, Level 1. The battery charger shall be model
no. A46 of current design and manufacture by LaMarche Manufacturing Company, Des Plaines,
Illinois, or approved equal. The charger’s alarms shall be wired to the generator set for generator
control panel alarm annunciation and to the DC junction box for remote annunciation use. The
charger shall be located and installed within the generator enclosure and located so as to allow
charger front panel viewing and charger door full open swing for maintenance / service access.
J. Generator
1. The generator set’s alternating current synchronous generator shall be minimally rated for
continuous standby service at 200KW, 250KVA, 0.80 power factor, 277/480 volt AC, 3-phase,
4-wire, wye-connected, 60 hertz. The generator set’s rating shall be based on a 105 degrees C
temperature rise when operated at the generator’s Standby power rating within a 40 degrees C
ambient. Generator shall be capable of supplying power to solid state switching devices and non-
linear loads such as variable frequency drives, and solid state soft starters and associated
harmonics.
2. As manufactured, furnished, and installed, the generator shall meet or exceed these
Specifications and the applicable sections of the following standards:
a. National Electrical Manufacturers Association (NEMA) - NEMA MG1, Motors and
Generators
Addendum No. 3 263200 - 21
b. Institute of Electrical and Electronic Engineers (IEEE) - IEEE 43, Recommended Practice
for Insulation Testing of Large AC Rotating Machinery
c. United States military Standards for Generators and Controls – (MIL-STD)
3. The generator shall be four (4) poles, twelve (12) lead re-connectable brushless, revolving field
design with rotating rectifier system sized for maximum motor starting, air cooled, with an open
drip proof enclosure, single or two bearing.
4. The generator housing shall be one piece and mounted directly to the engine flywheel housing.
Engine torque shall be transmitted through a torsional coupling to the generator rotor. The
torsional coupling shall be designed such the engine-generator set coupled package shall be free
from objectionable vibration in any mode of operation. Provide generator set manufacturer’s
torsional vibration testing analysis for the engine generator set model to confirm that it has been
designed, constructed and assembled so as to be free from objectionable or harmful vibrations in
any operational mode. The manufacturer’s detailed torsional report for the factory testing of a
similar production unit shall demonstrate that the generator set model to be furnished shall
operate free from excessive torsional vibrations and is to be submitted to the ENGINEER for
review prior to generator set manufacture.
5. The generator set shall be furnished with a permanent magnet and shall be capable of
maintaining field forcing of the generator during generator set operation to sustain 300% of rated
generator current for 10 seconds when a 3 phase symmetrical short circuit is applied at the
generator terminals.
6. Stator and rotor insulation system shall all be NEMA Class H as defined by NEMA MG1-1.65.
The alternator insulation must be certified under UL 1446 Standard. The generator shall be
vacuum impregnated with epoxy resin, which after complete curing shall have additional
treatment of epoxy for resistance to an environment of moisture and salt air.
7. All generator mounted potential transformers and current transformers shall be U.L. labeled and
recognized.
8. The generator’s permanent magnet generator (PMG) excitation system shall provide power to the
automatic voltage regulator. The exciter shall be high frequency, direct connected, rotating
brushless type, three-phase, full wave rectified, completely compatible with the furnished
automatic voltage regulator. The rotating part of the exciter, including the rectifier assembly,
shall rotate together with the generator rotor as a complete assembly on one shaft. Surge
suppressors shall be included to protect the rotating diodes from abnormal transient voltage
conditions.
9. The generator shall comply with the requirements of NEMA MG 1-22, IEC 34-1, ISO-8528-3.
Radio frequency noise suppression shall meet or exceed the requirements of MIL-STD-461.
Total Harmonic Distortion (THD) shall be less than 5%.
10. The generator shall be designed, prototype tested and manufactured for 150% of rated generator
set speed without incurring damage.
11. The generator shall be equipped by the generator manufacturer with internally installed, UL
Listed, 120 volt AC single-phase alternator anti-condensation space heater(s) appropriately sized
to minimize condensation while the generator is not operating. The heater shall be capable of
Addendum No. 3 263200 - 22
being readily removed from the assembled generator and shall be field replaceable. The heater
shall be energized when the generator is off and automatically cut off when the generator is
running via generator controls. The Installing CONTRACTOR shall connect electrical AC
service power to the generator space heaters.
12. Provide an installed appropriately selected ground fault sensing system utilizing current
transformer and UL Listed ground fault alarm monitoring relay installed and wired inside of the
generator for ground fault alarm indication only on the generator mounted control panel. Provide
a ground fault relay dry alarm contact wired to terminal points inside of the generator DC control
interconnection junction box for remote annunciation use.
13. Provide, install, and appropriately wire three-phase fused UL Listed lightning arrestor (GE p/n
9L15ECC001) and UL Listed surge capacitor (GE p/n 9L18BBB301) inside of the generator
housing.
K. Generator Voltage Regulator
1. The generator voltage regulator shall be furnished by the engine generator manufacturer and shall
be automatic to maintain generator output voltage by controlling the current applied to the exciter
field of the generator during generator set operation at all levels of the generator set’s operating
range.
2. The regulator shall be a digital design with microprocessor control to allow for programmability
based on the type of load connected.
3. The regulator shall be mounted within the generator assembly, and shall be manually adjustable
from the generator mounted control panel. The supplied voltage regulator shall be tested with the
furnished generator set at the manufacturer’s factory during the factory generator set testing as
specified herein prior to shipment.
4. The automatic voltage regulator shall be programmable, microprocessor based, and shall
incorporate the following characteristics/features:
a. True RMS Line to line, three phase sensing of the generator output.
b. Generator output voltage maintained within 0.25% at steady state conditions for any load
variation between no load and full load.
c. Generator output voltage drift no more than 0.25% of rated value within a 40° change over
ambient temperature range of -40°C to 70°C.
d. Telephone Influence Factor (TIF) of less than 50.
e. Electronic Interference/Radio Frequency Interference (EMI/RFI) suppressed to commercial
standards.
f. Maintain voltage control with 20% total harmonic distortion.
L. Generator Circuit Breaker
Addendum No. 3 263200 - 23
1. Provide one (1) generator mounted UL Listed main line, solid-state trip, three-pole generator
output circuit breaker for the purpose of providing an AC electrical load circuit interrupting and
protection device on the generator. The circuit breaker shall be an LSI unit of the amperage size
and rating as shown on the Contract Drawings. The circuit breaker’s electronic trip current
sensors shall monitor each phase It shall have adjustable long time and long time delay during
overload conditions, instantaneous magnetic tripping for short circuit protection, adjustable short
time and short time delay features. Generator exciter field circuit breakers do not meet this
requirement and are not acceptable in lieu of the generator mounted circuit breaker.
2. A generator DC battery control voltage operated circuit breaker shunt trip coil shall be furnished
to automatically trip open the circuit breaker concurrently with any generator set fault,
emergency shutdown condition, and generator set diagnostic detection of an event that could
cause catastrophic failure of the generator.
3. The circuit breaker shall be furnished with a minimum of one (1) set of circuit breaker installed
auxiliary circuit breaker open / close status dry contacts for remote signal annunciation purposes.
Auxiliary contacts shall be wired to the generator DC junction interface box.
4. Provide a generator neutral conductor bus bar arrangement inside of an adequately sized
generator mounted circuit breaker enclosure connected to the generator neutral leads. The circuit
breaker and generator neutral bar assembly shall be furnished with mechanical lugs suitable for
proper connections with the quantities and sizes of the generator AC power conductors / conduits
as shown on the Contract Drawings. AC power cable and conduit entry into the generator for
connection to the circuit breaker shall be from the bottom through the opening of the sub-base
fuel tank.
M. Engine Generator Set Control
1. The generator set shall be provided with an open protocol, digital microprocessor-based,
environmentally sealed control system which is designed to allow generator set automatic
starting and stopping, monitoring and control functions for the generator set. The control system
shall also be designed and provided to allow local and remote start and stop control and
monitoring of the generator set. The generator control panel shall be vibration isolated and
mounted on the generator set. The control panel shall UL508A Listed and shall be NEMA 12,
dust proof enclosure with all control panel switches, lamps and meters gasketed to be oil-tight
and dust-tight and furnished with a lockable hinged door cover. The control panel and generator
set controls shall operate from the EG vendor furnished 24 VDC starting / control battery for the
generator set which shall be integrated with the required generator start / stop control circuitry
from the remote transfer control equipment.
2. The generator mounted control panel shall include, as a minimum, the following features and
functions.
a. Operational switches or keys to provide RUN/STOP/AUTO/OFF RESET operations for the
generator set. In the RUN position the generator set shall automatically start, and accelerate
to rated speed and voltage and maintain operation. In the STOP position the generator set
shall stop after a programmable cool down period has elapsed. In the AUTO position the
generator set shall be ready to accept a signal from the remote generator start / stop control
transfer equipment. When the remote signal is received, the generator set shall start and
accelerate to rated speed and voltage and maintain operation until the signal is removed
whereby, the generator set shall shut down after a programmable cool down period has
Addendum No. 3 263200 - 24
elapsed. In the OFF RESET position, the generator set is immediately shutdown and
generator control panel fault lights/controls are reset.
b. Provide minimum adjustable cycle cranking of 15 seconds on and 15 seconds off for three
cycle cranking attempts (total of 90 seconds). If the engine fails to start at the completion of
the three cranking attempts, the generator set shall shutdown, lockout the engine and
indicate overcrank on alarm status panel and provide a signal for remote annunciation use.
The generator controls shall also be selectable and adjustable to allow one continuous 90-
second engine crank attempt before generator shutdown and lockout occurs.
c. A red EMERGENCY STOP maintained push button switch to cause the generator set to
immediately shut down, and be locked out from automatic restarting. The generator set
controls shall also accept a contact closure signal from additional remote emergency
generator shutdown switches resulting in immediate shutdown of the generator set. A
common safety shutdown relay with dry contacts for remote annunciation use shall be
provided.
d. A reset switch to clear a fault and allow restarting the generator set after it has shut down
for any fault condition unless the fault condition continues to exist.
e. A lamp test switch to cause the entire control panel to be lighted with DC control power.
The panel lamps shall automatically be switched off within 15 minutes after the switch is
depressed, or after the switch is depressed a second time.
f. Panel illumination lights (24 VDC operated) with panel mounted on / off switch shall be
furnished for the control panel.
g. Unlimited event logging of generator alarms, events, and trips accessible from an LED or
liquid crystal display screen for event or alarm or repair diagnosis. Events, alarms or trips
shall be recorded by calendar date and time of occurrence, not on engine running time. The
event log shall be able to be downloaded to a laptop computer for printing and analysis.
3. The control panel shall include a true RMS sensing with 0.5% electrical characteristic
accuracy metering package with the following monitoring and display parameters:
4. Digital (LCD) indications for each of the following:
a. AC voltage – 3 phase (L-L, & L-N).
b. AC Amps (3 Phase & Total)
c. KW (total and per phase)
d. KVA (total)
e. PF (average total and per phase)
f. Frequency
g. DC voltage
h. Coolant temperature
Addendum No. 3 263200 - 25
i. Oil pressure
j. Engine operating RPM
k. Engine running hours
5. The generator control system shall automatically shut down and lock out the generator set from
starting upon each of the following conditions:
a. Overcrank
b. Overspeed
c. Low lubricating oil pressure
d. High engine coolant temperature
e. Low coolant level
f. Operation of a local or remote manual stop station wired to the generator set.
6. The generator mounted control panel shall include alarm and individual status indications for
each of the following:
a. Overspeed shutdown (red)
b. Low engine oil pressure shutdown (red)
c. Overcrank shutdown (red)
d. High coolant temperature shutdown (red)
e. High coolant temperature pre-alarm (yellow)
f. Low engine oil pressure pre-alarm (yellow)
g. Low coolant temperature pre-alarm (yellow)
h. Low coolant level shutdown (red)
i. Controls not in automatic (flashing red)
j. Battery charger malfunction (red)
k. High/Low battery voltage (red)
l. Ground fault (yellow)
m. Emergency Stop (red) (from generator control panel E-Stop switch and from remote
breakglass station activation).
n. Common fault shutdown (red) (10A, 120V dry contact for all monitored fault conditions).
Addendum No. 3 263200 - 26
o. Common fault pre-alarm (yellow) (10A, 120V dry contact for all monitored fault
conditions). Common pre-fault alarm is the combination of all the pre-alarm stated above.
N. The generator mounted control panel shall incorporate true RMS sensing of electrical parameters and
immediately trip open the generator breaker and simultaneously stop generator set operation for
occurrence of any of the following conditions (provide adjustable level settings and time delays for
each):
a. Undervoltage.
b. Overvoltage.
c. Phase Over current.
d. Phase loss.
e. Overfrequency.
f. Underfrequency.
g. Overload KW.
h. Fault Conditions.
O. The generator control panel shall be provided with dry contact (10 amp at 120VAC) outputs wired to
the generator mounted low voltage/DC junction box for the following signal conditions:
1. Generator RUNNING status.
2. Generator PRE-FAIL warning alarm.
3. Generator FAIL shutdown alarm.
4. Fuel System TROUBLE alarm.
5. Generator circuit breaker OPEN status alarm.
6. Battery system TROUBLE alarm
P. Electrical interconnection of all wiring between the EG system equipment, the transfer switch
equipment, plant PLC system and other required remote annunciation requirements shall be furnished
by the Installing CONTRACTOR. The EG vendor shall provide project specific electrical wiring
schematics with numbered terminal point wiring interface connections clearly indicated for
ENGINEER review and for the Installing CONTRACTOR’S wiring information and use.
2.03 ENGINE-GENERATOR BASE
A. Engine generator base requirements
1. The engine and generator shall be assembled to a common base to provide suitable mounting on
any solid level surface. The base shall be constructed of heavy-duty structural steel, designed,
Addendum No. 3 263200 - 27
and built to resist deflection and maintain alignment during skidding, lifting and operation and
minimize resonant linear vibration during any range of normal generator set operation.
2. Both sides of the generator set mounting base assembly shall be bolt and nut secured to the top of
the furnished generator set sub base tank prior to delivery. The EG vendor shall confirm proper
securement of the generator set to the sub base tank after installation on the site and prior to
generator equipment startup. The Installing CONTRACTOR shall be responsible to provide and
install all hardware required to properly secure the sub base tank to the site foundation.
2.04 WEATHER PROTECTED ENCLOSURE (NON WALK-IN TYPE)
A. The EG Vendor shall furnish one (1) generator outdoor weather protective enclosure installed on
top of the generator fuel oil sub base tank as specified herein and as shown on the Drawings. The
enclosure shall be aluminum construction and shall completely enclose the generator set and all
generator system auxiliary equipment. The enclosure is to be installed and secured on top of the
diesel fuel oil sub base tank. The enclosure shall be sized large enough so as to allow personnel
adequate reach-in access to the equipment installed within the enclosure for operation and normal
maintenance purposes and shall provide all NEC and OSHA required clearances. The engine
exhaust silencer shall be mounted inside of the enclosure.
B. The enclosure as mounted on the sub base tank shall be designed, rated, and built to reduce
generator set mechanical and exhaust transmitted noise.
C. The enclosure, engine-generator set, and sub base tank assembly shall be complete in every detail
and requiring no additional in field modifications. It will be the responsibility of the Installing
CONTRACTOR to properly install the enclosure/sub base tank package on the site foundation,
as coordinated with and supervised by the EG vendor, and as approved by the Engineer.
D. The entire enclosure, installed generator set and accessory equipment, and sub base fuel tank
assembly shall be in compliance with the International Building Code (IBC), the National
Electrical Code (NEC) and the National Fire Protection Association (NFPA) including physical
space clearances around electrical equipment. The enclosure and sub base fuel tank assembly
shall conform to the equipment design criteria as specified herein and as shown on the Drawings.
E. The enclosure design and construction shall bear the UL label “Commercial Building Classified
by Underwriter’s Laboratories in Accordance with the National Electric Code”. The label shall
also indicate compliance with UL2200 for enclosures. The enclosure shall be certified by a
Professional Engineer (P. E.) licensed in the US Virgin Islands, to be designed and constructed to
withstand a constant wind load resistance up to 180 MPH. Provide eight (8) originals and eight
(8) copies of P. E. stamped certified wind load calculations and report, and drawings indicating
compliance for the specific enclosure to be furnished for this Project to the Engineer prior to site
delivery. The enclosure’s design and construction compliance with the specified wind load rating
are to be included on the Manufacturer’s enclosure drawings, and included in the EG system
Shop drawing submittals and the EG system As Built drawings included in the generator
equipment parts, operation and maintenance manuals.
F. Enclosure construction shall include individual components generally consisting of a roof, two
(2) side walls, and two (2) end walls using prepainted white epoxy formed aluminum. Contractor
shall verify the color of the owner preference. Enclosure mounted intake and discharge air
acoustic hoods or plenums, with fiberglass (non asbestos) acoustical insulation and securement
linings, and all hardware shall be stainless steel.
Addendum No. 3 263200 - 28
G. The roof shall be constructed of 5052 marine grade mill finish 0.125 in. minimum thickness
formed aluminum panels using an interlocking seam design. The roof top skin shall be painted
the same color (white) as the enclosure. A weatherproof mastic / sealant shall be used along the
roof perimeter and any roof skin joints. The roof rail perimeter shall have internally installed two
(2) roof lifting rings per side (a total of 4 lifting points) of 10,000 pound lifting capacity each for
lifting of the complete enclosure. All external roof attaching hardware shall be stainless steel
screw type mechanical fastener utilizing neoprene watertight washers. The roof shall be
designed and built for 75 pounds per square foot, which shall be substantiated by the enclosure
Manufacturer on the enclosure drawings. The enclosure roof shall incorporate an internally
installed and removable aluminum or stainless steel construction rain collar and rain shield for
the generator exhaust silencer piping at the roof penetration point to prevent the entry of
rainwater into the enclosure and allow for expansion and vibration of the exhaust piping without
stress to the exhaust system. Installed removable aluminum or stainless steel construction rain
collars and shields shall also be furnished for all sub base tank UL approved screened vents /
caps that penetrate the enclosure roof.
H. The walls shall be manufactured utilizing formed 3105 grade 0.080 minimum thickness
prepainted aluminum modular panels utilizing an interlocking seam design. Thermal acoustic
insulation with fire retardant properties shall be installed on all of the interior sidewalls and roof
of the enclosure.
I. All external attaching hardware shall be stainless steel screw type mechanical fasteners. The
enclosure shall be fastened to the sub base tank by the enclosure manufacturer by means of an
aluminum base channel and stainless steel clips that are welded to the sub base tank and bolted to
the base channel with stainless steel bolts, washers, and nuts. The base channel shall include
enclosure water drainage construction.
J. Thermal acoustic insulation shall be fiberglass and shall not include any asbestos materials, with
fire retardant properties. The insulation shall be installed on all of the interior sidewalls and roof
of the enclosure. The insulation will be completely covered with mill finish 0.032 inch thick
perforated aluminum lining secured to the enclosure interior. Provide thickness of sound
attenuation material as required to meet the noise level requirements specified herein Provide
thickness of sound attenuation material as required to meet the noise level requirements specified
in Paragraph 2.7 NOISE LEVEL REQUIREMENTS.
K. The generator intake air shall enter the end of the enclosure through the bottom of an enclosure
installed ventilation air intake hood / plenum section with removable 1” by 1” galvanized wire
cloth attached at the intake air opening,. The ventilation intake air assembly shall be constructed
of the same materials as the enclosure. The ventilation intake and discharge assemblies as
installed on the enclosure shall also be 180 MPH wind resistance rated, same as the enclosure
and shall be included in the P.E. wind load analysis and certifications provided. The enclosure air
intake system shall be designed and constructed to minimize water penetration into the enclosure
during heavy rainfall and be constructed for automatic drainage of falling rain water into the
plenum to the outside of the enclosure.
L. The radiator discharge end wall section shall incorporate a properly sized opening for the
furnished generator set radiator discharge core / opening and shall include appropriately
furnished and installed shroud or baffle assemblies to prevent the recirculation of radiator
discharge air into the enclosure. The radiator air shall be vertically discharged from the enclosure
end wall through the top of an enclosure mounted discharge air acoustic plenum with sound
baffles and shall be of the same materials as the enclosure. Provide removable 1” by 1”
Addendum No. 3 263200 - 29
galvanized wire cloth attached to the discharge plenum opening. The air discharge plenum shall
be furnished with a deflector plate and a bottom drain extension line for prevention of falling
water entry into the enclosure and for rainwater removal from the plenum. The discharge plenum
shall incorporate a side installed access door for plenum cleanout maintenance access.
M. The combined air inlet and discharge system shall be designed to maintain a combined total static
pressure restriction of no more than 0.5 inches of water gauge through the enclosure with the
generator set operating at full rated load and duty. Maximum design enclosure air flow velocity
through the enclosure shall not exceed 1250 FPM. The enclosure manufacturer shall submit EG
system / enclosure ventilation airflow calculations for confirmation of these requirements.
N. The generator set exhaust silencer exhaust discharge shall be piped to the outside of the enclosure
through the enclosure roof for vertical discharge of engine exhaust gases. Provide an installed
aluminum construction counter balanced exhaust piping raincap at the exhaust piping termination
point and an aluminum or stainless steel construction counter balanced piping raincap for the
exhaust piping termination.
O. The enclosure shall incorporate two (2) personnel doors located on each side of the enclosure for
a total of four (4) enclosure personnel access doors. The rear doors shall allow personnel reach-in
access to the generator set and enclosure installed equipment. Provide adequate operational and
access space, and NEC and OSHA compliant clearances for all equipment. The doors shall be 36
inches wide. All doors shall be constructed of 3105 prepainted aluminum to match the enclosure
exterior color, and installed into 3/16 inch mill finish aluminum frames that are structurally
integrated into the enclosure wall using heavy duty continuous stainless steel hinges constructed
with stainless steel hinge pins of a diameter not less than 0.25 inch. Provide gasketing to prevent
entry of water into the enclosure through the closed doors. The door passage latches shall be
stainless steel and all doors shall be padlockable from the outside. Each passage latch shall each
incorporate an operator with interior release handle for ease of egress in the event of an
emergency and shall allow escape from within the enclosure while the door is externally locked.
Each door shall include “holdback” hardware and restraints to secure the door to the enclosure
side wall when the door is opened fully. Include door handle strike plates on the enclosure walls
adjacent to the door to provide impact protection from the door handle. Rain gutters that shall
channel rainwater away from the top of the enclosure door opening shall be provided for the top
of all doors. Generator shall be provided with aluminum stairs, handrails and platforms at all
personnel doors to provide per NEC and OSHA compliance.
P. All components of the enclosure shall be assembled utilizing 0.375 inch minimum stainless steel
bolts or screw fasteners, nuts, and lock washers. In addition, watertight neoprene flat washers
shall be used on all roof bolts.
Q. The enclosure manufacturer shall provide all required hangars, supports, mounting materials and
hardware for the generator exhaust silencer and exhaust piping installed inside of the enclosure.
Provide insulation blankets on the entire exhaust system physically located inside of the
enclosure with the exception of the engine flexible exhaust connection.
R. The generator set high sound attenuation exhaust muffler and associated piping system size and
type is to be furnished so as not to exceed the engine manufacturer’s published maximum
exhaust flow restriction values and to provide attenuation so as to not allow more than the
specified maximum enclosure sound and noise levels at any range of generator set operation.
Addendum No. 3 263200 - 30
S. The enclosure shall be manufactured to be finish coated with a long lasting epoxy coating finish
to prevent oxidation and maintain the paint finish.
T. The enclosure sidewalls shall incorporate externally located threaded stainless steel N.P.T.
fittings with stainless steel caps for connection with enclosure interior installed piping and
flexible hoses and shut-off valves at the generator set for connection to the engine’s lubricating
oil, coolant, and exhaust silencer drains. All drain connections to the generator set and muffler
shall be flexible. The engine’s crankcase fumes disposal hoses shall be routed to inside of the
radiator air discharge plenum by the enclosure manufacturer. Install permanently secured weather
resistant “Engine Oil Drain”, “Radiator Drain”, and “Muffler Drain”, nameplates on the outside
of the enclosure next to each respective drain fitting.
U. The enclosure manufacturer shall install the specified generator emergency shutdown breakglass
station on the outside of the enclosure and wire to the generator emergency shutdown controls.
The breakglass station shall be located on the exterior side of the enclosure, next to the enclosure
door closest to the generator end of the enclosure.
V. Provide one (1) commercially available DC powered light bulb installed within a protective
covered fixture and mounted on the interior roof of the enclosure above the generator’s control
panel, away from damaging heat, and secured against harmful vibrations. The light is to be
connected to a manually operated automatic timer switch, labeled “DC Light”, installed inside
the enclosure adjacent to a rear door of the enclosure. The DC light shall be appropriately fused
and wired to the generator set’s starting/control battery power in conduit by the enclosure
manufacturer. The light shall be large enough to provide adequate illumination for the generator
control panel in an emergency situation yet not such that overburdening drain shall be placed on
the generator set starting battery system. Provide two (2) spare DC light bulbs with generator set
spare parts provisions.
W. The enclosure manufacturer shall be responsible to electrically wire the following items in the
interior and on the exterior of the enclosure as indicted herein. All enclosure electrical equipment
shall be installed and electrically wired and interconnected between the required equipment items
and a separate AC service power junction box by the enclosure manufacturer in accordance with
National Electric Code (NEC) and National Fire Protection Association (NFPA) requirements,
including proper clearance around all electrical equipment. All wiring will be in Rigid Metal or
liquid-tight conduit, utilizing compression fittings and all connections at the generator set shall be
flexible:
a. Generator anti-condensation space heater.
b. Engine jacket water heater.
c. Automatic battery charger.
d. Sub base tank fuel alarm panel.
X. The enclosure manufacturer shall provide the necessary electrical interconnection wiring and
conduit for all generator set equipment, DC power, controls, and alarms to the generator set,
battery charger, sub base tank fuel level switches and fuel alarm panel, and emergency shutdown
break glass station.
Addendum No. 3 263200 - 31
Y. All wiring within the enclosure shall be in RGS conduit, utilizing compression fittings and all
connections at the generator set shall be flexible. The enclosure manufacturer shall provide the
necessary DC electrical interconnection wiring and conduits for all generator set equipment,
including sub base tank, fuel level alarm panel, and the emergency shutdown break glass station,
located on electrical building, to be connected to the generator set. Generator AC power
conductors, AC service, control and remote annunciation wiring, and AC service power wiring
and conduits shall enter the enclosure from the bottom of the sub base tank through the sub base
tank cable stub up opening which shall be located directly under the installed generator mounted
circuit breaker. All of the generator system electrical wiring interface requirements, including AC
power, AC service, control and signal wiring for interface with the remote electrical transfer and
remote monitoring and annunciation equipment shall be furnished, installed, and terminated by
the Installing CONTRACTOR. Refer to the Drawings for additional wiring requirements.
Ground the engine generator frame and enclosure in accordance with the NEC.
Z. The Installing CONTRACTOR shall provide the required AC electrical service to the enclosure
manufacturer’s furnished NEMA 3R stainless steel terminal junction box installed on the interior
of the enclosure. The junction box shall be furnished with appropriate wiring terminal lugs for
the AC service wiring. The junction box shall be AC power wired in RGS conduit (with
compression fittings) to the generator set / sub base tank /enclosure package installed electrical
items within the enclosure by the enclosure manufacturer.
2.05 GENERATOR VIBRATION ISOLATORS
A. The engine and generator shall be assembled to a common base frame to provide suitable mounting
on any solid level surface. The base shall be constructed of heavy-duty structural steel, designed, and
built to resist and prevent deflection and maintain alignment during skidding, lifting and operation
and minimize resonant linear vibration during any range of normal generator set operation.
B. The generator set shall be provided with Manufacturer furnished resilient linear vibration isolators
installed between the generator set and the generator set mounting base providing over 95%
efficiency in reducing vibration transmissions. The isolators must be deflection restraint limiting, able
to withstand high loads in any plane, and comply with Seismic Zone 4 requirements. The isolators
shall be resistant to heat and age, and impervious to oil, coolant, diesel fuel, and cleaning compounds.
2.06 TORSIONAL VIBRATION
A. The complete engine generator set shall be so designed, constructed, and installed as to be free from
objectionable vibration in any mode. Freedom from torsional vibration shall be demonstrated by
torsion graph records taken during factory test of this or a similar unit. Copies of the generator set
manufacturer’s torsional compatibility analysis report for the model generator set furnished shall be
provided to the ENGINEER prior to site delivery of the generator set.
2.07 NOISE LEVEL REQUIREMENTS
A. The average overall sound pressure level on the A scale produced by the furnished equipment
operating as specified herein shall not exceed 70 decibels (dBA), reference 21 micro-newtons per
square meter, at a distance of 20 feet from the weatherproof enclosure, measured in accordance with
NEMA standards.
PART 3 EXECUTION
Addendum No. 3 263200 - 32
3.01 FACTORY TESTING AND INSPECTION
A. Engine-Generator Set
1. The engine-generator set manufacturer shall perform factory testing and quality control
inspections on the specific engine-generator set to be provided prior to being shipped from the
factory. The manufacturer’s certified report of these tests and inspections shall be submitted to
the ENGINEER prior to delivery of the unit to the site.
2. The engine, generator, and engine-generator set shall be subjected to the factory testing and
quality control inspections to insure proper and reliable operation. The Manufacturer’s certified
report of these tests and inspections shall be submitted to the ENGINEER prior to delivery of the
new generator equipment to the project site These tests and inspections shall include, but not
necessarily be limited to, the following:
a. Specific observances and corrective actions for any excessive engine blow-by, combustion
gas leaks, inlet air leaks, excessive vibration, and unusual noises.
b. Retest the generator set after any change affecting airflow through the engine, fuel injected
into the engine, engine combustion, or any reassembly which potentially affects mechanical
integrity.
c. Perform Factory testing of the generator set to be furnished to confirm baseline data with
recording of each of the following:
1) Voltage ( each of three phases and average)
2) Amperage ( each of three phases and average)
3) KW output
4) Power factor
5) Frequency
6) Rated engine speed
3. Prior to delivery the engine-generator set shall be Factory tested to show it is free of any
defects and will start automatically and carry full rated electrical load.
4. The Factory furnished generator set load testing shall be performed with reactive load
banks capable of definite and precise incremental loading of the generator set at 0.8 power
factor. The testing shall be performed at the generator set’s rated load and rated power
factor.
5. The load banks utilized for Factory testing of the generator set shall not be dependent on
the generator control instruments to read amperage and voltage on each phase. Rather, the
test instrumentation shall serve as a check of the generator set meters. Confirmation of
comparable readings of the generator control panel display parameters with the load bank
testing instrumentation shall be indicated on the furnished Factory test reports.
Addendum No. 3 263200 - 33
6. The engine generator Manufacturer’s certified Factory test report of the Factory testing and
inspection shall be submitted to the ENGINEER for approval prior to delivery of the unit
to the project site. Copies of the factory test reports shall also be included in the EG vendor
furnished generator set equipment Parts, Operation and Maintenance manuals.
7. Any generator equipment defects that become evident during the Factory testing shall be
corrected by the engine Manufacturer at his own expense prior to Factory shipment of the
generator set, no exceptions.
8. All consumables necessary for testing shall be furnished by the engine generator
Manufacturer. All generator equipment defects which become evident during the Factory
testing shall be corrected by the engine Manufacturer at his own expense prior to Factory
shipment.
9. Confirm through actual testing, and include verification in the testing report, that the
generator set physically shuts down in the event of simulation of each of the following
generator set shutdown conditions:
a. Overspeed
b. Overcrank
c. High water temperature
d. Low oil pressure
e. Low water level
f. Emergency shutoff switch
g. Overcurrent
10. The reactive load banks utilized for testing of the generator set at the factory shall not be
dependent on the generator control instruments to read amperage and voltage on each phase.
Rather, the test instrumentation shall serve as a check of the generator set meters. Confirmation
of comparable readings of the generator control panel display parameters with the load bank
testing instrumentation shall be indicated on the furnished factory test reports.
11. The EG manufacturers certified Factory test report of the factory testing and inspection shall be
submitted to the ENGINEER for approval prior to delivery of the unit to the project site. Copies
of the factory test report for the furnished generator set shall also be included in the EG vendor
furnished generator set equipment Parts, Operation and Maintenance manuals.
3.02 INSPECTION
A. Examine the area to receive the EG equipment to assure adequate clearance for installation.
B. Check to confirm that the generator concrete foundation pad is level, free of unacceptable
irregularities, and adequate for generator equipment installation.
C. Provide adequate information to ensure that the delivered generator equipment will be properly
offloaded, rigged, stored, installed, and protected by the Installing CONTRACTOR.
Addendum No. 3 263200 - 34
D. Start work only after all unsatisfactory conditions are corrected.
3.03 INSTALLATION
A. The generator set equipment shall be installed by the Installing CONTRACTOR as indicated on the
Drawings and per the manufacturer’s required and recommended procedures and guidelines. The
Installing CONTRACTOR shall properly protect and store the delivered generator equipment as
recommended by the generator set manufacturer and the EG vendor.
B. The EG vendor will be responsible for providing a qualified field service technician to oversee the
Installing CONTRACTOR’S installation of the EG system equipment, including setting, alignment,
assembly, piping, mechanical and electrical connections.
C. The EG vendor shall be responsible for providing the coordinating wiring diagrams indicating all
required the Project specific point to point electrical interconnection information between all of the
generator set equipment, including interconnection identification for interface to the automatic
transfer and annunciation equipment (furnished by others) for use by the Installing CONTRACTOR
during installation, wiring and checkout of the equipment.
D. After installation by others, the EG vendor shall provide the services of competent factory trained and
experienced service engineers to provide installation instructions to the Installing CONTRACTOR,
and to coordinate the installation completion of the equipment. They shall assist in placing the
equipment into operation and provide instruction, as required, to the persons who are delegated to
operate the equipment. EG vendor services shall include a minimum of six (6) visits by the factory
service engineers as follows:
1. Pre-installation coordination meeting to coordinate the installation and interconnection of the
automatic transfer equipment with the engine-generator equipment and all interface equipment.
2. Initial checkout of the installation of the equipment prior to start up and testing.
3. Post-installation start-up and testing to confirm proper operation prior to system turnover. This
trip may include multiple, not necessarily consecutive days and shall include all services required
to checkout, startup, load bank test and test the emergency power system at the facility.
4. Generator set equipment operation demonstration for the ENGINEER and OWNER’S
representatives and any other applicable approval Jurisdictions.
5. Initial Instruction period for initial EG system operating personnel.
6. Within four (4) months after generator system turnover, provide an additional one (1) day
instructional period for the OWNER’S engineering, operating, and maintenance personnel on
complete operation and maintenance of the EG system equipment as described herein and as
coordinated with the OWNER.
E. The EG vendor shall maintain a local competent and responsible factory authorized service and parts
organization that is available to the OWNER for service and parts procurement on a 24-hour / 365
day call basis.
3.04 FIELD QUALITY CONTROL
Addendum No. 3 263200 - 35
A. Technical representatives of the engine-generator set vendor shall check the complete installation of
the EG system equipment for installation acceptance and procedural and operational compliances.
The Installing CONTRACTOR shall note any installation deficiencies for prompt correction or
appropriate remedial action. Any EG equipment operational deficiencies shall be promptly corrected
by the EG vendor.
B. The EG vendor shall be available to assist the Installing CONTRACTOR during installation delivery
of the generator system equipment.
C. The EG vendor shall perform EG system start-up procedures, systems checks, provide necessary
adjustments, and provide site testing required after the installation is complete as coordinated with the
ENGINEER.
D. The proper initial service fill of engine lubricating oil and ethylene glycol based antifreeze coolant
solution, as recommended by the engine manufacturer, shall be provided and installed by the
generator set manufacturer or EG vendor.
3.05 SYSTEM START-UP AND OPERATIONAL TESTING
A. The EG vendor’s manufacturer trained field service technician shall be responsible for field start-up
and testing of the furnished generator system. The manufacturer shall furnish the ENGINEER with
written certification assuring that each item of equipment is complete, in good condition, free from
damage and properly installed, connected, adjusted and operating properly.
B. The installing CONTRACTOR shall provide the required and immediate assistance to the EG
manufacturer’s field service technician during start-up and testing. This assistance shall be generally
limited to tasks directly associated with the installation of the EG and interface wiring, not with the
internal components or inherent function of the EG equipment.
C. The Installing CONTRACTOR shall be responsible to fill the furnished generator sub base fuel tank
to 75% full capacity with new acceptable quality on road diesel fuel, engine manufacturer
recommended and approved for use with furnished generator set engine, immediately prior to
generator set equipment site startup initiation.
D. The EG vendor shall coordinate the operation of the engine-generator with the automatic transfer
control and remote annunciation control equipment suppliers so that automatic and manual operation
and annunciation of the complete emergency power system functions as described and as required by
these Specifications.
E. System start-up and operational testing procedures shall not be limited to those specified herein.
Others shall be performed as required to prove that the system functions as described and required by
these specifications.
F. EG operational testing shall be performed by the EG vendor in conjunction with technical
representatives of the transfer equipment, controls equipment, and the Installing CONTRACTOR in
the presence of the ENGINEER and OWNER. The same aforementioned personnel shall perform
system start-up but it is not necessary to perform start-up functions and procedures in the presence of
the ENGINEER unless specifically noted or required otherwise. Two (2) weeks advance written
notice shall be given to the ENGINEERS for all EG system start-up and testing procedures.
G. Operational Testing
Addendum No. 3 263200 - 36
1. The EG vendor shall provide temporary dry type, resistive load banks and appropriate power
conductor cables for the specified and required generator set site testing. The Installing
CONTRACTOR shall be responsible for connection and disconnection of the temporary load
bank cables to the equipment. Building load shall not be used to supplement load bank testing of
the generator equipment.
2. Load testing - Cold start block load the generator set at the full load 100% standby rating in one
step and operate sustained load for two (2) hours continuous. Remove the load from the generator
set and allow to cool down for five (5) minutes, then immediately reapply full standby 100%
standby rating block load onto the generator set in one step and operate sustained load for
additional two (2) hours continuous for a combined load testing period of four (4) hours. Record
each of the generator block loading transient high and low voltage and frequency levels and
actual recovery time to achieve to steady state operation and stabilized voltage and frequency
levels, Record the following readings in five (5) minute increments for the first fifteen (15
minutes at the initiation of each block load testing and at fifteen (15) minute increments
thereafter for the duration of the testing.
a. Voltage (3 phases)
b. Amperage (3 phases)
c. Frequency
d. Kilowatts
e. Power Factor
f. Fuel pressure, oil pressure and water temperature
g. Exhaust gas temperature at engine exhaust outlet
h. Ambient temperature
i. Battery charger amperage rate
j. Time at each recorded measurement
3. Check and demonstrate proper operation of the EG system controls, generator set alarms and
shutdowns, and safety devices in the presence of the ENGINEER.
4. Provide generator equipment testing including, but not limited to, generator set cycle cranking
and overcrank shutdown testing and other EG system safety alarm / shutdown testing.
5. Should these tests fail or indicate that the equipment does not meet the specified performance
requirements, the cost of all corrective measures shall be borne by the EG vendor if equipment
related and by the Installing CONTRACTOR if installation related. Once corrective measures are
implemented, the operational testing shall be repeated at the cost of the responsible party,
whether EG vendor or Installing CONTRACTOR.
6. Provide eight (8) copies of Certified test reports of the complete generator equipment field testing
as required herein after satisfactory completion of startup and testing of the generator set
Addendum No. 3 263200 - 37
equipment by the EG vendor. The certified generator equipment testing documentation and
reports to be furnished to the ENGINEER must be include all recorded EG system testing
information as required by NFPA 110, for Level 1 generator systems and as required by these
Specifications. Approved copies of the generator equipment test reports shall additionally be
included in the generator equipment operation and maintenance manuals as furnished by the EG
vendor.
7. The Installing CONTRACTOR shall refill the sub base fuel tank to 100% full level with engine
manufacturer recommended and approved on road diesel fuel oil after completion of all testing
and demonstration and the generator equipment has been accepted by the ENGINEER for
substantial completion.
H. Engine-Generator Pre-start Checks
1. Engine oil level
2. Engine coolant system and coolant water level
3. All generator equipment heater operations
4. Equipment fluid leakage
5. Vibration isolator adjustment
6. Battery connections, voltage and charge conditions
7. Engine to controls and all equipment electrical interface interconnections
8. Engine-generator intake /exhaust air obstructions
9. EG system AC power connections
10. Removal of all packing materials
11. EG system installation acceptance
3.06 SPARE PARTS
A. The EG vendor shall furnish the following spare parts at the time of completion of satisfactory
generator set startup to be maintained at the facility by the OWNER:
1. One (1) set of air filters and gaskets.
2. One (1) set of fuel filters and gaskets.
3. One (1) set of lubricating oil filters and gaskets.
4. Two (2) sets of Racor water separator fuel filter elements.
5. Two (2) fuses for each type and size used in the generator controls.
6. Two (2) fuses for each type and size used in the generator voltage regulator circuitry.
Addendum No. 3 263200 - 38
7. One (1) set of generator rotating positive and negative rectifier diodes, exciter resistor, voltage
regulator surge suppressor diodes/varistors, and one container of electrical heat sink compound.
8. One (1) engine coolant antifreeze test hydrometer.
9. One (1) battery post-cleaner brush.
10. One (1) battery electrolyte test hydrometer.
11. Two (2) spare DC light bulbs ( for outdoor enclosure)
3.07 INSTALLATION, OPERATION AND MAINTENANCE
A. Parts, Operation Instructions, and Maintenance Manuals
1. After completion of work, and satisfactory start-up and testing of the equipment at the project
site, deliver to the ENGINEER, five (5) copies of the generator equipment Parts, operation
instructions, maintenance manuals and drawings presenting full details for care and maintenance
of each item of equipment provided under this Contract.
2. Each manual shall contain the information and documentation for the generator system
equipment as indicated in other sections of these Specifications and must include operating and
maintenance information and parts lists for all equipment provided under this Contract. When
necessary, provide supplemental drawings to show system operation and servicing and
maintenance points. For all electrical components, provide complete, as field installed and wired
electrical wiring and connection diagrams. Manuals shall include instructions required to
accomplish specified operation and functions. Data shall be neat, clean, legible copies.
Drawings larger than standard size notebook paper shall be accordion folded. Non-applicable
information shall not be included or must be sufficiently crossed out.
3. In general the manual shall include, but not necessarily be limited to, the following:
a. Operating Instructions - with description and illustration of the engine-generator set, engine
and generator controls and any other controls and indicators.
b. Parts Books / information- that illustrate and list all assemblies, subassemblies and
components, including gaskets, hoses and fastening hardware (nuts, bolts, washers, etc.).
All EG system parts shall be clearly identified by description and associated part numbers.
c. Detailed sequence of operation instructions for both manual and automatic operation of the
complete EG system equipment.
d. Preventative Maintenance Instructions - on the complete system that cover daily, weekly,
monthly, and annual maintenance requirements and schedules including a complete
lubrication chart and information.
e. Routine Test Procedures - for all EG system equipment including all electronic and
electrical circuits and for the main AC generator.
f. Troubleshooting Chart - covering the complete engine-generator set showing description of
trouble, probable cause, and suggested remedy.
Addendum No. 3 263200 - 39
g. Recommended Spare Parts List - showing all consumables anticipated to be required during
normal operation, routine maintenance and testing, including pricing and quantities
recommended to be maintained on hand at the OWNER’S facility.
h. Project specific as field installed and EG system tested electrical schematics including
Wiring Diagrams with point to point interconnection diagrams for all interface equipment -
showing function and operational sequences of all electrical components and electrical
systems.
4. Manuals shall be furnished in suitably sized, maximum three inch, three ring binders, each binder
shall be adequately labeled on the outside and inside with the project name and location and the
contents clearly indexed. Include model, arrangement, and serial number identification for all
equipment furnished. Manuals not containing all of the information as indicated herein shall be
returned to the EG vendor for compliance provision. Five (5) sets of approved manuals shall be
transmitted to the ENGINEER for final distribution to the OWNER.
3.08 OWNER TRAINING
A. The EG vendor shall provide for complete training for the OWNER’S engineering, operation, and
maintenance personnel. Training shall include hands-on instructions. Topics covered shall include
complete EG system manual and automatic operation, control operation, schematics, wiring
diagrams, metering operations, indicators, warning lights, shutdown system, remote annunciation,
routine maintenance, remedial trouble shooting procedures, maintenance contract and warranty
explanations and details. Allow two (2) complete separate man-days for this OWNER’S training.
METHOD OF MEASUREMENT
The quantity of units to be paid for under this item shall be the number of each type installed, adjusted,
removed or replaced, complete in place, ready for operation, and accepted by the Engineer.
BASIS OF PAYMENT
No direct payment shall be made for the work described in this section. The work described in this section is
incidental to bid items in section L-109 and shall be paid for in the respective bid item of which it is a
component part.
END OF SECTION 26 32 00