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187-26 RESOLUTION
Page 1 113 West Mountain Street Fayetteville, AR 72701 (479) 575-8323 Resolution: 187-26 File Number: 2026-2730 A RESOLUTION TO AWARD BID 26-38 AND AUTHORIZE THE PURCHASE OF A NEW AIRCRAFT RESCUE AND FIRE FIGHTING VEHICLE FROM OSHKOSH AIRPORT PRODUCTS FOR DRAKE FIELD IN THE AMOUNT OF $1,112,386.00; TO AUTHORIZE THE ACCEPTANCE OF A FEDERAL AVIATION ADMINISTRATION GRANT IN THE AMOUNT OF $1,100,197.00; TO EXECUTE AMENDMENT NO. 1 TO TASK ORDER 11 WITH GARVER, LLC IN THE AMOUNT OF $7,100.00 FOR BIDDING SERVICES; TO AUTHORIZE THE MAYOR OR THE MAYOR’S DESIGNEE TO LOAN CASH FROM THE GENERAL FUND TO THE AIRPORT FUND IF NEEDED; AND TO APPROVE A BUDGET AMENDMENT BE IT RESOLVED BY THE CITY COUNCIL OF THE CITY OF FAYETTEVILLE, ARKANSAS: Section 1: That the City Council of the City of Fayetteville, Arkansas hereby authorizes Mayor Rawn to sign an grant agreement with the Federal Aviation Administration to accept a grant in the amount of $1,100,197.00 to fund 95% of the cost for the procurement of a new Aircraft Rescue and Fire Fighting (ARFF) vehicle for Drake Field, and further authorizes the Mayor to sign all documents necessary to receive these funds and any additional funds that may be awarded by the Federal Aviation Administration for this project. Section 2: That the City Council of the City of Fayetteville, Arkansas hereby awards Bid 26-38 and authorizes Mayor Rawn to sign a contract with Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. for the purchase of the ARFF vehicle in the amount of $1,112,386.00. Section 3: That the City Council of the City of Fayetteville, Arkansas hereby authorizes Mayor Rawn to execute Amendment No. 1 to Task Order 11 with Garver, LLC in the amount of $7,100.00 for bidding services. Section 4: That the City Council of the City of Fayetteville, Arkansas hereby authorizes the Mayor or the Mayor’s designee to loan cash from the General Fund to the Airport Fund if needed to cover expenses related to this item, and further authorizes the Mayor or the Mayor’s designee to repay any loan as soon as practicable when the Airport Fund receives grant-related reimbursements. Section 5: That the City Council of the City of Fayetteville, Arkansas hereby approves a budget amendment, a copy of which is attached to this Resolution. PASSED and APPROVED on September 1, 2026 Approved: _______________________________ Molly Rawn, Mayor Attest: _______________________________ Kara Paxton, City Clerk Treasurer Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Mailing address: 113 W. Mountain Street Fayetteville, AR 72701 www.fayetteville-ar.gov CITY COUNCIL MEMO 2026-2730 MEETING OF SEPTEMBER 1, 2026 TO: Mayor Rawn and City Council THROUGH: Keith Macedo, Chief Information Officer Chris Brown, Public Works Director Terry Gulley, Asst Public Works Director - Ops FROM: Jared Rabren, Airport Director SUBJECT: FYV ARFF – FAA AIG Grant Acceptance, Procurement Contract, Garver Task Order 11, Amendment 1 RECOMMENDATION: Staff requests approval for the Aviation Division to accept a Federal Aviation Administration (FAA) Grant Offer in the amount of $1,100,197.00, representing 95% of the total project cost, for the procurement of a new Aircraft Rescue and Fire Fighting (ARFF) Vehicle for Drake Field (FYV). Upon execution of the grant agreement, staff also requests authorization to execute a Procurement Contract, pursuant to Bid 26-38, with Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc., in the amount of $1,112,386.00 for the acquisition of the ARFF vehicle, and to execute Task Order 11, Amendment 1 with Garver, in the amount of $7,100.00 to provide bidding services associated with the purchase. Staff also requests approval of a budget amendment in the amount of $1,120,104, and to authorize a temporary loan from the General Fund to provide funding for this item if needed. Loan Agreement: The Mayor or Mayor's designee (Chief Financial Officer) is authorized to provide a temporary loan from the General Fund if needed to cover expenses related to this item until the Airport Fund receives grant related reimbursements from the granting agency. When the Airport Fund receives grant related reimbursements, repayment of any loan from the General Fund will be made as soon as practicable. BACKGROUND: Drake Field's AARF services are currently provided by a single E-One ARFF truck that is over 20 years old. The vehicle has required more frequent maintenance with age, and the lack of a secondary ARFF truck results in interruptions to airport ARFF services. Additionally, the FAA classifies Drake Field's current ARFF capabilities as Index A, limiting the airport’s ability to accommodate demand for larger charter aircraft. Acquisition of a new ARFF vehicle will allow Drake Field to provide reliable ARFF services and satisfy charter demand by increasing Drake Field’s ARFF Index to B. Garver was contracted to perform project administration, procurement package consultation, and contracting and delivery consultation services for this project under a previously approved Task Order 11. Bidding services were excluded from that Task Order with the understanding that City staff would pursue procurement through the HGACBuy program - however - after approval of Task Order 11, the FAA determined that this project must undergo a traditional bidding process to be eligible for AIG Grant funding. DISCUSSION: Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Mailing address: 113 W. Mountain Street Fayetteville, AR 72701 www.fayetteville-ar.gov The Aviation Division is requesting permission to 1.Accept an FAA Grant Offer in the amount of $1,100,197.00 (95% of Total Project Costs) for the procurement of an ARFF Vehicle for FYV. 2.Upon execution of the grant offer, execute a Procurement Contract with Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. in the amount of $1,112,386.00 for the procurement of an ARFF Vehicle for FYV. 3.Upon execution of the grant offer, execute Task Order 11 Amendment 1 with Garver for bidding services for the procurement of a new ARFF vehicle for FYV, in the amount of $7,100. 4.Approval of a budget amendment in the amount of $1,120,104. 5.Finance requests authorization of a loan from the General Fund to provide temporary funding related to this item if needed. Any temporary loan from the General Fund would be reimbursed as soon as practicable when the Airport receives drawdowns of grant funding. Below is a summary of the anticipated costs and funding breakdown for this grant. Administrative Fees: $617.01 Garver Task Order 11 (Engineering Fees)1: $38,000.00 FAA: $1,100,197.00 Garver TO 11 Amendment 1 (Bidding Services): $7,100.00 ADA2: $57,905.00 Procurement Contract (Oshkosh): $1,112,386.00 City: $1.01 TOTAL: $1,158,103.01 TOTAL: $1,158,103.01 1Previously approved by City Council under separate request 2Amount Estimated at this time BUDGET/STAFF IMPACT: The Aviation Division requests approval of a budget amendment in the amount of $1,120,104. This amount includes cash-flow to cover the FAA’s 95% share of billed invoices until monthly reimbursement is issued, cover the ADA’s share until reimbursement at the end of the project, and $1.01 to cover the City’s share. Staff requests approval to authorize a temporary loan from the General Fund to provide funding for this item if needed, to be fully reimbursed when the Airport receives funding from the granting agency. ATTACHMENTS: 3. Staff Review Form, 4. Budget Amendment, 5. FYV-SWG-3-05-0020-057-2026-Grant Agreement, 6. Bid 26-38, Bid Tab - Final, 7. Bid 26-38, Submittal - Oshkosh Airport Products - E, 8. Procurement Contract (Oshkosh Signed), 9. Garver Task Order 11 Amendment 1 - FYV ARFF Bidding Services Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Page 1 City of Fayetteville, Arkansas Legislation Text 113 West Mountain Street Fayetteville, AR 72701 (479) 575-8323 File #: 2026-2730 A RESOLUTION TO AWARD BID 26-38 AND AUTHORIZE THE PURCHASE OF A NEW AIRCRAFT RESCUE AND FIRE FIGHTING VEHICLE FROM OSHKOSH AIRPORT PRODUCTS FOR DRAKE FIELD IN THE AMOUNT OF $1,112,386.00; TO AUTHORIZE THE ACCEPTANCE OF A FEDERAL AVIATION ADMINISTRATION GRANT IN THE AMOUNT OF $1,100,197.00; TO EXECUTE AMENDMENT NO. 1 TO TASK ORDER 11 WITH GARVER, LLC IN THE AMOUNT OF $7,100.00 FOR BIDDING SERVICES; TO AUTHORIZE THE MAYOR OR THE MAYOR’S DESIGNEE TO LOAN CASH FROM THE GENERAL FUND TO THE AIRPORT FUND IF NEEDED; AND TO APPROVE A BUDGET AMENDMENT BE IT RESOLVED BY THE CITY COUNCIL OF THE CITY OF FAYETTEVILLE, ARKANSAS: Section 1: That the City Council of the City of Fayetteville, Arkansas hereby authorizes Mayor Rawn to sign an grant agreement with the Federal Aviation Administration to accept a grant in the amount of $1,100,197.00 to fund 95% of the cost for the procurement of a new Aircraft Rescue and Fire Fighting (ARFF) vehicle for Drake Field, and further authorizes the Mayor to sign all documents necessary to receive these funds and any additional funds that may be awarded by the Federal Aviation Administration for this project. Section 2: That the City Council of the City of Fayetteville, Arkansas hereby awards Bid 26-38 and authorizes Mayor Rawn to sign a contract with Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. for the purchase of the ARFF vehicle in the amount of $1,112,386.00. Section 3: That the City Council of the City of Fayetteville, Arkansas hereby authorizes Mayor Rawn to execute Amendment No. 1 to Task Order 11 with Garver, LLC in the amount of $7,100.00 for bidding services. Section 4: That the City Council of the City of Fayetteville, Arkansas hereby authorizes the Mayor or the Mayor’s designee to loan cash from the General Fund to the Airport Fund if needed to cover expenses related to this item, and further authorizes the Mayor or the Mayor’s designee to repay any loan as soon as practicable when the Airport Fund receives grant-related reimbursements. Section 5: That the City Council of the City of Fayetteville, Arkansas hereby approves a budget amendment, a copy of which is attached to this Resolution. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 TO: Molly Rawn, Mayor THRU: Keith Macedo, Interim Chief of Staff Staff/Contract Review Committee FROM: Jared Rabren, Airport Director DATE: August 18, 2026 SUBJECT: FYV ARFF – FAA AIG Grant Acceptance, Procurement Contract, Garver Task Order 11 Amendment 1 RECOMMENDATION: Staff requests approval for the Aviation Division to pursue the following: 1.Execute a Federal Aviation Administration (FAA) procurement grant to fund 95% of project costs for the acquisition of an Aircraft Rescue and Fire Fighting (ARFF) Vehicle for FYV. 2.Execute a Procurement Contract with Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. for the acquisition of an Aircraft Rescue and Fire Fighting (ARFF) Vehicle for FYV. 3.Execute a Task Order Amendment with Garver to provide bidding services related to the acquisition of an Aircraft Rescue and Fire Fighting (ARFF) Vehicle for FYV. BACKGROUND: Fayetteville-Drake Field AARF Aircraft Fire Fighting and Rescue services are currently provided by a single E-One ARFF truck that is over 20 years old. The vehicle has required more frequent maintenance with age, and the lack of a secondary ARFF truck results in interruptions to airport ARFF services. Additionally, the Federal Aviation Administration (FAA) classifies Drake Field current ARFF capabilities as Index A, limiting the airport’s ability to accommodate demand for larger charter aircraft. Acquisition of a new ARFF vehicle will allow Drake Field to provide reliable ARFF services and satisfy charter demand by increasing Drake Field’s ARFF Index to B. Garver was contracted to perform project administration, procurement package consultation, and contracting and delivery consultation services for this project under a previously approved Task Order 11. Bidding services were excluded from that Task Order with the understanding that City of Fayetteville was going to pursue procurement through the HGACBuy program; however, the FAA determined that this project must undergo a traditional bidding process to be eligible for the AIG Grant funding that is planned for the procurement of the ARFF truck. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 2 DISCUSSION: The Aviation Division is requesting permission to 1. Accept an FAA Grant Offer in the amount of $1,100,197.00 (95% of Total Project Costs) for the procurement of an ARFF Vehicle for FYV. 2.Upon execution of the grant offer, execute a Procurement Contract with Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. in the amount of $1,112,386.00 for the procurement of an ARFF Vehicle for FYV. 3. Upon execution of the grant offer, execute Task Order 11 Amendment 1 with Garver for bidding services for the procurement of a new ARFF vehicle for FYV. Below is a summary of the anticipated costs and funding breakdown for this grant. Administrative Fees: $617.01 Garver Task Order 11 (Engineering Fees)1: $38,000.00 FAA: $1,100,197.00 Garver TO 11 Amendment 1 (Bidding Services): $7,100.00 ADA2: $57,905.00 Procurement Contract (Oshkosh): $1,112,386.00 City: $1.01 TOTAL: $1,158,103.01 TOTAL: $1,158,103.01 1Previously approved by City Council under separate request 2Amount Estimated at this time BUDGET/STAFF IMPACT: The Aviation Division may expend up to $1,158,103.01 of its fund balance reserve. This amount includes $1,100,197.00 for cash-flow to cover the FAA’s 95% share of billed invoices until monthly reimbursement is issued, $57,905.00 for cash-flow to cover the ADA’s share until reimbursement at the end of the project, and $1.01 to cover the City’s share. Attachments: Staff Review Form FAA AIG Grant Offer Procurement Contract (Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc.) Garver Task Order 11 Amendment 01 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 City of Fayetteville Staff Review Form 2026-2730 Item ID 9/1/2026 City Council Meeting Date - Agenda Item Only N/A for Non-Agenda Item Jared Rabren 8/4/2026 AIRPORT SERVICES (760) Submitted By Submitted Date Division / Department Action Recommendation: Staff requests approval for the Airport to accept a Federal Aviation Administration (FAA) Grant Offer in the amount of $1,100,197.00, 95% of the total project cost, for the purchase of a new Aircraft Rescue and Fire Fighting (ARFF) Vehicle for Drake Field (FYV). Staff also requests authorization to execute a contract with Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc., in the amount of $1,112,386.00 for the acquisition of the ARFF vehicle, and to execute Task Order 11, Amendment 1 with Garver, in the amount of $7,100.00 to provide bidding services associated with the purchase. Staff also requests approval of a budget amendment in the amount of $1,120,104.00. Staff also requests approval to authorize a temporary loan from the General Fund to provide temporary funding for this item if needed.Budget Impact: 5550.760.3960-5802.00 5550.760.3960-5860.00 Airport Account Number Fund 05046.2501 ARFF Truck Project Number Project Title Budgeted Item?Yes Total Amended Budget $28,510.00 Expenses (Actual+Encum)$28,510.00 Available Budget $- Does item have a direct cost?Yes Item Cost $ 1,119,486.00 Is a Budget Amendment attached?Yes Budget Amendment $ 1,120,104.00 $639.00 Remaining Budget $618.00 Purchase Order Number:Previous Ordinance or Resolution #128-25 Change Order Number:Approval Date: Original Contract Number: Comments: Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 9/01/2026 Molly Rawn Mayor City Clerk Treasurer Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 City of Fayetteville, Arkansas - Budget Amendment/Adjustment (Agenda) Budget Year Division /Org2 AIRPORT SERVICES (760) BA Number 2026 Requestor:Dee Simpson BUDGET AMENDMENT/ADJUSTMENT DESCRIPTION: Staff requests approval for the Airport to accept a Federal Aviation Administration (FAA) Grant Offer in the amount of $1,100,197.00, 95% of the total project cost, for the purchase of a new Aircraft Rescue and Fire Fighting (ARFF) Vehicle for Drake Field (FYV). Staff also requests authorization to execute a contract with Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc., in the amount of $1,112,386.00 for the acquisition of the ARFF vehicle, and to execute Task Order 11, Amendment 1 with Garver, in the amount of $7,100.00 to provide bidding services associated with the purchase. COUNCIL DATE:9/1/2026 ITEM ID#:2026-2730 Holly Black 8/12/2026 9:12 AM Budget Division Date TYPE:D - (City Council) JOURNAL #: GLDATE: RESOLUTION/ORDINANCE CHKD/POSTED:/ v.2026714TOTAL1,120,104 1,120,104 Increase / (Decrease)Project.Sub# Account Number Expense Revenue Project Sub.Detl AT Account NameGLACCOUNTEXPENSEREVENUEPROJECTSUBATDESCRIPTION X 5550.760.3960-5802.00 1,112,386 -05046 2501 EX Vehicles & Equipment - base 5550.760.3960-5301.00 618 -05046 2501 EX Public Notification 5550.760.3960-5860.02 7,100 05046 2501 EX Capital Prof Svcs - Engineering/Architectural 5550.760.3940-4999.99 -19,907 RE Use Fund Balance - Current 5550.760.3960-4309.00 -1,100,197 05046 2501 RE Federal Grants - Capital -- -- -- -- -- -- -- -- -- -- -- 1 of 1 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Line #Description QTY UOM Unit Extended Unit Extended 1 1 LS $1,112,386.00 Kenny Fitch, Sr Procurement Agent Bid 26-38, Aircraft Rescue and Fire Fighting (ARFF) Vehicle BID TABULATION ______________________________________________________________________________ Trevel Young, Procurement Agent * NOTICE: Bid award is contingent upon supplier meeting minimum specifications and formal authorization by City Officials. Oshkosh Airport Products Rosenbauer Minnesota, LLC ______________________________________________________________________________ Deadline: Tuesday, June 16, 2026 at 2:00 PM Total $1,114,826.00$1,112,386.00 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Bid 26-38 Addendum 2 Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. Supplier Response Event Information Number:Bid 26-38 Addendum 2 Title:Aircraft Rescue and Fire Fighting (ARFF) Vehicle Type:Invitation to Bid Issue Date:5/24/2026 Deadline:6/16/2026 02:00 PM (CT) Notes:The City of Fayetteville is accepting sealed bids from suitable suppliers to procure a 1,500 gallon Aircraft Rescue and Fire Fighting (ARFF) Vehicle. Questions regarding this bid should be addressed to Kenny Fitch, Sr. Procurement Agent at kfitch@fayetteville-ar.gov. Contact Information Contact:Kenny Fitch - Sr Procurement Agent Address:Procurement City Hall Room 306 113 W. Mountain St. Fayetteville, AR 72701 Phone:(479) 575-8258 Email:kfitch@fayetteville-ar.gov Vendor: Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. Bid 26-38 Addendum 2Page 1 of 3 pages Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. Information Contact:Dustin Raddatz Address:1515 County Road O, Suite A Neenah, WI 54956 Phone:(920) 215-5127 Email:draddatz@airport.oshkoshcorp.com By submitting your response, you certify that you are authorized to represent and bind your company. Dustin Raddatz draddatz@airport.oshkoshcorp.com Signature Email Submitted at 6/15/2026 12:15:47 PM (CT) Supplier Note Oshkosh Striker 4x4 Delivery time: 425 Days ARO Full specification is enclosed. Feel free to reach out with any questions. Requested Attachments Signature Forms for Bid 26-38 Oshkosh Airport Products Bid 26- 38.pdf Please attach your completed forms. These documents can be found in FILE #01 - BID SPECIFICATIONS in the Attachments tab. Please be sure to include ALL required information stated in the specifications. Bid Bond for Bid 26-38 Oshkosh Bid Bond for Bid 26- 38.pdf Please attach a signed and completed copy of your bid bond. The Bid Bond must be signed by both the bidder and the surety company to be considered valid. An invalid Bid Bond shall be grounds for bid rejection. Bid bonds in the form of a cashier's check shall be delivered to City Hall, Procurement Division before bid deadline and have a copy of the cashier's check uploaded with submittal. Response Attachments Oshkosh Striker Technical Specification.pdf Oshkosh Airport Products - Striker 4x4 Technical Specification Oshkosh Airport Products Supporting Documents Bid 26.38.pdf Oshkosh Airport Products supporting documents including warranty statements and product literature. Bid Attributes 1 System for Award Management (SAM.gov) Registration Number ZHMHC2YER1X3 Vendor: Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. Bid 26-38 Addendum 2Page 2 of 3 pages Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 2 Check Yes or No: Pursuant Arkansas Code Annotated §25-1-503, the Contractor agrees and certifies that they do not currently boycott Israel and will not boycott Israel during any time in which they are entering into, or while in contract, with any public entity as defined in §25-1-503. If at any time during contract the contractor decides to boycott Israel, the contractor must notify the contracted public entity in writing. Yes, I agree No, I don't agree 3 Check Yes or No: Pursuant Arkansas Code Annotated §25-1-1002, the Contractor agrees and certifies that they do not currently boycott Energy, Fossil Fuel, Firearms, and Ammunition Industries during any time in which they are entering into, or while in contract, with any public entity as defined in §25-1-1002. If at any time during the contract the contractor decides to boycott Energy, Fossil Fuel, Firearms, and/or Ammunition Industries, the contractor must notify the contracted public entity in writing. Yes, I agree No, I don't agree 4 Addendum Acknowledgement: By selecting "I agree", you acknowledge that you have read and understand any addendums that have been issued for this bid. I agree Bid Lines 1 1,500 Gallon Aircraft Rescue and Fire Fighting (ARFF) Vehicle Quantity:1 UOM:LS Price:$1,112,386.00 Total:$1,112,386.00 Supplier Notes:Price includes 9.75% sales tax Response Total: $1,112,386.00 Vendor: Oshkosh Airport Products, a Division of Pierce Manufacturing, Inc. 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63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 City of Fayetteville, Arkansas Fayetteville – Drake Field (FYV) Bid 26-38 Aircraft Rescue and Fire Fighting (ARFF) Vehicle June 15, 2026 Oshkosh Airport Products Bid Proposal Comments We are pleased to offer our Striker 4x4 1500-gallon Aircraft Rescue and Fire Fighting vehicle in response to your invitation to bid. The proposed vehicle meets the performance and construction requirements of NFPA 1900/414, the FAA 150/5220-10F Advisory Circular and your bid specification. We are taking no exceptions to the vehicle specification. A full vehicle specification is enclosed detailing our product offering. Delivery will be 425 days after receipt of order. If further information is required, please contact: Dustin Raddatz – Senior Requirements Manager, ARFF Products Phone: (920) 215-5127 Email: draddatz@airport.oshkoshcorp.com Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 EVIDENCE OF LIABILITY INSURANCE April 1, 2026 PRODUCER Brown & Brown Insurance Services, Inc. 1200 N. Mayfair Road Suite 100 Milwaukee, WI 53226 Phone: 414-443-0000 Fax: 414-259-8448 THIS DOCUMENT IS ISSUED AS A MATTER OF INFORMATION ONLY AND CONFERS NO RIGHTS UPON THE DOCUMENT HOLDER. THIS DOCUMENT DOES NOT AMEND, EXTEND OR ALTER THE COVERAGE AFFORDED BY THE POLICIES INSURERS AFFORDING COVERAGE INSURED OSHKOSH CORPORATION 1917 Four Wheel Drive Oshkosh, WI 54902 INSUR Westchester Surplus Lines Insurance Company INSUR Twin City Fire Insurance Company INSUR Hartford Accident and Indemnity Company INSUR Hartford Fire Insurance Company INSU RER Berkley National Insurance Company COVERAGES THE POLICIES OF INSURANCE LISTED BELOW HAVE BEEN ISSUED TO THE INSURED NAMED ABOVE FOR THE POLICY PERIOD INDICATED. NOTWITHSTANDING ANY REQUIREMENT, TERM OR CONDITION OF ANY CONTRACT OR OTHER DOCUMENT WITH RESPECT TO WHICH THIS DOCUMENT MAY BE ISSUED OR MAY PERTAIN. THE INSURANCE AFFORDED BY THE POLICIES DESCRIBED HEREIN IS SUBJECT TO ALL THE TERMS EXCLUSIONS AND CONDITIONS OF SUCH INSR LTR TYPE OF INSURANCE POLICY NUMBER POLICY EFFECTIVE DATE POLICY EXPIRATION DATE LIMITS GENERAL LIABILITY EACH OCCURRENCE USD 1,000,000 A COMMERCIAL GENERAL LIABILITY G7446676A003 April 1, 2026 April 1, 2027 DAMAGE TO RENTED PREMISES (Ea. occurrence) USD 500,000 OCCURRENCE FORM MED EXP (Any one person) EXCLUDED INCL GARAGE LIABILITY PERSONAL & ADV INJURY USD 1,000,000 GENERAL AGGREGATE USD 5,000,000 PRODUCTS-COMP/OP AGG USD 3,000,000 AUTOMOBILE LIABILITY D Any Auto (Symbol 1) 83 AB S68003 October 1, 2025 October 1, 2026 COMBINED SINGLE LIMIT USD 1,000.000 A UMBRELLA LIABILITY G72515511006 April 1, 2026 April 1, 2027 EACH OCCURRENCE USD 15,000,000 Occurrence Form AGGREGATE USD 15,000,000 B C WORKERS’ COMPENSATION AND 83 WBR S68001 83 WN S68000 October 1, 2025 October 1, 2025 October 1, 2026 October 1, 2026 WORKERS COMPENSATION WC STATUTORY LIMITS E.L. EACH ACCIDENT USD 1,000,000 E.L. DISEASE – EA USD 1,000,000 E.L. DISEASE – POLICY USD 1,000,000 F Aviation Liability See Attached Schedule April 1, 2026 April 1, 2027 Each Occurrence Prod Comp/Ops Aggregate $25,000,000 $25,000,000 D GARAGEKEEPERS 83 AB S68003 October 1, 2025 October 1, 2026 Limit of Insurance USD 1,000.000 E EXCESS LIABILITY CEX09600174-13 April 1, 2026 April 1, 2027 Each Occurrence/Aggregate USD 15,000,000 ADDITIONAL INFORMATION NAMED INSURED LISTING: Oshkosh Corporation Oshkosh Commercial Products, LLC Oshkosh Defense, LLC Oshkosh HD, LLC Oshkosh Logistics Corporation Oshkosh Manufacturing, LLC Iowa Mold Tooling Co., Inc. Iowa Contract Fabricators, Inc. JLG Industries, Inc. JLG Equipment Services, Inc. Frontline Communications, a Division of Pierce Manufacturing, Inc. Oshkosh Airport Products, Division of Pierce Manufacturing, Inc. Jerr-Dan Corporation AUSA US Corp. Oshkosh Specialty Vehicles, a Division of Pierce Manufacturing, Inc. JLG Latino Americana Ltda. Kewaunee Fabrications, LLC McNeilus Companies, Inc. McNeilus Financial, Inc. McNeilus Truck and Manufacturing, Inc. Viking Truck & Equipment Sales, Inc. McIntire Fabricators, Inc. Pierce Manufacturing Inc. Pratt & Miller Engineering & Fabrication, LLC Oshkosh AeroTech, LLC Oshkosh AeroTech Oregon, Inc. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 ADDITIONAL REMARKS SCHEDULE AGENCY NAMED INSURED Oshkosh AeroTech, LLC POLICY NUMBER See Below CARRIER See Below EFFECTIVE DATE: April 1, 2026 ADDITIONAL REMARKS THIS ADDITIONAL REMARKS FORM IS A SCHEDULE TO ACORD FORM, FORM NUMBER: 25 FORM TITLE: Aviation Liability Schedule of Insurers (Insurer F) SECURITY (the “Insurers”) Insurer Policy Number NAIC Code Allianz Global Risks US Insurance Company USA000224260 35300 Starr Indemnity & Liability Company 1000189341-05 38318 National Union Fire Insurance Co. of Pittsburgh PA PL007741013-15 19445 QBE Insurance Corporation 100010221 39217 Old Republic Insurance Company MP00045905 24147 XL Specialty Insurance Company UA00019286AV26A 37885 Underwriters at Lloyds of London & Certain Insurance Companies B0507PE2600045 N/A Several Liability Notice The subscribing insurers’ obligations under contracts of insurance to which they subscribe are several and not joint and are limited solely to the extent of their individual subscriptions. The subscribing insurers are not responsible for the subscription of any co-subscribing insurer who for any reason does not satisfy all or part of its obligations. LSW 1001 (insurance) In the event of cancellation or adverse material change of the policies by Insurers, Insurers agree that such cancellation or change shall not be effective as to the Additional Insured until thirty (30) days after issuance of notice by the Insurers to the certificate holders. ACORD 101 (2008/01) The ACORD name and logo are registered marks of ACORD © 2008 ACORD CORPORATION. All rights reserved. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Proposal for Drake Field - Fayetteville Executive Airport (FYV) Prepared by Airport Sales - Direct 06/15/2026 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 1 of 36 VEHICLE PERFORMANCE FIGURES/MEASUREMENTS Balances and Clearances The vehicle weight will be distributed as equally as practical over the axles and tires. The difference in tire load between tires on any axle will not exceed 5 percent of the average tire load for that axle. The difference in load between axles will not exceed 10 percent of the load on the heaviest axle meeting NFPA 414 requirements using the 24R21 tire size. Approach & Departure Angles 30 degrees Inter Axle Clearance Angle 12 degrees Underbody Clearance 22.26 inches (565 millimeters) Under Axle Clearance at Differential Housing Bowl 16.5 inches (419 millimeters) Wall-to-Wall Turning Circle Diameter 91.2 feet (27.8 meters) Exterior Dimensions The overall vehicle height, length, and width of the vehicle will be consistent with the rated payload and operational performance. Overall Length 427 inches (10,847 millimeters) Overall Width (Excluding Mirrors) 120 inches (3,048 millimeters) Overall Height (Top of Handrails Fully Laden) 136 inches (3,454 millimeters) *Overall vehicle height and length indicated in table is with standard height handrails and rear roof access ladder equipped* Acceleration Performance The fully laden vehicle acceleration will be from 0-50 mph (0-80 km/h) in 21 - 23 seconds depending on vehicle configuration as well as road and wind conditions. The fully laden vehicle acceleration time will not exceed 25 seconds per NFPA 414 requirements. Top Speed Performance The fully laden vehicle will have a minimum top speed of 71 mph (115 km/h) on a flat, level, improved (paved) surface. Braking Performance The brake system will meet the following performance requirements at gross vehicle weight (fully laden): Service Brake: Stopping Distance From 20 mph (32 km/h) 31 feet (9.5 meters) Maximum Stopping Distance From 40 mph (64 km/h) 116 feet (35.4 meters) Maximum Hold Fully Laden Vehicle On Grade 50% Minimum Descending 50% Minimum Ascending Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 2 of 36 Emergency Brake: (Depending on vehicle configuration) Stopping Distance From 40 mph (64 km/h) 288 feet (88 meters) Maximum Parking Brake: Hold Fully Laden Vehicle on Grade 20% Minimum Descending 20% Minimum Ascending Suspension Performance An off-road, high mobility Oshkosh® TAK-4®, all-wheel independent suspension system will be provided resulting in no more than 0.5 g rms acceleration at the seat of the vehicle when traversing an 8 inch (24 centimeter) half round at 35 mph (56 km/h) without causing injury to the operating personnel, loss of vehicle control, or damage to the vehicle. The design will allow the vehicle to travel safely at minimum off-road speeds of 35 mph (56 km/h). The Oshkosh® TAK-4®, Independent suspension system design will allow for a minimum of 16 inches (406 millimeters) of total wheel travel and is NFPA414 and 150/522-10E certified. Gradeability The vehicle will be able to: • Ascend a smooth, dry, paved road having a 20 percent grade and maintain a speed of at least 8 mph (13 km/h). • Ascend and descend a dry, hard surface incline having a 50 percent grade at not less than 1 mph (1.6 km/h). • Climb a vertical wall at least 18 inches (450 millimeters) high and negotiate terrain that will deflect the opposite wheels of the truck in alternately contrary directions at least 14 inches (360 millimeters). Dynamic and Static Stability The vehicle will meet the following stability requirements: Side Slope Stability (Tilt Table Meeting SAE J2180) 30 degrees (58 percent grade) Dynamic Balance (Min. Speed on 100 foot (30 meter) Radius Circle) 22 mph (35 km/h) Capable of performing NATO double lane change at speed up to 50 mph (80 km/h) Environmental Conditions The vehicle will be capable of withstanding the following conditions without detrimental effect to the operation: • Dust particles, as encountered in desert areas • The corrosive effects of salt fog • Material decay from fungus and mildew Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 3 of 36 •Relative humidity up to 100 percent •Ambient temperature ranging from 17.6 to 122 degrees Fahrenheit (-8 to 50 degrees Celsius) •Altitude ranging from 0 to 1,968 feet (0 to 600 meters) CHASSIS DESIGN The vehicle frame will be designed to provide the required strength and torsional rigidity of the ARFF vehicle application. The chassis frame rail will be high strength steel alloy with a minimum yield strength of 80,000 psi (551,500 kPa) and a section modulus of 49.4 in3 (809 cm3). The main frame rails will be rectangular tube type with minimum dimensions of 12 inches (305 millimeters) by 4 inches (102 millimeters) with a minimum wall thickness of .47 inch (12 millimeters). Frames will use bolted-in crossmembers with class 10.9 metric fasteners. The minimum width to the outside of the main frame rails of an assembled chassis will be 36 inches (914 millimeters). The vehicle frame, suspension, and mounting of major components will provide for diagonally opposite wheel motion of up to 14 inches (360 millimeters) above the ground without raising the remaining wheels from the ground or causing interference. The integrity and longevity of the main frame rails will not be compromised by any welding of bracketry, suspension parts, or reinforcements. TOWING DEVICES Four (4) towing hooks / eyes with shackles will be attached directly to the frame rails. Two (2) will be provided at the front of the vehicle and two (2) will be provided at the rear of the vehicle. PAINT PROCESS The vehicle shall be painted per Oshkosh Airport Products procedures and standards per PQCP-0309. All aluminum components shall be pre-treated prior to paint using an aluminum conversion coating process. All parts of the vehicle shall be cleaned, treated and primed prior to assembly and final painting. The paint applied to the vehicle shall be a durable, single color acrylic urethane. CAB PAINT The cab will be painted #35 Safety Lime (FLNA 10322), the fenders will be painted #35 Safety Lime (FLNA 10322), and the skidplate inserts will be painted #99 Semi-Gloss Black (FLNA 41735). Final colors and layout will be confirmed prior to vehicle construction. BODY PAINT The body will be painted #35 Safety Lime (FLNA 10322), the chassis will be #35 Safety Lime (FLNA 10322) and the hubs will be painted #35 Safety Lime (FLNA 10322). Final paint colors and layout will be confirmed prior to vehicle construction. REFLECTIVE STRIPING / GRAPHICS Striping and lettering will be provided and installed on the vehicle. The following items will be included in the standard graphics package: •Four (4) 16 inch (406.4 millimeter) retroreflective graphic film unit numbers; one (1) on left side and of the vehicle, one (1) on the right side of the vehicle, one (1) on the rear of the vehicle, and one (1) on the front of the vehicle Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 4 of 36 • One (1) 24 inch (609.6 millimeter) retroreflective graphic film unit number on the cab roof of the vehicle • The airport name in up to 6 inch (152.4 millimeter) retroreflective graphic film lettering on the left side of the vehicle and on the right side of the vehicle • Two (2) up to 24 inch (609.6 millimeter) retroreflective graphic film airport logos/insignias, one (1) on the left side and on the right side of the vehicle • Two (2) up to 16 inch (406.4 millimeter) retroreflective graphic film fire department logos/patches, one (1) on the left side of the vehicle and on the right side of the vehicle • An 8 inch (203.2 millimeter) retroreflective graphic film horizontal band along the left side bodywork and right side bodywork • An 8 inch (203.2 millimeter) retroreflective graphic film horizontal band across the rear bodywork The numbers, lettering, airport logo and/or fire department logos can have the retroreflective graphic film substituted with vinyl to align with logo complexity, marketing, airport branding requirements or end user preferences. The graphics package will be presented to and confirmed by the end user prior to approval packet submission. LABELS The vehicle will be furnished with all informational, functional and safety related labels necessary for operating the vehicle and systems as required by local requirements. The labels will be in the English language. SWITCH LABELS Labels will be installed above or below rocker switch banks and electronic controls to indicate the function of the switches. The labels will have a black background with white lettering. Labels will be installed on the following controls (if applicable): Cab Interior Rocker Switch Labels • Agent activation • Firefighting system discharges • AC powered lighting • DC powered lighting • Upper discharge functions • Lower discharge functions • Emergency lighting • Cab interior lighting • Chassis controls • Defroster fans / heated mirror / winterization controls • Power window controls • Bus style door controls (if equipped) Cab Interior Rotary Switch Labels Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 5 of 36 • Ignition / engine start • Headlight / marker lights • Driveline lock • Electric mirror adjustment Body Rocker Switch Labels • Left structural panel function controls ENVIRONMENTAL CONDITIONS The vehicle will be capable of operation in temperatures ranging from 0 C (33 F) to 50 C (122 F). CAB ERGONOMICS AND ACCESSORIES Cab Features The cab will be 3-point mounted on rubber bushings and constructed of welded aluminum extrusions, aluminum plates and bonded fiberglass panels. The design and construction of the cab will provide the best strength to weight ratio to prevent cab collapse in the event of a vehicle rollover. The cab will comply with ECE R29-3 standards/directive for occupant protection of a commercial vehicle. The cab will include gutters of sufficient size to prevent foam and water from dripping onto the windshield and side windows during turret discharge operations. The cab will have a minimum internal volume of 275 cubic feet (7.79 cubic meters) with a lateral field of vision of 254 degrees (127 degrees left and right of center), with 90 degrees upward and 25 degrees downward visibility when measured from the center of the cab. The cab ground visibility for the driver will be a minimum nearest point of 8.8 feet (2.7 meters) in front of the vehicle. The cab will have the following features: • Control console provided between driver and officer positions • Dashboard console and gauges in front of driver position • Integrated electronic control and diagnostic systems • Interior surface coating will be a painted durable grey spatter type finish CAB VISIBILITY There will be a total of 7.8 m² (84 ft².) area for superior visibility of shatterproof automotive tinted safety glass installed in the cab for all windows certified to DOT and ECE 43. The window measurements will be as follows: 1. A tinted single-piece laminated windshield 3.99 m² (42.9 ft².). 2. Tinted tempered glass upper door window with surface area of 0.66 m² (7.15 ft².). 3. Tinted tempered glass upper rear cab window with surface area of 0.41 m² (4.44 ft².). 4. Tinted tempered glass front angled lower corner window with surface area of 0.34 m² (3.7 ft².). 5. Tinted tempered glass lower door window with surface area of 0.5 m² (4.9 ft².). Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 6 of 36 CAB DOOR WINDOWS The cab doors will be equipped with electric controlled slide type windows. There will be a control switch provided for each cab door sliding window that are accessible by the seated driver and turret operator. located on the center console. CAB MIRRORS The vehicle cab will be equipped with two (2) Rosco 8 inch x 17 inch (203 millimeters x 432 millimeters) door mounted combination upper and lower convex mirrors, one (1) located on each side of the cab. The upper flat glass mirrors and lower convex glass mirrors on each side will be heated and electrically adjustable. The horizontal rotational viewing range will be no less than 60 degrees. Electrical switches for the mirror adjustment and heating feature will be provided within easy reach of the driver. Two (2) rectangular convex lens spotter mirrors will be provided on the A pillars of the cab structure to eliminate blind spots in front of the vehicle. One (1) mirror will be mounted on the left side of the vehicle and one (1) mirror will be mounted on the right side of the vehicle. WINDSHIELD DELUGE SYSTEM The cab windshield will be equipped with a deluge system. Four (4) nozzles will be spaced across the face of the cab above the windshield to distribute water. The nozzles will be constructed from brass and have a 40 degree tapered edge flat spray pattern. The deluge system will have a 24-volt DC pump motor to draw fresh water from the vehicle water tank. Two (2) 24-volt DC valves will be incorporated in the deluge piping to supply water when activated and will automatically drain the deluge system piping when deactivated. The deluge circuit will include an in- line serviceable strainer and quarter-turn shut off valve for system maintenance. The piping drain outlet will be located behind the left front lower body compartment and will drain onto the ground. The deluge system will be activated by a backlit momentary ON/OFF rocker switch in the cab. When switched on the windshield wipers will be activated automatically while the system is in operation. The activation switch will have a pictogram applied to the surface for identification. CAB STEPS There will be a heavy duty step provided below the left side and right side cab doors. The steps will include an aggressive pattern on the stepping surface to provide high traction when entering or exiting the cab. The step design will be self-cleaning so that a maximum amount of water, snow, mud or other debris can fall off or through the step. The step will be collapsible and spring loaded to allow the step to contact obstacles and ensure that the required 30 degree angle of approach at the front of the of the vehicle and return to the default shape. CAB DOORS Access to the cab will be gained with a single hinged door located on each side of the vehicle that opens at least to a 90-degree angle. Woven nylon door check straps will be installed on each door to limit opening travel. The bottom of the cab door openings will include scuff plates for surface protection. CAB DOOR INTERIOR GRAB HANDLES The cab doors will have angled tubular grab handles with an integrated door opening mechanism. The door opening mechanism will be operable with a gloved hand and release the door latch when the Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 7 of 36 interior button/lever is depressed. The door grab handles will have a durable single stage semi-gloss black paint applied to the surface. CAB INTERIOR The cab will be weather-tight, acoustically and thermally insulated to provide noise level not to exceed 85 dB (A) at the driver's ear position. Foam-backed black textured rubber material will cover the interior floor of the cab. The rear wall of the cab will have vinyl covered foam material to dampen noise. CAB SUN VISORS There will be five (5) double swing sun visors provided across the top of the cab interior just behind the windshield. One (1) will be provided in the center for the driver seating position and two (2) will be provided on each side of the center visor for the crew positions. Each padded visor will be approximately 19.7 inches (500 millimeters) wide and 7.2 inches (183 millimeters) tall. The visors will be adjustable and covered in a dark grey vinyl material. CAB GRAB HANDLES There will be grab handles covered with cushioned and slip resistant material located inside the driver's and passenger door openings to facilitate safe entry and exit from the cab. The grab handles will be placed to ensure three-point contact can be maintained. CAB CENTER CONSOLE The cab will have an angled top center console located between the driver and turret operator seating positions. The upper surface of the center console will be angled upward toward the rear of the cab to raise the installed components to a more ergonomic height for the driver and turret operator. ROOF HATCH The roof hatch will be constructed from acrylic and will be located on the left side of the cab roof above the outermost seat. The roof hatch will have two (2) manual latches to secure the hatch closed and two (2) gas shocks to hold the hatch lid in the open position. CREW SPACE DRIVER POSITION (CENTER) The driver's seat will be a Seats, Inc., 911 Series SCBA type with an integral 3-point seat belt. The seat will be air-ride adjustable, include a fixed back design and manual forward/backward slide adjust feature. The seating material will be black vinyl resistant to wear and staining. RIGHT TURRET OPERATOR SEAT POSITION The right side turret operator/officer seat will be a Seats, Inc., 911 Series SCBA type with an integral 3- point seat belt. The seat will include a fixed back design and will be a slide adjustable, non-suspension type. The seating material will be vinyl, black in color and resistant to wear and staining. LEFT INSIDE SEAT POSITION The left inside seat will be a Seats Inc., 911 Series SCBA compatible with an integral red 3-point seat belt. The seat will have a non-adjustable design and will be fixed mounted. The seating material will be vinyl, black in color and will be resistant to wear and staining. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 8 of 36 LEFT OUTSIDE SEAT POSITION The left outside seat will be a Seats Inc., 911 Series SCBA compatible with an integral red 3-point seat belt. The seat will have a non-adjustable design and will be fixed mounted. The seating material will be vinyl, black in color and will be resistant to wear and staining. RIGHT INSIDE SEAT POSITION There will be no seat provided to the right rear of the driver seating position. CAB HVAC (HEATING, VENTILATION, AIR CONDITIONING) The cab will be heated and cooled by a dual air conditioning and heating system with two (2) separate HVAC units. The controls for the HVAC will be backlit and provided to the left of the driver seating position with: • A rotary control for temperature control from hot to cold • A rotary control for vent control to blend from full defrost to full vent • A rotary control for fan speed with OFF, LOW, MEDIUM, and HIGH positions • A button to activate air conditioning with indicator light • A button to activate the recirculate function with indicator light A Bergstrom HVAC unit will be incorporated into the structure of the cab dashboard and a remote Bergstrom HVAC unit will be mounted to the rear wall of the cab behind the driver seat. The dashboard HVAC unit will have an output of 22,300 BTU for cooling and 48,300 BTU for heating the remote HVAC unit will have an output of 19,000 BTU for cooling and 37,000 BTU for heating. Air Conditioning Operation The cab air conditioning system will be charged with HFC R134A refrigerant. The air conditioning system compressor will have a displacement of 313cc and will be driven by a serpentine belt drive mounted on the engine. Heat Operation The cab heating system will use a propylene glycol/water mixture. The cab heating system will be incorporated into the engine cooling system and will use coolant circulated by the engine water pump. SIREN / PA SYSTEM Siren Head The vehicle will be equipped with a full function siren with public address capability. The siren will be a Whelen, Model 295SL series. The siren head will be backlit for visibility in dark or low light conditions. The siren system will include a hard wired microphone. Siren Speaker There will be one (1) Whelen, Model SA315 Series 100-watt speaker mounted at the lower portion of the right front skidplate assembly. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 9 of 36 AIR HORNS There will be a set of dual high/low stutter-tone Hadley air horns mounted underneath the cab, forward of the driver. The horns will be activated by a momentary switch located at the center of the steering wheel. FOOT SWITCHES Driver Position There will be two (2) foot switches provided in the cab at the driver seating position. One (1) foot switch will activate the vehicle air horns and one (1) foot switch will activate the siren or public address system. VIDEO SYSTEMS Thermal Imaging Camera There will be a Teledyne FLIR, MD-625, NFPA 2020 compliant thermal imaging camera fix mounted to the roof turret. The thermal imaging camera will aid the driver and crew during complete darkness, severe weather, smoky, foggy or other low visibility conditions. The camera will follow the turret movement for rotation and elevation. REAR NAVIGATION CAMERA There will be a rear facing navigation camera to aid in movement while traveling in reverse or to view the area directly behind the vehicle. A compact, fixed image color camera will be provided and will feature LED infrared illuminators to enhance the visible image in low-light situations. The infrared LEDs will have automatic day/night sensing to adjust the image in all lighting conditions. The camera will be mounted at the midpoint of the rear ladder, will activate automatically when the vehicle is placed in reverse and will have a manually activated switch in the cab. The camera image will be shown on the in-cab 12 inch (304.8 mm) color display. CONTROLS All instruments, warning lights and controls relative to truck operation will be displayed to the left of the driver so that they will be useful, convenient, and visible to the driver. All instruments, warning lights and controls relative to the firefighting system will be displayed to the right of the driver for center steer so that they will be ergonomic, convenient, and visible to both the driver and the officer (turret operator). Agent activation to be clearly identified with color coded switches providing the operator immediate identification of the agents. Blue will identify water, Yellow will identify water/foam, and Purple will identify dry chemical powder. There will be a 12 inch (304.8 mm) display provided in the center of the cab control panel to aid the driver and turret operator. The display will show pump pressure, water levels, foam levels, roof turret position as well as diagnostics with fault codes. The display utilizes the Oshkosh designed control electronics which is CAN based and uses D-Series modules. The display can be user customizable and be programmed for any language. The following cab mounted controls will be provided as a minimum: • Accelerator Pedal Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 10 of 36 • Air Conditioner Controls • Brake Pedal • Color Coded Complementary Agent / System Activation • Rotary Differential Lock Control • Dome Light Switch Manual / Door Activated • Foam Concentrate Reservoir Control Valve • Headlight Switch w/ Dimmer Control • Heater / Defroster Controls • Horn Control • Master Electrical Disconnect Switch (located in engine compartment) • Panel Lights Switch with Dimmer • Parking Brake Control • Power Adjustable Mirror Control • Rotary Ignition Start/Stop Switch • Siren Switch with Microphone • Switches for Emergency Beacon(s) / Strobe(s) • Switches for Exterior Lights • Switches for Non-Emergency Amber Beacon(s) / Strobe(s) • Tilt / Telescoping Steering Wheel Column • Transmission Range Selector • Turret Control • Windshield deluge • Windshield Wiper and Washer, column mounted • Cup Holders • Hand throttle INSTRUMENTS AND WARNING LIGHTS The following instruments and warning lights will be provided in the cab: • Air Pressure (brake and other air-driven accessories) • Complementary Agent Tank-Charged Indication • Beacon / Strobe Indicator (s) • Foam Agent Tank Level Indicator • Water Tank Level Indicator • Water Pump Pressure • Low Air Pressure Warning • Compartment Door Open Indicator • Differential Lock Indicator • Engine Coolant Temperature • Engine Tachometer • Fuel Level • Headlight Beam Indicator • Speedometer / Odometer Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 11 of 36 • Voltmeter • Low Engine Coolant Audible / Visual Alarm • Digital clock • Low Oil Pressure / High Water Temperature Audible / Visual Alarm • Complementary Agent System Pressure Indicator • Two (2) 12-volt DC accessory power outlets, one (1) each side (keep alive powered) • Two (2) 5-volt DC USB A ports, one (1) each side (keep alive powered) LATERAL ACCELEROMETER There will be an electronic rollover warning system provided. The system will detect "g" forces exerted on the vehicle. A display will be integrated into the vehicle dash in view of the driver and include an audible alarm. The sensor base unit will be installed in an easily accessible location within the cab. MONITORING AND DATA ACQUISITION SYSTEM (MADAS) A Monitoring and Data Acquisition System (MADAS) which is an electronic vehicle system analyzer that constantly records preprogrammed vehicle characteristics will be installed for the collection of various performance measurements to monitor, as a minimum, the following: 1. Vehicle speed 2. Transmission gear 3. Vehicle heading 4. Lateral acceleration 5. Vertical acceleration 6. Longitudinal acceleration and deceleration 7. Brake Application 8. Engine rpm 9. Throttle position 10. Steering input 11. Vehicle braking input (pedal position and brake pressure) 12. Date, time, and location for all data collected The MADAS system will record information and store the critical period of time including 120 seconds before an event and 15 seconds afterwards. It will require a customer supplied portable PC. The MADAS system will include software to download and to use the data. The MADAS system will require no operator input, and until it is triggered by an event all of its' operation will be fully automatic. When an event occurs, the MADAS will provide a fault code to the operator on the main display screen in the cab. When active and ready to record vehicle attributes, it will report that to a visual indicator in the cab. The MADAS system will be capable of recording a minimum of thirty events. Data logger capacity will be indicated to the operator via the main display. Access to the memory for downloading, viewing or deleting will require a pass code. The data software will include native features such as graphing analyses. The system will be designed so that the data being recorded will not be lost or overwritten immediately after the incident due to the use of an emergency shut-off or a master electrical disconnect switch. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 12 of 36 ELECTRICAL SYSTEM LIGHTING AND MARKING SYSTEM The vehicle will be equipped with lighting designed and installed to be compliant with requirements of Federal Motor Vehicle Safety Standard - FMVSS 108. CLEARANCE / MARKER LIGHTING All clearance and marker lights will be LED type, 24-volt DC. The lights will be placed in the required locations at the front, sides and rear of the vehicle. A minimum of four (4) amber LED side marker lights will be located on each side of the vehicle. One (1) red LED marker light will be located on each side of the vehicle nearest to the rear. Five (5) amber LED clearance lights will be mounted at the front of the vehicle. A centered high mount red LED brake light will be installed at the rear of the vehicle and a series of five (5) red LED clearance lights will be mounted at the rear across the top of the bodywork. TURN SIGNAL INDICATORS Amber LED lights will be integrated into the headlight placed at the front bumper to function as front marker and turn signal indicator lights. Two (2) LED light assemblies will be installed at the rear of the vehicle with integrated reverse, stop, tail and turn light functions. The amber turn signal indicators will be located at the outside edge of each assembly, the red tail/brake lights will be located in the middle and clear backup lights will be located to the inside of the housing. The turn signals will be self-cancelling by the cancel cam in the steering column. HEADLIGHTS There will be two (2) FMVSS/ECE compliant LED headlights installed, one (1) on each side at the front of the vehicle. The headlights will be certified for local requirements for right-hand traffic (RHT/left-hand steering). A rotary headlight activation switch will be provided on the dashboard and a high/low beam headlight dimmer switch will be provided on the steering column. The headlights will include a daytime running light (DRL) feature. When the transmission is shifted into neutral and the parking brake is set the daytime running lights (DRL)will be deactivated automatically. HEADLIGHT ALTERNATING FLASH The high beam headlights will have an alternating flash emergency lighting function. An activation switch will be provided in the cab emergency lighting switch panel to control the high beam flash. The headlight flash switch will be enabled only when the ignition and master warning light switches are both in the on position. The alternating flash functions will automatically be deactivated when the headlight switch is active and the high beam headlights are activated. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 13 of 36 GROUND LIGHTING There will be ground lighting installed under the vehicle to illuminate the adjacent ground/work area. The ground lights will be IP 68 rated Luma Bar white LED strip lights encased in aluminum housings. There will be an ON/OFF ground lighting activation switch located in the cab and in addition, the ground lighting will only operate with the parking brake applied and transmission in neutral. The eight (8) lights will be distributed as follows: • Two (2) under the cab doors, one (1) on each side • Four (4) under the body compartments, two (2) on each side • Two (2) under the rear of the vehicle, one (1) on each side aimed rearward FOG / DRIVING LIGHTS There will be two (2) LED driving lights and two (2) LED fog lights. The lights will be mounted one (1) of each on the left side and one (1) of each on the right side in a common recessed bezel. The fog lights will be located at the front of the vehicle directly below the headlight assemblies. The fog and drive lights will be activated by switched located on the cab dashboard to the left side of the driver. SECONDARY DAYTIME RUNNING LIGHTS No secondary DRL (daytime running lights) will be provided on the front skidplates. LICENSE PLATE ILLUMINATION There will be two (2) license plate brackets with LED lights provided on the vehicle to install standard U.S. sized license plates. One (1) license plate bracket with LED illumination will be installed on the left the front skidplate and one (1) license plate bracket with LED illumination will be installed at the left rear of the vehicle. The license plate lights will be activated with the marker lights. CAB SCENE / WORKLIGHTS There will be two (2) 24-volt DC J.W. Speaker 7250T LED front worklights provided above the cab windshield. The spotlights will have a trapezoidal beam pattern with an output of 3,715 raw lumens and an output of 2,204 effective lumens. The light housings will be constructed from black polycarbonate and the lens will be clear polycarbonate. The cab worklights will be activated from an ON/OFF momentary rocker switch in the cab. SCENE / WORKLIGHTS - SIDE There will be four (4) 24-volt DC, J.W. Speaker 7250T LED side worklights provided on the vehicle. Two (2) lights will be installed on the left side of the vehicle and two (2) lights will be installed on the right side of the vehicle. Each worklight will have a trapezoidal beam pattern with an output of 3,715 raw lumens and an output of 2,204 effective lumens. The light housings will be constructed from black polycarbonate and the lens will be clear polycarbonate. The side worklights will be switched from an ON/OFF momentary rocker switch in the cab and from an external ON/OFF momentary toggle switch on each side of the vehicle. The exterior toggle switches will activate the worklights on their respective sides. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 14 of 36 SCENE / WORKLIGHTS - REAR There will be two (2) 24-volt DC J.W. Speaker LED rear worklights provided at the top of the of the vehicle bodywork. The spotlights will each have a trapezoidal beam pattern with an output of 3,715 raw lumens and an output of 2,204 effective lumens. The light housings will be constructed from black polycarbonate and the lens will be clear polycarbonate. The rear worklights will be switched from an ON/OFF momentary rocker switch in the cab and from an external ON/OFF momentary toggle switch at the rear of the vehicle accessible from ground level. The lights will automatically illuminate when the vehicle is shifted into the reverse gear. WARNING LIGHTS PERIMETER WARNING LIGHTS There will be ten (10) Whelen, 700 Series, 3 inch (76.2 millimeter) x 7 inch (178 millimeter) red LED warning lights installed around the lower perimeter of the vehicle at or near bumper height. Three (3) lights will be installed on the left side, three (3) lights will be installed on the right side, two (2) lights will be installed at the front and two (2) lights will be installed at the rear of the vehicle. The perimeter warning lights will be switched independently from upper warning lights. STANDBY LIGHTING There will be two (2) Whelen, Model L40AP, amber LED standby beacon lights with amber dome located on the roof of the vehicle. The lights will be located close to the mid-point of the water tank, one (1) on the left side and one (1) on the right side for 360-degree visibility and switched from within the cab. FRONT UPPER WARNING LIGHTS There will be two (2) Whelen, Model L40, red LED warning beacon lights installed on the roof of the vehicle near the front of the body. One (1) light will be installed on the left side and one (1) light will be installed on the right side. The lights will be activated with the upper warning light switch in the cab. UPPER REAR WARNING LIGHTS There will be two (2) Whelen, Model L40BF, red LED warning beacons installed on the roof of the engine cowling at the rear of the vehicle. One (1) beacon will be installed on the left side and one (1) beacon will be installed on the right side. The upper rear warning lights will be activated by a switch in the cab on the left side of the dash panel. COMPARTMENT LIGHTING There will be 24-volt DC white LED strip lighting provided to illuminate the interior of the compartments. The compartment lighting will be switched with the opening or closing of the roller shutter door with the ignition in the "ON" position. Each compartment will have a magnetic switch to activate and deactivate the compartment lights when the doors are opened or closed. An indicator light in the cab will illuminate when a compartment door is not in the closed position to alert the driver. If the parking brake is released, or the vehicle shifted out of neutral an audible alarm will sound and the compartment door indicator light will flash. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 15 of 36 POWER GENERATION No power generation system is required. RIGHT REAR LOWER BODY COMPARTMENT There will be a full width roll-out shelf in upper portion of the right rear lower body compartment in the place of the generator. The roll-out shelf will have a capacity of 500 lb. (227 kg) with provisions for locking in place in the fully stowed and fully deployed positions. The shelf will have a latch bar for easy one (1) handed use. SIDE MOUNTED WIDELIGHTS There will be two (2) FRC Spectra, model Q20, 20,000 lumen, 24-volt DC LED widelights with white housings provided, one (1) on each side of the vehicle. The lightheads will be adjustable, mounted on manually raised telescopic poles. The lights will be powered by the on board 24-volt DC electrical system and activated by a switch on the center console in the cab. An indicator light in the cab will illuminate when the lights are not in the stowed position to alert the driver. POWER SUPPLIES A 24-volt DC vehicle electrical system will be provided. The vehicle DC power will be supplied by a two (2) alternator charging system with a minimum output of 100 amps each. A warning system will be provided in the cab to indicate an alternator failure. The electrical system will include the following: • Four (4) group 31, 12-volt DC maintenance free, top post, flooded lead-acid batteries with a minimum of 950 CCA @ 0 degree F (each) and 190 minutes of reserve capacity @ 25 amps. • A warning label will state that connecting incorrectly to a 12-volt DC system will cause electrical system damage. • Color coded, heavy duty, insulated battery and ground cables with wire code numbers. • A backlit remote voltmeter will be installed adjacent to the batteries to read the battery state of charge. • An engine start disable switch will be provided in the left side engine compartment that will prevent the vehicle from being started from the cab during routine maintenance. • A lockable total vehicle master electrical disconnect switch rated for full vehicle current to completely de-energize the DC electrical system after the switch. • Unused electrical distribution connectors or components located on the walls of the upper and lower compartments will have sturdy protective coverings installed to prevent unwanted contact with stored gear. BATTERY CHARGER There will be a Delta Q, 120/220-volt AC, 60/50 Hz waterproof battery charger installed in the right rear engine compartment to maintain the chassis batteries. The charger will incorporate a microprocessor controller and will charge and maintain the batteries automatically. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 16 of 36 ENGINE COOLANT PREHEATER There will be one (1) 110/120-volt AC, 1500-watt engine coolant preheater with thermostat provided to heat and maintain engine temperatures of approximately 100-120 degrees Fahrenheit (38-49 degrees Celsius). The preheater will be connected to and powered by the shoreline inlet on the vehicle. RECEPTACLE INLETS There will be two (2) Kussmaul™, 20-amp, 120-volt AC shoreline inlets provided to operate the dedicated 120-volt AC circuits at right rear of the vehicle. One (1) shoreline will be connected to the battery charger and auxiliary air compressor and one (1) shoreline will be connected to the engine pre- heater. The shoreline inlets will include yellow weatherproof flip up covers. There will be a release solenoid wired to the vehicle's starter to eject the AC connectors when the engine is starting. There will be two (2) mating connector bodies supplied with the loose equipment. There will be a label installed near the inlets stating the following: • Line Voltage • Frequency • Load(s) connected to the circuit AUXILIARY START FEATURE There will be 24-volt DC positive and negative posts for jump starting the vehicle provided in the right engine access compartment. The jumper studs will be located adjacent to the battery box and will have removeable color coded protective plastic covers; a red cover for the positive stud and a black cover for the negative stud. AIR INLET RECEPTACLE There will be a pneumatic inlet with yellow weatherproof cover located at rear of the vehicle provided to maintain vehicle air pressure when connected to an external pressurized air source. The air inlet connection will be a quick disconnect type with a check valve installed to prevent air from bleeding out the connector when disconnected. There will be a release solenoid wired to the vehicle's starter to automatically eject the air inlet connection when the engine is cranked. A quick release air inlet connection will be provided and shipped with the loose equipment to install on the compressed air line and the end user's facility. AIR OUTLET RECEPTACLE No air outlet receptacle is required. PUMP AND ROLL The vehicle will be capable of pump and roll operations up to 20 mph (32 km/h) on a hard, level, improved surface. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 17 of 36 ENGINE AND ACCESSORIES ENGINE There will be a certified EPA Tier 4f, Stage IV, Scania, Model DC16, water cooled V8 design engine with a displacement of 16.4 liters. The engine will produce a maximum of 500 kw (670 hp) and electronically limited to 2,644 Nm (1,950 ft. lbs.) of torque at 2,100 RPM. The engine will have common rail fuel injection system and will be equipped with a single turbo charger with an electronic fuel management system. The engine will have a Selective Catalyst Reduction (SCR) system for the mitigation of engine emissions. The urea tank will be located in the left rear engine cover compartment with a minimum capacity of 12 gallons (45 liters). An engine high idle control will be provided to maintain the engine idle at approximately 1,450 rpm when activated. The control for this system will be safety interlocked to activate only after the transmission has been placed in the neutral position and the parking brake has been set. An electronically controlled engine governor will be provided and set to limit engine speed so that it will not exceed the maximum rpm recommended by the engine manufacturer. TRANSMISSION There will be an Allison, EVS-4800 Series, planetary type, fully automatic, electronic controlled seven- speed transmission provided. The shift pad for the transmission will be located in the cab to the left of the driver seating position with backlit switched and a gear indicator display. The transmission will be separate from the transfer case and located at the rear for easier maintenance. The seven-speed transmission creates better gear ratios, smoother shifting, and less wear and tear on drive components. The transmission level dipstick will be located in the left rear engine cover compartment. A single speed transfer case with lockable differential will be provided to supply power to both the front and rear axles. The driveline will be composed of heavy duty metal driveshafts with universal joints at each connection yoke. POWER DIVIDER There will be a power divider to allow the pump to be engaged at any speed or engine RPM and in any gear which is automatically activated for pump operation when the pump switch is engaged from the cab. When in pump mode, the pumping RPM will increase automatically only after a discharge orifice is opened, to minimize heat build-up during standby operation. ENGINE AIR CLEANER The engine will be equipped with an easily replaceable canister type single stage air filter with a pleated paper element. The engine fresh air inlet will have a bonnet installed on the intake piping to shed water and will be located on the roof of the vehicle. EXHAUST SYSTEM The vehicle will have a vertical stainless steel exhaust stack with a rain cap. The exhaust outlet will be located on the roof of the vehicle. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 18 of 36 FUEL PRIMING PUMP The vehicle fuel system will be equipped with a 24-volt DC electric fuel priming pump. The activation switch will be located on the interior of the left engine compartment near the fuel filters. MUDFLAPS There will be a .19 inch (4.8 millimeter) thick flexible rubber mud flap provided behind each wheel well position to minimize the amount of water and road debris cast behind the vehicle by the tires. The size and positioning of the mudflaps will be FMVSS and ECE compliant. CHASSIS AIR The vehicle will be equipped with a Bendix, Model AD-IS, air dryer. The air dryer module will include an integrated air dryer, a reservoir, a governor, a heater and four (4) pressure protection valves. The air dryer will incorporate a spin-off replaceable desiccant cartridge. The chassis air system will be supplied by color coded nylon tubing and will have circuit numbers printed on each section of line for easy identification. The color coding on the air lines will be as follows: • Red will represent the primary air circuit (rear brakes) • Green will represent the secondary air circuit (front brakes) • Orange will represent the parking brake and cab air inlet circuit • Yellow will represent the parking brake air delivery circuit • Blue will designate auxiliary air circuits (air-ride seats, firefighting system air supply, chassis accessories, etc.) • Black will represent the rear air inlet and air system drains FUEL TANK CAPACITY The fuel tank will be constructed from formed and welded aluminum with a fluid capacity of 80 gallons (303 liters). The fuel tank will have a bottom drain plug and the filler pipe will be located no higher than 60 inches (152 centimeters) from ground level. The fuel fill will be located on the right side of the vehicle behind a hinged access door with a push to open latch. The fuel tank cap will have provisions to install a lock to prevent the cap from being removed. An anti-drain vent valve will be installed on the fuel tank to prevent fuel spillage in the event of a rollover. A fuel water separator with drain valve will be provided for the main engine. A label will be provided near the fuel fill indicating that diesel fuel is required. FMVSS STEERING & SUSPENSION SYSTEM The front and rear axles will have adequate capacity to carry the fully loaded vehicle under all intended operating conditions with a GVWR of 62,000 pounds (28,122 kilograms). For vehicle handling, stability and off-runway performance, the axles will have an identical track width of 96 inches (244 centimeters). The axles will consist of the following: 1. Front Axle - 31,000 pounds (14,061 kilograms) rating, double reduction (axle housing and wheel end), enclosed steering drive ends, bevel gear differential with driver operated differential lock. 2. Rear Axle - 31,000 pounds (14,061 kilograms) rating, double reduction (axle housing and wheel end), bevel gear differential with driver operated differential lock. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 19 of 36 The suspension will incorporate the following design elements: 1.Upper and lower control arms will be used on each side of the axle. 2.Each axle will be equipped with an anti-roll bar for increased cornering stability. 3.Steering and non-steering axles will have an adjustable tie rod for alignment of the wheel to the center of the chassis. 4.Each wheel position will have at least one (1) coil spring and one (1) heavy-duty dual acting shock absorber. 5.All pivot and joints will be designed to meet the 20-year service life of ARFF vehicles and include only two (2) grease points per wheel and with proper Oshkosh factory alignment does not require special maintenance. An off-road, high mobility Oshkosh TAK-4, all-wheel Independent suspension system will be provided resulting in no more than 0.5 g rms acceleration at the seat of the vehicle when traversing an 8 inch (24 centimeter) half round at 35 mph (56 km/h) without causing injury to the operating personnel, loss of vehicle control, or damage to the vehicle. The design will allow the vehicle to travel safely at minimum off-road speeds of 35 mph (56 km/h). The Oshkosh TAK-4, Independent suspension system design will allow for a minimum of 16 inches (406 millimeters) of total wheel travel. The chassis will be equipped with power assisted FMVSS compliant steering that will permit manual steering to bring the fully loaded vehicle to a safe stop in the event of power assist failure. A tilt / telescoping steering wheel will be provided. BRAKE SYSTEM The vehicle will be equipped with a dual air braking system including front and rear brakes with an overall vehicle tread width of 3,048 mm (120 in.) in accordance with FMVSS 121 Legislation. The brakes will be drum type and equipped with automatic brake adjusters, to be clutch and worm drive type. The system will feature a dual type brake treadle valve with separate supply and delivery circuits. The system to include an all-wheel, split-circuit, powered-assisted service brake, a modulated emergency brake, and a parking brake. There will be a 6S-6M electronic antilock brake system with a sensor and modulator at each wheel controlled by an electronic control unit (ECU). The ECU will monitor wheel speed during braking and modulate the brakes when excessive wheel slip or lockup is detected. The ECU will blend the feedback from steering wheel ends to reduce steering wheel pull during an ABS event. There will a be provision for ABS diagnostics provided. The brake system will have the following features: 1.A Bendix AD-IS, automatic air-drying system downstream of the compressor. 2.Air brake chamber for each brake with self-adjusting mechanisms. 3.Drain on all reservoirs controlled from one (1) common location on the exterior of the vehicle. 4.Three (3) quarter-turn air drain valves will be located on the side of the vehicle below the left rear lower body compartment. 5.Visual and audible low air pressure warning device. 6.A manual parking brake valve will be installed in the cab within easy reach of the driver. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 20 of 36 The brake system will meet the following design requirements: 1.Capacity to increase air pressure in the supply and service reservoirs from 85 to 100 psi (552 to 690 kPa) when the engine is operating at the vehicle manufacturer's RPM in less than 25 seconds. 2.Capacity for buildup of tank pressure from 0 psi (0 kPa) to the pressure required to release the spring brakes within 15 seconds relying solely on vehicle air compressor. 3.Have a volume 12 times the total combined brake chamber volume at full stroke. The brake system will meet the following performance requirements at gross vehicle weight (fully laden): 1.Service Brake: (Depending on truck configuration) A.Stopping Distance from 20 mph (32 km/h) : Maximum 33 feet (10 meters) B.Stopping Distance from 40 mph (64 km/h) : Maximum 121 feet (37 meters) C.Hold Fully Loaded Vehicle: Minimum 50% Grade Ascending & Descending 2.Emergency Brake: (Depending on truck configuration) A.Stopping Distance from: 64 km/h (40 mph): Maximum 288 feet (86 meters) 3. Parking Brake: A.Hold Fully Loaded Vehicle: Minimum 20% Grade Ascending & Descending WHEEL AND TIRE ASSEMBLY The vehicle will be equipped with Michelin, Model XZL, size 24R21 all-terrain radial tires. The tires will be tubeless type with full width steel belting and will be non-directional mounted on steel wheels equipped with beadlocks. SPARE TIRE The quantity of spare tire and wheel assemblies included with the vehicle and shipped loose will be one (1) Each spare tire and wheel assembly will be composed of one (1) new and unused Michelin, Model XZL 24R21 tire and one (1) new wheel assembly with beadlocks. Each spare tire and wheel assembly will be interchangeable with any wheel position on the vehicle. WHEEL PAINT COLOR The wheels will be painted #35 Safety Lime (FLNA 10322) SHIP LOOSE BEADLOCK PRESS A beadlock press tool will be provided to aid in the removal of the beadlocks installed on the wheel/tire assemblies. The beadlock tool will be shipped with the loose equipment. UPPER MOUNTED EQUIPMENT TOP MOUNTED LADDER No ladder or vehicle mounted ladder storage brackets willll be provided. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 21 of 36 FIREFIGHTING SYSTEM COMPLEMENTARY AGENT SYSTEM DRY CHEMICAL SYSTEM Agent Container and Components There will be a 550 pound (250 kilogram) capacity dry chemical extinguishing system provided. The powder vessel will be capable of holding potassium based, sodium bicarbonate or other commercially available dry chemical fire extinguishing agents. The weight held in the powder vessel will be dependent on the density of the powder chosen by the end user. The system will include piping, valves, fittings, components necessary for the storage and discharge of dry chemical complementary agent. The container will be constructed and stamped in accordance with ASME Code for Unfired Pressure Vessels. An over pressure safety valve will be integrated into the system. The system will include the following: •Quick acting agent system activation controls will be easily accessed by the seated driver and at least one (1) other crew position. Similar controls will be located near the agent handline (if equipped). •Cab mounted pressure indicators will be installed that, when the system is activated, will allow the vehicle operator to determine the propellant reservoir pressure as well as the system operating pressure. •There will be system clean out / blowdown provisions utilizing the propellant for purging dry chemical agent from all discharge piping and hose after use, saving the remaining dry chemical powder in the vessel. •There will be a feature to "fluff" the dry chemical powder within the storage vessel to prevent caking. The procedure will not require the system to be opened or discharge any powder. •A 24-volt DC electric winch will be provided to lift and lower the nitrogen cylinder from the ground level to the stored position. The design will be such that it will allow the operator to perform the nitrogen cylinder servicing without the need for any heavy lifting. •Remote LED bar graph type pressure gauges will be provided in the cab on the firefighting display to indicate system operating pressure and the propellant cylinder pressure. Propellant, Propellant Containers and Components The propellant gas will be dry nitrogen. All propellant gas cylinders and valves will comply with United States Department of Transportation (DOT) requirements (if provided with the vehicle from the manufacturer). The propellant gas cylinder(s) will be stored vertically and will be easily loaded and removed with the assistance of the integrated lifting device and cylinder guide. One (1) propellant cylinder lifting cradle will be supplied with the system for vehicle storage of one (1) cylinder. A lifting cradle constructed from formed and welded aluminum with woven nylon lifting device will be provided. The lifting cradle will be utilized as part of the propellant cylinder storage within the compartment. After the lifting cradle is moved into the storage position there will be a bracket installed to retain the cradle. The cradle will remain installed in the vehicle until the propellant cylinder requires service or replacement. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 22 of 36 DRY CHEMICAL FILL FUNNEL There will be one (1) dry chemical fill funnel provided and shipped loose with the vehicle. The funnel will measure approximately 18 in. (457 mm) high, 17 in. (432 mm) in diameter at the top opening and 3.75 in. (953 mm) at the bottom opening. NITROGEN PROPELLANT CYLINDER There will be one (1) full 400 ft³. (11,327 liter) when pressurized to 2,640 psi (182 bar) Nitrogen cylinder(s) provided and mounted in the truck with a pressure gauge and removable carrier. All propellant gas cylinders and valves will comply with United States Department of Transportation (DOT) requirements. Propellant gas cylinder(s) will be stored vertically and must be easily loaded and removed with the assistance of an integrated lifting device and cylinder guide. SPARE NITROGEN CYLINDER There will be one (1) full 400 ft³. (11,327 liter) when pressurized to 2,640 psi (182 bar) dry nitrogen propellant gas cylinder(s) with pressure gauge provided and shipped loose with the vehicle. WATER AND FOAM SYSTEMS ELECTRONIC FOAM PROPORTIONER (EFP) SYSTEM The vehicle will be equipped with an electronic foam proportioning (EFP) system capable of metering firefighting foam at a 3% ratio within +/- 0.1% in accordance with NFPA. The system will also have provisions to easily select and change the foam proportioning rate to operate with 1%, 3%, 6%, or 8% foam concentrates. The foam proportioning rates will be selectable by the operator using the center console mounted 12 inch (304.8 millimeter) color display in the cab. The main foam system drain will have a pull-type valve drain. OSHKOSH ECO-EFP™ FOAM MEASUREMENT SYSTEM A secondary surrogate foam testing system will be provided to measure the foam proportioning system performance from every discharge on the vehicle without necessitating the actual discharge of foam into the environment. The system will measure discharge flow rates for each discharge on the vehicle. The system will be fully on-board, integrated into the vehicle plumbing and the electronic foam proportioning system. It will measure both the solution and foam fluid flow rates using only water. The system will have ability to archive foam test data for all individual discharges and provide a time and date stamp for up to (3) three years of data. An electronic display will be placed near the water pump the left rear lower body compartment. The display will provide access to view or control system settings, diagnostics functions, current and historical data and system test function. A USB port will provided to download digital data. FOAM TRANSFER PUMP There will be a Yamada, Model NDP-20, pneumatic diaphragm foam transfer pump permanently mounted in the left rear lower body compartment. The foam transfer pump will have the capability to fill or drain the vehicle foam concentrate tank. The foam transfer pump will share the primary inlet/drain connection on the left side of the vehicle and will have a selectable valve to bypass the foam transfer pump in the compartment. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 23 of 36 FOAM SYSTEM PIPING There will be two (2) 1.5 in. (38 mm) NSFHT threaded combination foam reservoir fill/drain connections provided. One (1) will be located on the left side of the vehicle below the left rear lower body compartment and one (1) will be located on the right side of the vehicle below the lower body compartments. FOAM FILL/DRAIN CONNECTION The foam fill/drain connection(s) will include two (2) 1.5 in. (38 mm) NSFHT threaded plug(s) with link chain to retain the plug(s) when removed. FOAM TANK LEVEL LIGHTS Foam tank level lights will not be provided. STRUCTURAL FIRE FIGHTING SYSTEM AND CONTROL PANEL There will be a Class "A" structural firefighting system capable of 1,000 gpm (3,785 lpm) discharge with fill from draft feature and priming pump provided. All primary pump suctions, controls and operator panel will be located in the left rear lower body compartment with a roll-up door for easy access. One (1) 6 inch (152 millimeter) NPT male pump suction inlet connection equipped with a .25 inch (6.35 millimeter) strainer will be installed in the left rear lower body compartment. A mating cap will be provided that will be capable of withstanding pressures of 500 psi (34.5 bar). A manually operated 2.5 inch (64 millimeter) pump suction inlet connection will be installed in the left rear lower body compartment. The pump suction inlet connection types will be described later in this specification. An auto-suction valve will be installed on the large diameter pump suction inlet. STRUCTURAL PANEL DISPLAY A pump operator's station with LCD display and switch panel will be provided in the left rear lower body compartment. The panel will include at a minimum the following gauges: •Engine tachometer gauge •Pump discharge pressure gauge •Pump suction pressure gauge •Engine oil pressure gauge •Engine coolant temperature gauge •Water tank level gauge •Foam tank level gauge The following functions and devices will be provided as part of the structural panel: •Manually adjustable pilot relief valve with strainer •A mechanical switch to control the operation of the priming pump (if equipped) •Structural panel activation switch •Water tank valve open / closed switch •A means of selecting water or foam induction for discharge •Pressure governor / Engine RPM control •Increase / Decrease hand throttle or system pressure switch Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 24 of 36 •Preset / Idle switch •Panel illumination •Flush mode activation switch •Red emergency engine shutdown switch STRUCTURAL PUMP SUCTION INLETS LARGE DIAMETER INLET The left large diameter pump suction inlet will have a 4.5 inch (114.3 millimeter) NSFHT male connection with female blind cap. The blind cap will have a link chain tether. SMALL DIAMETER INLET The small diameter pump suction inlet will have a 2.5 inch (64 millimeter) NSFHT female swivel coupling with a male blind plug. The blind cap will have a link chain tether. DISCHARGE PIPING There will be two (2) unregulated, manually operated, 2.5 inch (64 millimeter) structural discharges provided. One (1) will located in the left front lower body compartment and one (1) will be located in the right front lower body compartment. The discharges will have NSFHT threads and will each be equipped with pressure gauges and bleeder valves. Storage for two (2) SCBA cylinder will be provided on both left and right side front lower body compartments in the discharge panel adjacent to the discharges. DISCHARGE CAPS The two (2) 2.5 inch (64 millimeter) discharges will have NSFHT blind caps and link chain lanyards. WATER TANK There will be a water and foam tank constructed of UV resistant Polypropylene material provided. The minimum tank capacity will be 1,585 gallons (6,000 liters) of water and 222 gallons (840 liters) of foam concentrate with a top-fill opening of at least 27 inches (689 millimeters) for water and 23 inches (584 millimeters) for foam. Both reservoirs will be vented with overflow directed to the ground. The tank will be fitted with longitudinal and transverse baffles, anti-swirl baffles, a sump and isolation valve. WATER TANK LEVEL LIGHTS There will be no water tank level indicator lights provided on the upper exterior of the body or in the lower body compartments of the vehicle. WATER PUMP AND PUMP DRIVE The water pump will be a Waterous, Model CRQB (also commonly referred to as Model CR), single stage centrifugal design that meets all requirements of ICAO, NFPA 414 as well as FAA Advisory Circular 150/5220/10E. The pump will have a rated capacity of at least 2,000 gpm (7,511 lpm) at an operating pressure of 250 psi (17 bar) with suction vacuum at the manifold inlet of 9 IN-Hg. The pump gearbox will be driven by a driveline from the truck power divider. The pump and pump transmission will have the ability to run continuously without overheat issues in ambient temperatures up 122 degrees Fahrenheit (50 degrees Celsius). The pump body will be vertically split on a single plane for easy Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 25 of 36 removal of the entire impellor assembly including the bronze wear rings. A manual pump override will be provided in the left rear engine compartment. The pump will be constructed of the following materials: •Pump Body: Cast gray iron, class 35, 35,000 PSI tensile strength. •Impeller: Silicon brass, UNS C87500, 60,000 PSI tensile strength. •Impeller Shaft: 17-4 stainless steel, 135,000 PSI tensile strength. •Wear Ring: High leaded tin bronze, UNS C93200, 35,000 PSI tensile strength. The water pump will be gravity primed from the vehicle water reservoir. The vehicle will have a water piping system allowing the pump to remain primed while the water pump is not engaged. This reduces the time to discharge water when a discharge is opened providing immediate operations and a quicker response to a user input. The pump drive will be through a power divider to allow the pump to be engaged at any speed and in any gear, which is automatically activated for pump operation when the water pump switch is engaged from the cab. When in pump mode, the pumping RPM will increase automatically only after a discharge orifice is opened, to minimize heat build-up during standby operation. A pressure relief protection system will be provided to prevent over pressurization of the water piping system. An automatic pump overheat protection system will be provided that will discharge to the ground. The pump body and gearbox will be painted in a durable red primer. The entire pump will be bench tested at the original manufacturer to include 400 PSI pressure test and capacity test. A test certificate will be provided with the vehicle. PIPING, COUPLING, CONNECTIONS AND VALVES WATER FILL PIPING There will be one (1) 2.5 inch (64 millimeter) NPT male and one (1) 4.5 inch (114.3 millimeter) NPT male water fill inlet provided on the left side of the vehicle. The water fill piping will be sized to permit filling in no more than 2 minutes from an 80 psi (5.5 bar) supply source. The water fill connection types for each will be defined later in this document. The water fill piping will be constructed of welded passivated stainless steel with victaulic and threaded connections where necessary. All components in the water fill piping will be manufactured from stainless steel, brass or other corrosion resistant materials. There will be a brass unibody ball valve with stainless steel ball and manually operated quarter-turn handle to control the supply of water to the tank. Each inlet will have a .75 inch (19 mm) drain port with a quarter-turn valve. The drains will each extend through the compartment floor and drain onto the ground below the body. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 26 of 36 WATER FILL CAPS The water fill will be provided with one (1) 2.5 inch (64 millimeter) NSFHT swivel and a 2.5 inch (64 millimeter) NSFHT blind male plug with link chain lanyard. WATER FILL CAPS The water fill will be provided with one (1) 4.5 inch (114.3 millimeter) NSFHT male adapter and a 4.5 inch (114.3 millimeter) NSFHT blind cap with link chain lanyard. WATER/FOAM PIPING MATERIAL The water and foam system piping material will be 304 stainless steel. PRECONNECTED HANDLINES / CROSSLAYS PRIMARY CROSSLAY HANDLINE There will be a primary crosslay handline provided in the forward portion of the front lower body compartments. The crosslay will be transversely mounted with access from either the left or right side of the vehicle. The preconnected handline will include 200 feet (61 meters) of white 1.75 inch (44.5 millimeter) woven soft jacketed hose in 50 foot (15.2 meter) sections with 1.5 inch (38 millimeter) NHT (National Hose Thread) connections. The bezel color for the crosslay will match the hose color for easy identification. The primary crosslay will have a water/foam discharge of 95 gpm (360 l/min) at 100 psi (6.9 Bars) with the following minimum performance parameters per NFPA 1900: •Straight stream cast distance of 65.6 feet (20 meters) •Dispersed pattern cast distance of 19.7 feet (6 meters) •Dispersed pattern width of 14.8 feet (4.5 meters) A Akron Assault 4863 95 gpm (360 l/min) pistol grip nozzle will be provided on the end of the handline. A slide-out removeable tray will be provided for hose storage. The tray will be constructed from welded polypropylene plastic. The tray will have detents built into the body to hold the tray in place during vehicle movement. The primary crosslay hose sections and handline nozzle will be shipped with the loose equipment. PRIMARY PRECONNECT ACTIVATION The primary crosslay handline will have automatic activation with controls located in the cab and in the front lower body compartments near the crosslay handline. A safety interlock system will be provided that will only allow charging of the handline after all the hose has been deployed from the crosslay. An indicator light will be provided in the cab to alert operators when the crosslay hose is fully deployed from the primary preconnect hose tray. Throttle ramp up for the pumping RPM will be accomplished automatically when the handline discharge nozzle is opened. An override throttle control will be provided for the initial charging of the primary preconnected hose should the throttle not ramp up automatically due to a kink in the soft jacketed hose or flow through the handline being too low. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 27 of 36 SECONDARY CROSSLAY HANDLINE There will be a secondary crosslay handline provided in the forward portion of the front lower body compartments. The crosslay will be transversely mounted with access from either the left or right side of the vehicle. The preconnected handline will include 200 feet (61 meters) of yellow 1.75 inch (44.5 millimeter) woven soft jacketed hose in 50 foot (15.2 meter) sections with 1.5 inch (38 millimeter) NHT (National Hose Thread) connections. The bezel color for the crosslay will match the hose color for easy identification. The secondary crosslay will have a water/foam discharge of 95 gpm (360 l/min) at 100 psi (6.9 Bars) with the following minimum performance parameters per NFPA 1900: •Straight stream cast distance of 65.6 feet (20 meters) •Dispersed pattern cast distance of 19.7 feet (6 meters) •Dispersed pattern width of 14.8 feet (4.5 meters) A Akron Assault 95 gpm (360l/min) pistol grip nozzle will be provided on the end of the handline. A slide-out removeable tray will be provided for hose storage. The tray will be constructed from welded polypropylene plastic. The tray will have detents built into the body to hold the tray in place during vehicle movement. The secondary crosslay hose sections and handline nozzle will be shipped with the loose equipment. SECONDARY PRECONNECT ACTIVATION The secondary crosslay handline will have automatic activation with controls located in the cab and in the front lower body compartments near the crosslay handline. A safety interlock system will be provided that will only allow charging of the handline after all the hose has been deployed from the crosslay. An indicator light will be provided in the cab to alert operators when the crosslay hose is fully deployed from the secondary preconnect hose tray. Throttle ramp up for the pumping RPM will be accomplished automatically when the handline discharge nozzle is opened. An override throttle control will be provided for the initial charging of the secondary preconnected hose should the throttle not ramp up automatically due to a kink in the soft jacketed hose or flow through the handline being too low. LOWER DISCHARGE LOW ATTACK BUMPER TURRET There will be a front bumper mounted Elkhart Brass Scorpion turret installed on a low attack boom. The lower discharge will have water/foam discharge rates of 375/750 gpm (1,420/2,840 lpm) with a minimum straight stream cast distance of 190 feet (58 meters). The bumper turret will have the following design and performance features: TURRET SWEEP ASSEMBLY The turret sweep assembly will consist of two (2) swivel joints allowing the turret to sweep in both horizontal and vertical planes. The horizontal axis rotation will allow the turret discharge to be directed at least 90 degrees to either side of center for a minimum of 180 degree horizontal sweep. The elevation axis will allow the nozzle to be elevated at least 45 degrees above the horizontal and be Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 28 of 36 depressed to discharge agent within 30 feet (9 meters) of the front of the vehicle with the boom in the fully raised position. The turret assembly will be equipped with an auto leveling feature to maintain a consistent turret discharge angle regardless of the position of the boom mechanism during raising or lowering operations. Both the horizontal and vertical drive motors will be permanent magnet type, 24-volt DC electric gear motors and will have a clutch mechanism and/or limit switches to prevent damage to the motors at rotation limits. The motors will be sealed to NEMA 4 requirements. CONTROLS An electronic joystick control will be provided in the cab located within easy reach of the driver and turret operator/officer seating positions with integrated switches for the following: •Water/Foam discharge activation with LED indicator light (momentary or maintained) •Water/Foam discharge rate with LED indicator light, if applicable •Auxiliary agent activation with LED indicator light, if applicable •Nozzle pattern from straight stream to fully dispersed (fog pattern) The joystick fore/aft and left/right inputs will be used to control the movement of the turret position on the X and Y axes. The turret movement speed in the horizontal and vertical planes will be proportional to the amount of input angle applied to the joystick. A switch panel will be installed directly behind the joystick with rocker switches for the following functions: •Turret deploy/stow •Turret oscillate activation •Turret mounted floodlight activation, if applicable •Low attack boom up/down movement activation The rocker switches will be backlit and will be dimmable in tandem with all other cab control switch backlighting. The normal backlighting color will be white and should a malfunction occur, the switch backlighting color will change to red to indicate there is a fault with the control or turret for the lower discharge. LOW ATTACK BOOM DESIGN The low attack assembly will be capable of being lowered from the stored position near bumper height to the fully lowered position with the centerline of the turret discharge approximately 24 inches (610 millimeters) above the ground. The low attack boom will utilize a 24-volt DC motor to drive a hydraulic pump when actuated. The hydraulic pump will power two (2) hydraulic cylinders to lower and raise the boom assembly. A linear potentiometer and a proximity switch will be used to determine and communicate the position of the low attack boom during operation with the vehicle firefighting system. The turret assembly will be attached to the front bumper of the vehicle and will be mounted onto the low attack boom. The turret mounting and boom will be adequately reinforced to sustain all anticipated loads and reaction forces when the bumper discharge is activated. The design will allow the turret and Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 29 of 36 nozzle to be stored in a position providing minimum protrusion from the front of the vehicle to maintain a 30 degree angle of approach. LOWER DISCHARGE NOZZLE NASP HYDROCHEM NOZZLE A Williams Ranger hydrochem nozzle will be provided on the lower discharge with variable pattern control and an automatic flow mechanism. The auto flow mechanism will maintain consistent discharge pressure and flow whether in the straight stream or fully dispersed (fog) pattern. The nozzle will be a non-air aspirating (NASP) type with 24-volt DC powered electric infinitely variable pattern actuation for straight stream or fog pattern selection. To maximize distance and accuracy of dry the chemical discharge, the dry chemical powder will be entrained within the water stream. The dry chemical agent discharge rate of the nozzle will be a minimum of 16 pounds (7 kilograms) per second. The nozzle patterns will meet or exceed all performance requirements defined in the latest edition of NFPA-414. LOWER DISCHARGE LIGHTING There will be one (1) J.W. Speaker, model 7250S 24-volt DC LED spotlight(s) provided on the bumper turret. The spotlight(s) will be mounted to a bracket above the top of the turret and nozzle of the lower discharge. The J.W. Speaker light will have a spot beam pattern with an output of 3,715 raw lumens and an output of 2,174 effective lumens. The light housing will be constructed of black polycarbonate and the lens will be clear polycarbonate. The spotlight(s) will follow the bumper turret movements on the vertical and horizontal axes and will be controlled by a switch bank located near the bumper turret joystick. UPPER MOUNTED DISCHARGE ROOF TURRET There will be a high volume Elkhart Brass Sidewinder turret installed on the roof of the vehicle. The upper discharge will have a water/foam flow discharge rate of 375/750 gpm (1,420/2849 lpm) with a minimum straight stream cast distance of 190 feet (58 meters). The turret will include the following design and performance features: TURRET SWEEP ASSEMBLY The nozzle sweep assembly will consist of two (2) separate swivel joints allowing the nozzle to sweep in both the horizontal and vertical planes. The horizontal rotation axis will allow the nozzle to be directed at least 135 degrees to either side of center for a minimum of 270 degrees of horizontal sweep. The vertical elevation axis will allow the nozzle to be elevated at least 45 degrees above horizontal and be depressed 15 degrees below horizontal. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 30 of 36 Both horizontal and vertical drive motors will be permanent magnet type, 24-volt DC electric gear motors and will be with a clutch mechanism and/or limit switches to prevent damage to the motors at rotation limits. The motors will be sealed to NEMA 4 requirements. CONTROLS An electronic joystick control will be provided in the cab located within easy reach of the driver and turret operator/officer seating positions with integrated switches for the following: •Water/Foam discharge activation with LED indicator light (momentary or maintained) •Water/Foam discharge rate with LED indicator light, if applicable •Auxiliary agent activation with LED indicator light, if applicable •Nozzle pattern from straight stream to fully dispersed (fog pattern) The joystick fore/aft and left/right inputs will be used to control the movement of the turret position on the X and Y axes. The turret movement speed in the horizontal and vertical planes will be proportional to the amount of input angle applied to the joystick. A switch panel will be installed directly behind the joystick with rocker switches for the following functions: •Turret deploy/stow •Turret oscillate activation •Turret mounted floodlight activation, if applicable The rocker switches will be backlit and will be dimmable in tandem with all other cab control switch backlighting. The normal backlighting color will be white and should a malfunction occur, the switch backlighting color will change to red to indicate there is a fault with the control or turret for the upper discharge. TURRET BODY DESIGN The turret body assembly will be made from hard anodized Elk-O-Lite aluminum alloy for long life and corrosion resistance. The turret assembly and mounting will be adequately reinforced to sustain all anticipated loads and reaction forces when discharging. The design will allow the turret to be stowed in compact a position. UPPER DISCHARGE NOZZLE NASP HYDROCHEM NOZZLE A Williams Ranger hydrochem nozzle will be provided on the upper discharge with variable pattern control and an automatic flow mechanism. The auto flow mechanism will maintain consistent discharge pressure and flow whether in the straight stream or fully dispersed (fog) pattern. The nozzle will be a non-air aspirating (NASP) type with 24-volt DC powered electric infinitely variable pattern actuation for straight stream or fog pattern selection. To maximize distance and accuracy of dry the chemical discharge, the dry chemical powder will be entrained within the water stream. The dry chemical agent discharge rate of the nozzle will be a minimum of 16 pounds (7 kilograms) per second. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 31 of 36 The nozzle patterns will meet or exceed all performance requirements defined in the latest edition of NFPA-414. UPPER DISCHARGE LIGHTING There will be one (1) J.W. Speaker, model 7250S 24-volt DC light emitting diode (LED) spotlight(s) provided on the roof turret. The spotlight(s) will be mounted to a bracket above the top of the turret and nozzle of the upper discharge. The J.W. Speaker light will have a spot beam pattern with an output of 3,715 raw lumens and an output of 2,174 effective lumens. The light housing will be constructed of black polycarbonate and the lens will be clear polycarbonate. The spotlight(s) will follow the roof turret movements on the vertical and horizontal axes and will be controlled by a switch bank located near the roof turret joystick. JOYSTICK LOCATION The turret control joysticks will be located on top of the center console between the driver and turret operator seating positions. The lower discharge joystick and switch panel will be mounted on the left side of the center console, nearest the driver and the upper discharge joystick and switch panel will be mounted on the right side of the center console, nearest the turret operator. UNDERTRUCK NOZZLES There will be four (4) undertruck nozzles provided to discharge water/foam beneath the vehicle as well as the inner sides of the wheels and tires spaced in a pattern from the front axle to the rear axle of the chassis. The nozzles will be brass construction and will be capable of flowing 19 gpm (72 lpm) each with a total flow of 76 gpm (288 lpm). The undertruck nozzles will be activated by a switch in the cab. BODY COMPONENTS COMPARTMENTS The body compartments will be weather-tight, vented and drained to allow collected water to run out under the vehicle. Each compartment will be equipped with Gortite brand roller shutter type doors. The doors will have replaceable aluminum slats with an anodized finish. The door lift bar will be constructed from round stainless steel and will have adequate room to be operated with a gloved hand. The spring loaded compartment door roller mechanism will be 3 inches (7.62 mm) in diameter to provide maximum interior space. The vehicle will have adequate compartment space to enclose the firefighting systems and storage of rescue equipment. The body construction will include one (1) upper body compartment and two (2) lower body compartments per side for a total of three (3) on the left and three (3) on the right. The lower compartments will have minimum door opening sizes of 50 inches (127 cm) in height and 62 inches (157.4 cm) in width. The total compartment space will be = 303.33 ft³. (8.59 m³) The left side compartment interior dimensions will be the following: Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 32 of 36 1.Left side upper: 27 inches (685.8 mm) high x 30 inches (762 mm) wide x 28 inches (711.2 mm) deep = 13.125 ft³. (.37 m³) 2.Left side front lower: 50inches (1,270 mm) high x 63 inches (1,600.2 mm) wide x 38 inches (965.2 mm) deep = 69.27 ft³. (1.96 m³) 3.Left side rear lower: 50 inches (1,270 mm) high x 63 inches (1,600.2 mm) wide x 38 inches (965.2 mm) deep = 69.27 ft³. (1.96 m³) The right side compartment interior dimensions will be the following: 1.Right side upper: 27 inches (685.8 mm) high x 30 inches (762 mm) wide x 28 inches (711.2 mm) deep = 13.125 ft³. (.37 m³) 2.Right side front lower: 50 inches (1,270 mm) high x 63 inches (1,600.2 mm) wide x 38 inches (965.2 mm) deep = 69.27 ft³. (1.96 m³) 3.Right side rear lower: 50 inches (1,270 mm) high x 63 inches (1,600.2 mm) wide x 38 inches (965.2 mm) deep = 69.27 ft³. (1.96 m³) The compartments will be fabricated from formed, welded and riveted aluminum sheet material. The interior of the compartments will be chemically pre-treated and painted with a durable grey spatter type textured finish. COMPARTMENT MATTING The vehicle will have matting placed in the bottom of each body compartment and the bottom of each shelf. The matting will be extruded PVC type or approved equivalent. The matting will be impervious to water or foam. The matting will afford some amount of protection for the floor finish and keep objects from direct contact with the shelving and compartment floor. The matting will allow water to flow to any drains or lowermost part of the compartment floor. REAR ACCESS LADDER There will be a sturdy vertical ladder attached at the center of the vehicle at the rear of the vehicle to provide access to the roof. The ladder will have a folding design so the lower most section can be stowed out of the way. The folding section will have a positive latching system with latches on both sides to keep the ladder safely in place. The ladder will be constructed from high-grip knurled aluminum material. HANDRAILS There will be extruded aluminum slip-resistant handrails or guardrail at all steps, walkways, and elevated workstations. RUNNING BOARDS, STEPS, AND WALKWAYS Running boards, step surfaces, ladder rungs, walkways, and catwalks will have anti-skid treads. REAR ENGINE ACCESS DOORS Walk-in access to the engine, cooling system and electrical components will be provided on each side of the vehicle by large, vertical roller shutter type doors. The doors will have aluminum slats with an anodized finish. The individual door slats will be replaceable. The opening lift bar will be constructed from stainless steel and will be an easy to open with a gloved hand. An audible alarm will activate in the cab when doors are opened and vehicle is shifted out of neutral or the parking brake released. A heavy Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 33 of 36 duty manually deployed step will be provided for maintenance access to the engine compartments. The steps will have a pin to retain them in the stowed position and will tilt down into place; one (1) on the left side of the vehicle and one (1) on the right side of the vehicle. LEFT UPPER COMPARTMENT A dry chemical hose reel will be provided in the left upper body compartment. The dry chemical reel will be equipped with 150 feet (45.7 meters) of 1 inch (25.4 millimeter) diameter booster hose. The hose reel will include a 24-volt DC electric rewind motor with manual rewind provisions and a tension device to prevent the unreeling of the hose. Roller guides will be provided to assure ease of deployment when hose is taken off the reel. A manual rewind handle will be securely stored near the cord reel within the compartment. They handline nozzle will be capable of 5 - 7 pounds per second (2.3 -3.2 kilograms per second) discharge rate of dry chemical powder with a minimum of straight stream pattern of 50 feet (15 meters). A control at the reel will allow charging of the dry chemical to the handline and charging of the dry chemical tank. A blow down control will be provided in the cab. RIGHT UPPER COMPARTMENT TILT DOWN TRAY There will be one (1) fixed height, tilt-down, slide out tray provided in the right upper body compartment. LEFT FRONT LOWER COMPARTMENT There will be one (1) height-adjustable fixed shelf mounted in the left front lower body compartment. The shelf will have exterior dimensions of 42.9 inches (1,089.7 millimeters) wide and 29 inches (736.6 millimeters) deep. The left, right, front, and rear sides of the shelf will be 2.5 inches (64 millimeters) high. The shelf will be constructed of .188 inch (5 millimeter) thick formed aluminum with welded corners and will be painted with a mulitspec paint to match the compartment interior. The corners of the shelf will be open to allow water to drain out. The weight capacity of the shelf will be 250 lbs. (113 kg). RIGHT FRONT COMPARTMENT There will be one (1) height-adjustable fixed shelf mounted in the right front lower body compartment. The shelf will have exterior dimensions of 13.88 inches (352.6 millimeters) wide and 24.38 inches (620 millimeters) deep. The left, right, front, and rear sides of the shelf will be 2.5 inches (64 millimeters) high. The shelf will be constructed of .188 inch (5 millimeter) thick formed aluminum with welded corners and will be painted with a mulitspec paint to match the compartment interior. The corners of the shelf will be open to allow water to drain out. RIGHT REAR COMPARTMENT FIXED SHELF There will be one (1) height-adjustable fixed shelf provided in the right rear lower body compartment. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 34 of 36 MANUALS The manuals provided will be in a commercial format utilizing primarily line art for parts identification/assembly drawings and a combination of line art and photographs for service and operations related information. Manuals will be identified with a title page to distinguish them from one another. WEB BASED SUPPORT A 24-hour web-based parts and service system will be accessible via an internet browser. Features of this website will include the following: •A user-specific, secure login •Access to digital copies of service bulletins and technical instructions •Access to digital copies of vehicle-specific operator and service manuals, schematics, service diagrams, and parts books •An aftermarket parts catalog with live inventory level information •A customer support contact page OPERATOR'S MANUAL One (1) hard copy and one (1) digital copy on USB flash drive of the vehicle operator's manual will be provided in the English language. The operator's manual will provide all information required for the safe, efficient operation of the vehicle fire extinguishing systems, equipment, special attachments or auxiliary support equipment. The operator's manual will include: •Drawings and descriptions of locations and functions for all controls and instruments •Safety information consistent with NFPA and OSHA safety standards •All operational checks, inspection procedures, and adjustments prior to putting the vehicle into service upon receipt from the manufacturer •Disabled vehicle towing procedure •Tire changing procedure •Tie-down procedures/lashing for vehicle transport via lowboy trailer •Step by step procedures and descriptions to operate the vehicle, firefighting systems, and auxiliary equipment •Draining, flushing, re-servicing, etc. post operation procedures •Operator daily maintenance inspection checklist and basic troubleshooting procedures •Periodic and preventative maintenance schedule in hours, miles, time period, etc. The operator's manual will contain line art drawings of the left side, right side, front, and rear of the vehicle exterior showing basic dimensions and weights. The weights provided will be total vehicle and individual axle weights when unladen (no agent, occupants or equipment). SERVICE AND MAINTENANCE MANUAL One (1) hard copy and one (1) digital copy on USB flash drive of the service and maintenance manual will be provided in the English language. The manual will cover vehicle maintenance, troubleshooting and repair procedures ranging from minor to major services. The manual will identify all special tools and testing equipment for inspection, servicing and maintenance. The manual will contain: Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 35 of 36 •Performance specifications •Tolerances •Fluid capacities •Current, voltage and resistance data •Test procedures •Illustrations and exploded views of assemblies •Table of contents •Alphabetical index •Preventative maintenance schedule •Required periodic maintenance schedule •Lubrication points and service intervals A set of the following schematics will be included with the service and maintenance manual: •Full vehicle electrical diagrams in color •Full vehicle water/firefighting system/plumbing diagrams •Full vehicle pneumatic diagrams in color •Full vehicle hydraulic diagrams in color PARTS MANUAL One (1) hard copy and one (1) digital copy on USB flash drive of the parts manual will be provided in the English language. The parts manual will provide the necessary information to locate and identify the parts and quantities of parts/hardware of vehicle assemblies and components. The parts manual will contain: •Exploded views of parts/assemblies/subassemblies/special equipment •Drawings with reference numbers for part identification •Description and quantity of each component used in an assembly •Size, thread information, and other information of non-standard hardware (bolts, nuts, washers, etc.) •Size, thread information, torque specifications and other information of non-standard fittings, lubricants or special components •A numerical index VEHICLE FAMILIARIZATION TRAINING An Oshkosh representative will be on-site for vehicle training and familiarization. Firefighting agents and required propellants are not provided for training purposes. For the duration of the training period only water will be used as an extinguishing agent. After delivery of the vehicle to the airport, the manufacturer will provide the services of a qualified technician for up to five (5) consecutive days for training. The training schedule will be optimized to cover all necessary shift schedules to maximize attendance during the course. During the training there will be several opportunities provided by the trainer to allow each shift to complete the vehicle training requirements. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 36 of 36 The trainer will provide thorough instruction in the use, operation, maintenance, and testing of the vehicle. This setup includes operator training for the primary operators, which will give them sufficient knowledge to train other personnel in the functional use of all firefighting and vehicle operating systems. The training will cover, but not be limited to: •Course outline •Vehicle specifications (dimension, agent capacities, etc.) •Vehicle familiarization (component location, storage areas, etc.) •Firefighting agent system operation •Operational procedures/hazards •Daily and routine maintenance checks •Hands-on operational training •Critical performance items •Critical maintenance items •Emergency/equipment failure procedures Prior to concluding the course, the trainer will review the maintenance instructions with the necessary personnel to acquaint them with the required checks and procedures to ensure maximum performance and up time. The trainer will also share how to obtain product support and service for the vehicle after the training is complete. The training course will include written operating instructions, electronic training aids (videos/power point), or other graphic representations to depict the step-by-step operation of the vehicle. The written instructions will include materials that can be used to train subsequent new operators. ALLISON TRANSMISSION WARRANTY A five (5) year Allison transmission will be provided. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 09/01/2026 Molly Rawn Mayor City Clerk Treasurer 09/01/2026 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Task Order 11 Amendment No. 1 1 of 2 FYV ARFF Bidding Services Garver Project No. 2402545 APPENDIX A-11.1 AMENDMENT TO TASK ORDER 11 FAYETTEVILLE – DRAKE FIELD AIRPORT AIRCRAFT RESCUE AND FIRE FIGHTING (ARFF) VEHICLE ACQUISITION Project No. 2502545 TASK ORDER AMENDMENT NO. 1 This Task Order Amendment No. 1 (“Amendment”), made as of , shall amend the original Task Order 11 between the CITY OF FAYETTEVILLE of Fayetteville, Arkansas hereinafter referred to as “CITY OF FAYETTEVILLE” and Garver, LLC, hereinafter referred to as “Garver”, dated May 20, 2025 referred to in the following paragraphs as the “Task Order.” This Amendment adds professional services for the bidding of the Aircraft Rescue and Fire Fighting (ARFF) Vehicle Acquisition project. Garver will provide professional services as described herein. Terms and conditions of the Task Order not modified herein remain unchanged and in full force and effect. The Task Order is hereby modified as follows: SECTION 1 – SCOPE OF SERVICES Garver’s scope of services is described in attached Appendix A-11.1. SECTION 2 – PAYMENT For the services set forth under SECTION 1 – SCOPE OF SERVICES, CITY OF FAYETTEVILLE will pay Garver on a lump sum basis as shown in the following table. The CITY OF FAYETTEVILLE represents that funding sources are in place with the available funds necessary to pay Garver. The table below presents a summary of the fee amounts and fee types for this Amendment. WORK DESCRIPTION FEE AMOUNT FEE TYPE Bidding Services $7,100.00 LUMP SUM TOTAL FEE $7,100.00 The lump sum amount to be paid under this Work Order is $7,100.00. For informational purposes, a breakdown of Garver’s estimated costs is included herein with approximate current hourly rates for each employee classification. 9/01/2026 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Task Order 11 Amendment No. 1 2 of 2 FYV ARFF Bidding Services Garver Project No. 2402545 Expenses other than salary costs that are directly attributable to performance of our Services will be billed as follows: 1. Direct cost for travel, long distance and wireless communications, outside reproduction and presentation material preparation, and mail/courier expenses. 2. Charges similar to commercial rates for reports, plan sheets, presentation materials, etc. 3. The amount allowed by the federal government for mileage with an additional $0.05 for survey trucks/vans. Additional Services (Extra Work). For services not described or included in SECTION 1 – SCOPE OF SERVICES, but requested by the CITY OF FAYETTEVILLE in writing the CITY OF FAYETTEVILLE will pay Garver as expressly set forth in the applicable Amendment. SECTION 3 – APPENDICES 3.1 The following Appendices are attached to and made a part of this Amendment: 3.1.1 Appendix A-11.1 – Scope of Services 3.1.2 Appendix B-11.1 – Manhour tables This Amendment may be executed in two (2) or more counterparts each of which shall be deemed an original, but all of which together shall constitute one and the same instrument. Approval and acceptance of this Amendment, including attachments listed in SECTION 3 – APPENDICES, shall incorporate this document as part of the Task Order. Garver is authorized to begin performance upon receipt of a copy of this Amendment signed by the CITY OF FAYETTEVILLE. The effective date of this Amendment shall be the last date written below. CITY OF FAYETTEVILLE GARVER, LLC By: By: Signature Signature Name: Name: Printed Name Printed Name Title:Title: Date: Attest: Attest: Adam Roberson Aviation Central - West Director Molly Rawn Mayor 09/01/2026 Kara Paxton, City Clerk Treasurer Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Appendix A-11.1 – Scope of Services FYV ARFF Bidding Services Garver Project No. 2402545 APPENDIX A-11.1 (SCOPE OF SERVICES) Generally, the Scope of Services includes the following professional services for procurement of one Airport Rescue and Fire Fighting (ARFF) vehicle at Drake Field – Fayetteville Airport. Procurement is anticipated to include one (1) FAA compliant ARFF truck that would carry fluorine-free firefighting agent and 1,500 gallons of water and provide Index B ARFF coverage. •Bidding Services 1. BIDDING SERVICES 1.1. Bidding. Garver will assist the Owner in advertising for and obtaining bids or negotiating proposals for one prime contract for equipment procurement; and, where applicable, maintain a record of prospective bidders to whom Bidding Documents have been issued, attend a virtual pre-bid conference and receive and process deposits for Bidding Documents. The Owner will prepare and submit the advertisement, pay all advertising costs outside of this contract, and manage the bid posting for the bidding of this project. 1.2. Garver will issue addenda as appropriate to interpret, clarify or expand the Bidding Documents. Garver will consult with and advise the Owner as to the acceptability of subcontractors, suppliers and other persons and organizations proposed by the prime manufacturer(s) (herein called "Manufacturer(s)") for those portions of the work as to which such acceptability is required by the Bidding Documents. Garver will consult with the Owner concerning the acceptability of substitute materials and equipment proposed by Manufacturer(s) when substitution prior to the award of contracts is allowed by the Bidding Documents. 1.3. Garver will attend the bid opening, assist the Owner in evaluating bids or proposals, and assist in assembling and awarding contracts for equipment and services. Garver will assist the Owner in the execution of all contract documents and furnish a sufficient number of executed documents for the Owner, Manufacturer and FAA. 2. PROJECT DELIVERABLES 2.1. The following deliverables will be submitted to the parties identified below. Unless otherwise noted below, all deliverables shall be electronic. •100% Issued for Bid Specifications to the Owner and FAA. •Issued for Construction Specifications to the Owner, Manufacturer, and FAA. •Other electronic files as requested. 3. ADDITIONAL SERVICES 3.1. The following items are not included under this agreement but will be considered as additional services to be added under Amendment if requested by the Owner. •Redesign for the Owner’s convenience or due to changed conditions after previous alternate direction and/or approval. Changed conditions may include, but are not limited to major changes to pavement, building, or utility alignments. •Deliverables beyond those listed herein. •Engineering, architecture, or other professional services beyond those listed herein. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Appendix A-11.1 – Scope of Services FYV ARFF Bidding Services Garver Project No. 2402545 •Environmental Handling and Documentation, including but not limited tot ARFF testing or monitoring. •ARFF Station design or modification services. •Change orders required for reasons outside of Garver’s control. •Acquisition of “Turnout” or “Bunker” gear. •Administrative services typical to FAA construction project including payroll & DBE compliance review. •Fabrication Administration Services including submittal review, RFI responses, or manufacturer payment coordination. •Pre-delivery equipment inspection at the manufacturing facility. •Equipment testing or certification. •Services after equipment acceptance not specifically identified, such as warranty follow-up and operations support. 4. SCHEDULE 4.1. Garver shall begin work under this Agreement upon execution of this Agreement and shall complete the work within a mutually agreeable schedule with the Owner. Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 Appendix B-11.1 City of Fayetteville FYV ARFF Bidding Services Bidding Services WORK TASK DESCRIPTION E-4 E-3 E-2 E-1 AM-2 AM-1 T-1 hr hr hr hr hr hr hr 1.Civil Engineering Coordination with FAA 2 4 2 6 1 4 1 4 1 1 2 2 1 2 2 4 Subtotal - Civil Engineering 0 9 24 0 6 0 0 Hours 0 9 24 0 6 0 0 SUBTOTAL - SALARIES:$7,068.00 DIRECT NON-LABOR EXPENSES Document Printing/Reproduction/Assembly $25.00 Postage/Freight/Courier $7.00 SUBTOTAL - DIRECT NON-LABOR EXPENSES:$32.00 SUBTOTAL:$7,100.00 SUBCONSULTANTS FEE:$0.00 TOTAL FEE:$7,100.00 Docusign Envelope ID: 63870A09-A886-82E7-82C6-0235D745C978 3-05-0020-057-2026 U.S.Department Airports Division FAA ASW-630 of Transportation Arkansas/Oklahoma 10101 Hillwood Pkwy Federal Aviation Airports District Office Fort Worth,TX 76177 Administration Southwest Region August 6, 2026 The Honorable Molly Rawn Mayor of Fayetteville 113 W. Mountain Street Fayetteville, AR 72701 Dear Mayor Rawn: The Grant Offer for Infrastructure Investment and Jobs Act(IIJA)Project No. 3-05-0020-057-2026 at Drake Field Airport is attached for execution.This letter outlines the steps you must take to properly enter into this agreement and provides other useful information. Please read the conditions, special conditions, and assurances that comprise the Grant Offer carefully. You may not make any modification to the text,terms or conditions of the Grant Offer. Steps You Must Take to Enter Into Agreement. To properly enter into this agreement,you must do the following: 1. The governing body must give authority to execute the grant to the individual(s)signing the grant, i.e., the person signing the document must be the sponsor's authorized representative(s) (hereinafter"authorized representative"). 2. The authorized representative must execute the grant by adding their electronic signature to the appropriate certificate at the end of the agreement. 3. Once the authorized representative has electronically signed the grant, the sponsor's attorney(s) will automatically receive an email notification. 4. On the same day or after the authorized representative has signed the grant, the sponsor's attorney(s) will add their electronic signature to the appropriate certificate at the end of the agreement. 5. If there are co-sponsors, the authorized representative(s) and sponsor's attorney(s) must follow the above procedures to fully execute the grant and finalize the process. Signatures must be obtained and finalized no later than September 11, 2026. 6. The fully executed grant will then be automatically sent to all parties as an email attachment. Payment. Subject to the requirements in 2 CFR § 200.305 (federal payment), each payment request for reimbursement under this grant must be made electronically via the Delphi elnvoicing System. Please see the attached Grant Agreement for more information regarding the use of this system. Project Timing. The terms and conditions of this agreement require you to complete the project without undue delay and no later than the Period of Performance end date four(4)years from the grant 1 3-05-0020-057-2026 execution date). We will be monitoring your progress to ensure proper stewardship of these federal funds. We expect you to submit payment requests for reimbursement of allowable incurred project expenses consistent with project progress.Your grant may be placed in "inactive" status if you do not make draws on a regular basis, which will affect your ability to receive future Grant Offers. Costs incurred after the Period of Performance ends are generally not allowable and will be rejected unless authorized by the FAA in advance. Reporting. Until the grant is completed and closed, you are responsible for submitting formal reports as follows: ➢ For all grants, you must submit by December 31ST of each year this grant is open: 1. A signed/dated SF-270(Request for Advance or Reimbursement for non-construction projects)or SF-271 or equivalent(Outlay Report and Request for Reimbursement for Construction Programs), and 2. An SF-425 (Federal Financial Report). ➢ For non-construction projects,you must submit FAA Form 5100-140, Performance Report within 30 days of the end of the federal fiscal year. ➢ For construction projects, you must submit FAA Form 5370-1, Construction Progress and Inspection Report, within 30 days of the end of each federal fiscal quarter. Audit Requirements. As a condition of receiving federal assistance under this award, you must comply with audit requirements as established under 2 CFR Part 200. Subpart F requires non-federal entities that expend $1,000,000 or more in federal awards to conduct a single or program specific audit for that year. Note that this includes federal expenditures made under other federal-assistance programs. Please take appropriate and necessary action to ensure your organization will comply with applicable audit requirements and standards. Closeout. Once the project(s) is completed and all costs are determined, we ask that you work with your FAA contact indicated below to close the project without delay and submit the necessary final closeout documentation as required by your Region/Airports District Office. FAA Contact Information. Kathy Franklin, (817) 222-5697, katherine.franklin@faa.govistheassigned program manager for this grant and is readily available to assist you and your designated representative with the requirements stated herein. We sincerely value your cooperation in these efforts and look forward to working with you to complete this important project. Sincerely, 0 0 Of,E19 4 CD Olufemi Adeoye(08/06/2026 09 19 4 CDT Femi Adeoye, P.E, CFM, PMP Manager(A) Arkansas/Oklahoma Airports District Office 2 3-05-0020-057-2026 O U.S. Department of Transportation Federal Aviation Administration FEDERAL AVIATION ADMINISTRATION FY 2026 AIRPORT INFRASTRUCTURE GRANT(AIG)GRANT AGREEMENT Part I -Offer Federal Award Offer Date August 6, 2026 Airport/Planning Area Drake Field Airport Airport Grant Number 3-05-0020-057-2026 Unique Entity Identifier FKCQRMDULFH9 TO: City of Fayetteville (herein called the "Sponsor") (For Co-Sponsors, list all Co-Sponsor names.The word "Sponsor" in this Grant Agreement also applies to a Co-Sponsor.) FROM: The United States of America (acting through the Federal Aviation Administration, herein called the "FAA") WHEREAS, the sponsor has submitted to the FAA a Project Application dated July 20, 2026, for a grant of federal funds for a project at or associated with the Drake Field Airport, which is included as part of this Grant Agreement; and WHEREAS, the FAA has approved a project for the Drake Field Airport(herein called the "Project") consisting of the following: Acquire Aircraft Rescue and Fire Fighting Vehicle which is more fully described in the Project Application. 1 3-05-0020-057-2026 NOW THEREFORE, Pursuant to and for the purpose of carrying out Title 49, United States Code (USC), Chapters 471 and 475;49 USC§§40101 et seq. and 48103; Consolidated Appropriations Act, 2024 (Public Law Number(P.L.) 118-42); Consolidated Appropriations Act, 2025 (P.L. 119-4); Consolidated Appropriations Act, 2026 (P.L. 119-75); FAA Reauthorization Act of 2024 (P.L. 118-63); Infrastructure Investment and Jobs Act of 2021 (IIJA) (P.L. 117-58) (as applicable); and the representations contained in the Project Application; and in consideration of: (a)the sponsor's adoption and ratification of the most recently published Grant Assurances; (b)the sponsor's acceptance of this offer;and (c) the benefits to accrue to the United States and the public from the accomplishment of the project, and compliance with the Grant Assurance and conditions as herein provided; THE FEDERAL AVIATION ADMINISTRATION, FOR AND ON BEHALF OF THE UNITED STATES, HEREBY OFFERS AND AGREES to pay(95)%of the allowable costs incurred accomplishing the Project as the United States'share of the Project. Assistance Listings Number(s): 20.117. This Offer is made on and SUBJECT TO THE FOLLOWING TERMS AND CONDITIONS: CONDITIONS 1. Maximum Obligation.The maximum obligation of the United States payable under this Offer is $1,100,197. The following amounts represent a breakdown of the maximum obligation for the purpose of establishing allowable amounts for any future grant amendment, which may increase the foregoing maximum obligation of the United States under the provisions of 49 USC§47108(b): $1,100,197 for airport development 2. Grant Performance.This agreement is subject to the following federal award requirements: a. Period of Performance: i. Start Date:The date the recipient formally accepts this agreement and the date signed by the last signatory to the agreement. ii. End Date: Four(4)years to the calendar day from the date of acceptance. iii. Extension of the Period of Performance (PoP): The recipient may request a one-time extension of up to one year after the PoP end date by submitting a request to the FAA.The request must include, at a minimum, supporting justification for the request and the amount of additional time requested.The request must be submitted at least 10 calendar days before the PoP end date.This one-time extension may not be exercised for the sole purpose of using unobligated balances. The PoP end date, or any extension as approved by FAA, shall not affect, relieve, or reduce recipient obligations and assurances that extend beyond the closeout of this agreement. b. Budget Period: i. For a single year grant offer, the budget period follows the same start and end date as the PoP provided in paragraph 2(a), and any extension of the PoP end date. ii. For a multi-year grant offer, per the authority provided in 49 USC §47108 and §47114, the budget period is from the initial PoP start date through the end of the final fiscal year identified on a multi-year grant offer(See Multi-Year Grant Special Condition, if applicable). 2 3-05-0020-057-2026 c. Appropriation Period of Availability and Expenditure: i. The FAA must obligate appropriated funds within the period of availability identified in the appropriation. ii. In accordance with 31 USC§ 1552, by September 30th of the fifth fiscal year after the period of availability, FAA must liquidate and close expired appropriations, and any remaining balance (whether obligated or unobligated) must be canceled and thereafter shall not be available for obligation or expenditure for any purpose. iii. IIJA and Supplemental AIP funding are subject to this condition. d. Close Out: Recipients shall begin the closeout process upon physical completion of the project(s) identified in this agreement. Closeout shall proceed expeditiously and without delay, even if the PoP end date has not been reached. In accordance with 2 Code of Federal Regulations (CFR) 200, unless the FAA authorizes a written extension,the recipient must submit all grant closeout documentation and liquidate (pay-off) all obligations incurred under this award no later than 120 calendar days after the PoP end date. If the recipient does not submit all required closeout documentation within this period, the FAA will proceed to close out the grant within one year of the PoP end date with the information available at the end of 120 days. e. Termination: The FAA may terminate this agreement and all of its obligations under this agreement if any of the following occur: i. The recipient fails to comply with the terms and conditions of this agreement; ii. The recipient fails to obtain or provide any recipient grant contribution as required by the agreement; iii. There is a material failure to comply with the Project Schedule even if it is beyond the reasonable control of the recipient; iv. Any project changes that the FAA determines are inconsistent with the FAA's basis for selecting the project to receive a grant; v. Continued grant payment inactivity,generally defined as no drawdowns over a 12-month period; vi. The recipient requests that the FAA terminate the agreement under this section; or vii. The FAA determines that termination of this agreement is in the public interest. In terminating this agreement under this section,the FAA may elect to consider only the interests of the FAA. 3. Ineligible or Unallowable Costs. In accordance with 49 USC §47110, the sponsor is prohibited from including any costs in the grant funded portions of the project that the FAA has determined to be ineligible or unallowable, including costs incurred to carry out airport development implementing policies and initiatives repealed by Executive Order 14148, provided such costs are not otherwise permitted by statute. 3 3-05-0020-057-2026 4. Indirect Costs-Sponsor.The sponsor may charge indirect costs under this award by applying the indirect cost rate identified in the project application, as accepted by the FAA,to allowable costs for sponsor direct salaries and wages. 5. Determining the Final Federal Share of Costs.The United States' share of allowable project costs will be made in accordance with 49 USC§47109,the regulations, policies, and procedures of the Secretary of Transportation ("Secretary"), and any superseding legislation. Final determination of the United States' share will be based upon the final audit of the total amount of allowable project costs, and settlement will be made for any upward or downward adjustments to the federal share of costs. 6. Completing the Project Without Delay and in Conformance with Requirements.The sponsor must carry out and complete the project without undue delay, and in accordance with this agreement, 49 USC Chapters 471 and 475, IIJA(P.L. 117-58) (as appropriate), and the regulations, policies, and procedures of the Secretary. Per 2 CFR§ 200.308, the sponsor agrees to report and request prior FAA approval for any disengagement from performing the project that exceeds three months, or a 25 percent reduction in time devoted to the project.The report must include a reason for the project stoppage.The sponsor also agrees to comply with the grant assurances,which are part of this agreement. 7. Amendments or Withdrawals before Grant Acceptance.The FAA reserves the right to amend or withdraw this offer at any time prior to its acceptance by the sponsor. 8. Offer Expiration Date.This offer will expire and the United States will not be obligated to pay any part of the costs of the project(s) unless this offer has been accepted by the sponsor on or before September 11, 2026, or such subsequent date as may be prescribed in writing by the FAA. 9. Improper Use of Federal Funds and Mandatory Disclosure. a. The sponsor must take all steps, including litigation, if necessary, to recover federal funds spent fraudulently, wastefully, or in violation of federal antitrust statutes, or misused in any other manner for any project upon which federal funds have been expended. For the purposes of this grant agreement, the term "federal funds" means funds however used or dispersed by the sponsor, that were originally paid pursuant to this or any other federal grant agreement.The sponsor must obtain the approval of the Secretary as to any determination of the amount of the federal share of such funds.The sponsor must return the recovered federal share, including funds recovered by settlement, order, or judgment,to the Secretary. Upon request, the sponsor must furnish to the Secretary all documents and records pertaining to the determination of the amount of the federal share, or to any settlement, litigation, negotiation, or other efforts taken to recover such funds.All settlements or other final positions of the sponsor, in court or otherwise, involving the recovery of such federal share require advance approval by the Secretary. b. The sponsor, a recipient, and a subrecipient under this federal grant must promptly comply with the mandatory disclosure requirements as established under 2 CFR §200.113, including reporting requirements related to recipient integrity and performance in accordance with Appendix XII to 2 CFR Part 200. 10. United States Not Liable for Damage or Injury.The United States is not responsible or liable for damage to property or injury to persons which may arise from, or be incident to, compliance with this agreement. 4 3-05-0020-057-2026 11. System for Award Management(SAM) Registration and Unique Entity Identifier(UEI). a. Requirement for System for Award Management (SAM): Unless the sponsor is exempted from this requirement under 2 CFR§25.110, the sponsor must maintain the currency of its information in the SAM until the sponsor submits the final financial report required under this grant, or receives the final payment,whichever is later. This requires that the sponsor review and update the information at least annually after the initial registration and more frequently if required by changes in information or another award term.Additional information about registration procedures may be found at the SAM website (currently at http://www.sam.gov). b. Unique entity identifier(UEI) means a 12-character alpha-numeric value used to identify a specific commercial, nonprofit, or governmental entity.A UEI may be obtained from SAM.gov at https://sam.gov/content/entity-registration. 12. Electronic Grant Payment(s). Unless otherwise directed by the FAA, the sponsor must make each payment request under this agreement electronically via the Delphi elnvoicing System for Department of Transportation (DOT) Financial Assistance Awardees. 13. Informal Letter Amendment of Projects. If, during the life of the project, the FAA determines that the maximum grant obligation of the United States exceeds the expected needs of the sponsor by $25,000 or five percent, whichever is greater,the FAA can issue a letter amendment to the sponsor unilaterally reducing the maximum obligation. The FAA can also issue a letter to the sponsor increasing the maximum obligation if there is an overrun in the total actual eligible and allowable project costs to cover the amount of the overrun, provided it will not exceed the statutory limitations for grant amendments.The FAA's authority to increase the maximum obligation does not apply to the "planning" component of Condition No. 1, Maximum Obligation. The FAA can also issue an informal letter amendment that modifies the grant description to correct administrative errors or to delete work items if the FAA finds it advantageous, and in the best interests of the United States. An informal letter amendment has the same force and effect as a formal grant amendment. 14. Environmental Standards.The sponsor is required to comply with all applicable environmental standards, as further defined in the Grant Assurances,for all projects in this grant. If the sponsor fails to comply with this requirement, the FAA may suspend, cancel, or terminate this Grant Agreement. 15. Financial Reporting and Payment Requirements.The sponsor will comply with all federal financial reporting requirements and payment requirements, including submittal of timely and accurate reports. 16. Buy American. Unless otherwise approved in advance by the FAA, in accordance with 49 USC § 50101, the sponsor will not acquire or permit any contractor or subcontractor to acquire any steel or manufactured goods produced outside the United States to be used for any project for which funds are provided under this grant.The sponsor will include a provision implementing Buy American in every contract and subcontract awarded under this grant. 17. Build America, Buy America. The sponsor must comply with the requirements under the Build America, Buy America Act (P.L. 117-58). 5 3-05-0020-057-2026 18. Maximum Obligation Increase. In accordance with 49 USC §47108(b)(2), as amended, the maximum obligation of the United States, as stated in Condition No. 1, Maximum Obligation, of this grant: a. May not be increased for a planning project; b. May be increased by not more than 15 percent for development projects, if funds are available; c. May be increased by not more than the greater of the following for a land project, if funds are available: i. 15 percent; or ii. 25 percent of the total increase in allowable project costs attributable to acquiring an interest in the land. If the sponsor requests an increase, any eligible increase in funding will be subject to the United States Government share as provided in 49 USC§47109, or IIJA(P.L. 17-58), or other superseding legislation if applicable, for the fiscal year appropriation with which the increase is funded. The FAA is not responsible for the same federal share provided herein for any amount increased over the initial grant amount.The FAA may adjust the federal share as applicable through an informal letter of amendment. 19. Audits for Sponsors. PUBLIC SPONSORS.The sponsor must provide for a Single Audit or program-specific audit in accordance with 2 CFR Part 200. The sponsor must submit the audit reporting package to the Federal Audit Clearinghouse on the Federal Audit Clearinghouse's Internet Data Entry System at http://harvester.census.gov/facweb/. Upon request of the FAA,the sponsor shall provide one copy of the completed audit to the FAA. Sponsors that expend less than $1,000,000 in federal awards and are exempt from federal audit requirements must make records available for review or audit by the appropriate federal agency officials, state, and Government Accountability Office.The FAA and other appropriate federal agencies may request additional information to meet all federal audit requirements. 20. Suspension or Debarment. When entering into a "covered transaction" as defined by 2 CFR § 180.200, the sponsor must: a. Verify the non-federal entity is eligible to participate in this federal program by: i. Checking the System for Award Management (SAM.gov) exclusions to determine if the non- federal entity is excluded or disqualified; or ii. Collecting a certification statement from the non-federal entity attesting they are not excluded or disqualified from participating; or iii. Adding a clause or condition to covered transactions attesting the individual or firm are not excluded or disqualified from participating. b. Require prime contractors to comply with 2 CFR§ 180.330 when entering into lower-tier transactions with their contractors and sub-contractors. c. Immediately disclose in writing to the FAA whenever(1)the sponsor learns they have entered into a covered transaction with an ineligible entity or(2) the public sponsor suspends or debars a contractor, person, or entity. 6 3-05-0020-057-2026 21. Ban on Texting While Driving. a. In accordance with Executive Order 13513, Federal Leadership on Reducing Text Messaging While Driving, October 1, 2009, and DOT Order 3902.10,Text Messaging While Driving, December 30, 2009, the sponsor is encouraged to: i. Adopt and enforce workplace safety policies to decrease crashes caused by distracted drivers, including policies to ban text messaging while driving when performing any work for, or on behalf of, the Federal Government, including work relating to a grant or subgrant. ii. Conduct workplace safety initiatives in a manner commensurate with the size of the business, such as: a) Establishment of new rules and programs or re-evaluation of existing programs to prohibit text messaging while driving; and b) Education, awareness, and other outreach to employees about the safety risks associated with texting while driving. f. The sponsor must insert the substance of this clause on banning texting while driving in all subgrants, contracts, and subcontracts funded with this grant. 22. Trafficking in Persons. a. Posting of contact information. i. The sponsor must post the contact information of the national human trafficking hotline (including options to reach out to the hotline such as through phone, text, or TTY) in all public airport restrooms. b. Provisions applicable to a sponsor that is a private entity. i. Under this grant,the sponsor, its employees, subrecipients under this grant, and subrecipient's employees must not engage in: a) Severe forms of trafficking in persons; b) The procurement of a commercial sex act during the period of time that the grant or cooperative agreement is in effect; c) The use of forced labor in the performance of this grant; or any subaward; or d) Acts that directly support or advance trafficking in persons, including the following acts: 1. Destroying, concealing, removing, confiscating, or otherwise denying an employee access to that employee's identity or immigration documents; 2. Failing to provide return transportation of pay for return transportation costs to an employee from a country outside the United States to the country from which the employee was recruited upon the end of employment if requested by the employee, unless: a. Exempted from the requirement to provide or pay for such return transportation by the federal department or agency providing or entering into the grant; or 7 3-05-0020-057-2026 b. The employee is a victim of human trafficking seeking victim services or legal redress in the country of employment or witness in a human trafficking enforcement action; 3. Soliciting a person for the purpose of employment, or offering employment, by means of materially false or fraudulent pretenses, representations, or promises regarding that employment; 4. Charging recruited employees a placement or recruitment fee; or 5. Providing or arranging housing that fails to meet the host country's housing and safety standards. ii. The FAA may unilaterally terminate this grant or take any remedial actions authorized by 22 USC§ 7104b(c), without penalty, if any private entity under this grant: a) is determined to have violated a prohibition in paragraph 2.a. (PoP) of this grant; or b) has an employee that is determined to have violated a prohibition in paragraph 2.a. (PoP) of this grant through conduct that is either: 1. Associated with the performance under this grant; or 2. Imputed to the recipient or the subrecipient using the standards and due process for imputing the conduct of an individual to an organization that are provided in 2 CFR Part 180, "OMB Guidelines to Agencies on Government- wide Debarment and Suspension (Nonprocurement)," as implemented by the FAA at 2 CFR Part 1200. c. Provisions applicable to a sponsor other than a private entity. i. The FAA may unilaterally terminate this award or take any remedial actions authorized by 22 USC§ 7104b(c), without penalty, if subrecipient is a private entity under this grant: a) is determined to have violated a prohibition in paragraph 2.a. (PoP) of this grant or b) has an employee that is determined to have violated a prohibition in paragraph 2.a. (PoP) of this grant through conduct that is either: 1. Associated with the performance under this grant; or 2. Imputed to the sponsor or subrecipient using the standards and due process for imputing the conduct of an individual to an organization that are provided in 2 CFR Part 180, "OMB Guidelines to Agencies on Government- wide Debarment and Suspension (Nonprocurement)," as implemented by the FAA at 2 CFR Part 1200. d. Provisions applicable to any sponsor or subrecipient. i. The sponsor or subrecipient must inform the FAA and the DOT Inspector General immediately of any information you receive from any source alleging a violation of a prohibition in paragraph 2.a. (PoP) of this grant. ii. The FAA's right to unilaterally terminate this grant as described in paragraphs 2.b. (Budget Period) or 3.a. (Close Out and Termination) of this grant, implements the requirements of 22 USC Chapter 78, and is in addition to all other remedies for noncompliance that are available to the FAA under this grant. 8 3-05-0020-057-2026 iii. The sponsor must include the requirements of paragraph 2.a. (PoP)of this grant award term in any subaward it makes to a private entity. iv. If applicable, the sponsor must also comply with the compliance plan and certification requirements in 2 CFR § 175.105(b). e. Definitions. For purposes of this grant award, term: i. "Employee" means either: a) An individual employed by the sponsor or a subrecipient who is engaged in the performance of the project or program under this grant; or b) Another person engaged in the performance of the project or program under this grant and not compensated by the sponsor or a subrecipient including, but not limited to, a volunteer or individual whose services are contributed by a third party as an in-kind contribution toward cost sharing requirements. ii. "Private Entity" means: a) Any entity, including for-profit organizations, nonprofit organizations, institutions of higher education, and hospitals. The term does not include foreign public entities, Indian Tribes, local governments, or states as defined in 2 CFR § 200.1. b) The terms "severe forms of trafficking in persons," "commercial sex act," "sex trafficking," "abuse or threatened abuse of law or legal process," "coercion," "debt bondage," and "involuntary servitude" have the meanings given at section 103 of the Victims of Trafficking and Violence Protection Act of 2000, as amended (22 USC § 7102). 23. Grant Funded Work Included in a PFC Application. Within 120 days of acceptance of this Grant Agreement,the sponsor must submit to the FAA an amendment to any approved Passenger Facility Charge (PFC) application that contains an approved PFC project also covered under this Grant Agreement as described in the project application.The sponsor may not make any expenditure under this Grant Agreement until project work addressed under this Grant Agreement is removed from an approved PFC application by amendment. 24. Exhibit"A" Property Map.The Exhibit "A" Property Map dated July 01, 2011, is incorporated herein by reference, or is submitted with the project application and made part of this Grant Agreement. 25. Employee Protection from Reprisal. In accordance with 2 CFR§ 200.217 and 41 USC§4701, an employee of a grantee, subgrantee contractor, recipient, or subrecipient must not be discharged, demoted, or otherwise discriminated against as a reprisal for disclosing to a person or body described in 41 USC§4712(a)(2) information that the employee reasonably believes is evidence of gross mismanagement of a federal contract or grant, a gross waste of federal funds, an abuse of authority relating to a federal contract or grant, a substantial and specific danger to public health or safety, or a violation of law, rule, or regulation related to a federal contract (including the competition for or negotiation of a contract) or grant. The grantee, subgrantee, contractor, recipient, or subrecipient must inform their employees in writing of employee whistleblower rights and protections under 41 USC §4712. See statutory requirements for whistleblower protections at 10 USC §4701,41 USC§4712, 41 USC§4304, and 10 USC§4310. 26. Prohibited Telecommunications and Video Surveillance Services and Equipment.The sponsor agrees to comply with mandatory standards and policies relating to use and procurement of certain telecommunications and video surveillance services or equipment in compliance with the National Defense Authorization Act [P.L. 115-232 §889] and 2 CFR § 200.216. 9 3-05-0020-057-2026 27. Critical Infrastructure Security and Resilience.The sponsor acknowledges that it has considered and addressed physical and cybersecurity and resilience in its project planning, design, and oversight, as determined by the DOT and the Department of Homeland Security(DHS). For airports that do not have specific DOT or DHS cybersecurity requirements,the FAA encourages the voluntary adoption of the cybersecurity requirements from the Transportation Security Administration and Federal Security Director identified for security risk Category X airports. 28. Title VI of the Civil Rights Act. As a condition of a grant award,the sponsor shall demonstrate that it complies with the provisions of Title VI of the Civil Rights Act of 1964 (42 USC§§2000d et seq.) and implementing regulations(49 CFR Part 21), the Airport and Airway Improvement Act of 1982 (49 USC§47123), the Age Discrimination Act of 1975 (42 USC § 6101 et seq.), Section 504 of the Rehabilitation Act of 1973 (29 USC§ 794 et seq.), the Americans with Disabilities Act of 1990 (42 USC§ 12101, et seq.), U.S. Department of Transportation and Federal Aviation Administration (FAA) Assurances, and other relevant civil rights statutes, regulations, or authorities, including any amendments or updates thereto. This may include, as applicable, providing a current Title VI Program Plan to the FAA for approval, in the format and according to the timeline required by the FAA, and other information about the communities that will be benefited and impacted by the project. The sponsor shall affirmatively ensure that when carrying out any project supported by this grant that it complies with all federal nondiscrimination and civil rights laws based on race, color, national origin, sex, creed, age, disability, and genetic information, in consideration for federal financial assistance. The Department's and FAA's Office of Civil Rights may provide resources and technical assistance to recipients to ensure full and sustainable compliance with federal civil rights requirements. Failure to comply with civil rights requirements will be considered a violation of the agreement or contract and be subject to any enforcement action as authorized by law. 29. Applicable Federal Anti-Discrimination Laws.The sponsor agrees: a. That its compliance in all respects with all applicable federal anti-discrimination laws is material to the government's payment decisions for purposes of 31 USC§ 3729(b)(4) and b. To certify that it does not operate any programs promoting Diversity, Equity, and Inclusion (DEI) that violate any applicable federal anti-discrimination laws. 30. National Airspace System Requirements. a. The sponsor shall cooperate with FAA activities installing, maintaining, replacing, improving, or operating equipment and facilities in or supporting the National Airspace System, including waiving permitting requirements and other restrictions affecting those activities to the maximum extent possible, and assisting the FAA in securing waivers of permitting or other restrictions from other authorities.The sponsor shall not take actions that frustrate or prevent the FAA from installing, maintaining, replacing, improving, or operating equipment and facilities in or supporting the National Airspace System. b. If FAA determines that the sponsor has violated subsection a.,the FAA may impose a remedy, including: i. Additional conditions on the award; ii. Consistent with 49 USC Chapter 471, any remedy permitted under 2 CFR §§ 200.339- 200.340, including withholding of payments; disallowance of previously reimbursed costs, requiring refunds from the recipient to the DOT; suspension or termination of the award; or suspension and debarment under 2 CFR part 180; or iii. Any other remedy legally available. 10 3-05-0020-057-2026 c. In imposing a remedy under this condition,the FAA may elect to consider the interests of only the FAA. d. The sponsor acknowledges that amounts that the FAA requires the sponsor to refund to the FAA due to a remedy under this condition constitute a debt to the Federal Government that the FAA may collect under 2 CFR 200.346 and the Federal Claims Collection Standards(31 CFR Parts 900- 904). 31. Signage Costs for Construction Projects.The sponsor agrees that it will require the prime contractor of a federally-assisted airport improvement project to post signs consistent with a DOT/FAA- prescribed format, as may be requested by the DOT/FAA, and further agrees to remove any signs posted in response to requests received prior to February 1, 2025. 11 3-05-0020-057-2026 SPECIAL CONDITIONS 32. Equipment Acquisition. The sponsor understands and agrees that any equipment acquired through this grant is considered a facility as that term is used in the Grant Assurances. Further, the equipment must be only operated by the sponsor.The sponsor agrees that it will maintain the equipment and use it exclusively at the airport for airport purposes. 33. Acquiring ARFF Vehicle in Excess of Minimum Standards.This grant is based in part on mitigating site-specific risks and protecting passengers based on current or reasonably forecast aeronautical activity levels.The certificate holder (sponsor)will have and maintain a sufficient number of adequately trained personnel and sufficient financial resources to operate and maintain the associated equipment for its intended, on-airport purpose. This grant does not set a precedent for future FAA support of similar equipment, particularly if aeronautical activity levels change. 12 3-05-0020-057-2026 The sponsor's acceptance of this offer and ratification and adoption of the Project Application incorporated herein shall be evidenced by execution of this instrument by the sponsor, as hereinafter provided, and this offer and acceptance shall comprise a Grant Agreement, constituting the contractual obligations and rights of the United States and the sponsor with respect to the accomplishment of the project and compliance with the Grant Assurances, terms, and conditions as provided herein. Such Grant Agreement shall become effective upon the sponsor's acceptance of this offer. Please read the following information: By signing this document,you are agreeing that you have reviewed the following consumer disclosure information and consent to transact business using electronic communications,to receive notices and disclosures electronically, and to utilize electronic signatures in lieu of using paper documents.You are not required to receive notices and disclosures or sign documents electronically. If you prefer not to do so,you may request to receive paper copies and withdraw your consent at any time. I declare under penalty of perjury that the foregoing is true and correct.1 UNITED STATES OF AMERICA FEDERAL AVIATION ADMINISTRATION 011/GOlufemi Adeoye(08/06/2026 09.19 4 CDT) (Signature) Olufemi 0 Adeoye (Typed Name) Manager (A) (Title of FAA Official) 1 Knowingly and willfully providing false information to the Federal government is a violation of 18 U.S.C. § 1001 (False Statements) and could subject you to fines, imprisonment, or both. 13 3-05-0020-057-2026 Part II -Acceptance The sponsor does hereby ratify and adopt all assurances, statements, representations, warranties, covenants, and agreements contained in the Project Application and incorporated materials referred to in the foregoing offer, and does hereby accept this offer and by such acceptance agrees to comply with all of the Grant Assurances,terms, and conditions in this offer and in the Project Application. Please read the following information: By signing this document,you are agreeing that you have reviewed the following consumer disclosure information and consent to transact business using electronic communications, to receive notices and disclosures electronically, and to utilize electronic signatures in lieu of using paper documents. You are not required to receive notices and disclosures or sign documents electronically. If you prefer not to do so,you may request to receive paper copies and withdraw your consent at any time. I declare under penalty of perjury that the foregoing is true and correct.' Dated September 3, 2026 City of Fayetteville (Name of Sponsor) ,Nfliodqva Molly Ra (09/03/2026 12:30:58 CDT) (Signature of Sponsor's Authorized Official) By: Molly Rawn (Typed Name of Sponsor's Authorized Official) Title: Mayor of Fayetteville (Title of Sponsor's Authorized Official) ' Knowingly and willfully providing false information to the Federal Government is a violation of 18 USC § 1001 (False Statements)and could subject you to fines, imprisonment, or both. 14 3-05-0020-057-2026 CERTIFICATE OF SPONSOR'S ATTORNEY I, Kit Williams , acting as Attorney for the Sponsor do hereby certify: That in my opinion the Sponsor is empowered to enter into the foregoing Grant Agreement under the laws of the State of Arkansas . Further, I have examined the foregoing Grant Agreement and the actions taken by said Sponsor and Sponsor's official representative, who has been duly authorized to execute this Grant Agreement, which is in all respects due and proper and in accordance with the laws of the said State; and Title 49, United States Code (USC), Chapters 471 and 475;49 USC§§40101 et seq., and 48103; Consolidated Appropriations Act, 2024(P.L. 118-42); Consolidated Appropriations Act, 2025 (P.L. 119-4); Consolidated Appropriations Act, 2026 (P.L. 119-75); FAA Reauthorization Act of 2024 (P.L. 118-63); and the representations contained in the Project Application. In addition, for grants involving projects to be carried out on property not owned by the Sponsor, there are no legal impediments that will prevent full performance by the Sponsor. Further, it is my opinion that the said Grant Agreement constitutes a legal and binding obligation of the Sponsor in accordance with the terms thereof. Please read the following information: By signing this document,you are agreeing that you have reviewed the following consumer disclosure information and consent to transact business using electronic communications, to receive notices and disclosures electronically, and to utilize electronic signatures in lieu of using paper documents. You are not required to receive notices and disclosures or sign documents electronically. If you prefer not to do so,you may request to receive paper copies and withdraw your consent at any time. I declare under penalty of perjury that the foregoing is true and correct.' Dated at September 3, 2026 Kit V�111 61.) t&a. i.� By. 03 2026 13 49 22 CDTi (Signature of Sponsor's Attorney) 3 Knowingly and willfully providing false information to the Federal Government is a violation of 18 USC § 1001 (False Statements) and could subject you to fines, imprisonment, or both. 15 3-05-0020-057-2026 ASSURANCES AIRPORT SPONSORS A. General. 1. These assurances shall be complied with in the performance of grant agreements for airport development, airport planning, and noise compatibility program grants for airport sponsors. 2. These assurances are required to be submitted as part of the project application by sponsors requesting funds under the provisions of Title 49, USC, subtitle VII, as amended. As used herein, the term "public agency sponsor" means a public agency with control of a public-use airport; the term "private sponsor" means a private owner of a public-use airport; and the term "sponsor" includes both public agency sponsors and private sponsors. 3. Upon acceptance of this Grant Offer by the sponsor,these assurances are incorporated in and become part of this Grant Agreement. B. Duration and Applicability. 1. Airport Development or Noise Compatibility Program Projects Undertaken by a Public Agency Sponsor. The terms, conditions and assurances of this Grant Agreement shall remain in full force and effect throughout the useful life of the facilities developed or equipment acquired for an airport development or noise compatibility program project, or throughout the useful life of the project items installed within a facility under a noise compatibility program project, but in any event not to exceed twenty (20)years from the date of acceptance of a Grant Offer of federal funds for the project. However,there shall be no limit on the duration of the assurances regarding Exclusive Rights and Airport Revenue so long as the airport is used as an airport. There shall be no limit on the duration of the terms, conditions, and assurances with respect to real property acquired with federal funds. Furthermore, the duration of the Civil Rights assurance shall be specified in the assurances. 2. Airport Development or Noise Compatibility Projects Undertaken by a Private Sponsor. The preceding paragraph (1) also applies to a private sponsor except that the useful life of project items installed within a facility or the useful life of the facilities developed or equipment acquired under an airport development or noise compatibility program project shall be no less than ten (10) years from the date of acceptance of federal aid for the project. 3. Airport Planning Undertaken by a Sponsor. Unless otherwise specified in this Grant Agreement, only Assurances 1, 2, 3, 5, 6, 13, 18, 23, 25, 30, 32, 33, 34, 37, and 40 in Section C apply to planning projects.The terms, conditions, and assurances of this Grant Agreement shall remain in full force and effect during the life of the project;there shall be no limit on the duration of the assurances regarding Exclusive Rights and Airport Revenue so long as the airport is used as an airport. Airport Sponsors Assurances Page 1 of 19 3-05-0020-057-2026 C. Sponsor Certification. The sponsor hereby assures and certifies,with respect to this grant that: 1. General Federal Requirements It will comply with all applicable federal laws, regulations, executive orders, policies, guidelines, and requirements as they relate to the application, acceptance, and use of federal funds for this grant. Performance under this agreement shall be governed by and in compliance with the following requirements, as applicable, to the type of organization of the Sponsor and any applicable sub-recipients.The applicable provisions to this agreement include, but are not limited to, the following: FEDERAL LEGISLATION a. 49 USC subtitle VII, as amended. b. Davis-Bacon Act, as amended —40 USC§§3141-3144, 3146, and 3147, et seq.' c. Federal Fair Labor Standards Act—29 USC§201, et seq. d. Hatch Act—5 USC§ 1501, et seq.2 e. Uniform Relocation Assistance and Real Property Acquisition Policies Act of 1970, 42 USC §4601, et seq.1' 2 f. National Historic Preservation Act of 1966—Section 106—54 USC§ 306108.' g. Archeological and Historic Preservation Act of 1974—54 USC§312501, et seq.' h. Native Americans Grave Repatriation Act—25 USC§ 3001, et seq. i. Clean Air Act, P.L. 90-148, as amended—42 USC§ 7401, et seq. j. Coastal Zone Management Act, P.L. 92-583, as amended—16 USC§ 1451, et seq. k. Flood Disaster Protection Act of 1973—Section 102(a)-42 USC§4012a.1 I. 49 USC§303, (formerly known as Section 4(f)). m. Rehabilitation Act of 1973—29 USC§794. n. Title VI of the Civil Rights Act of 1964 (42 USC§ 2000d et seq.) (prohibits discrimination on the basis of race, color, national origin). o. Americans with Disabilities Act of 1990, as amended, (42 USC§ 12101 et seq.) (prohibits discrimination on the basis of disability). p. Age Discrimination Act of 1975—42 USC§ 6101, et seq. q. American Indian Religious Freedom Act, P.L. 95-341, as amended. r. Architectural Barriers Act of 1968, as amended—42 USC §4151, et seq.' s. Powerplant and Industrial Fuel Use Act of 1978—Section 403—42 USC§8373.' t. Contract Work Hours and Safety Standards Act-40 USC§ 3701, et seq.' u. Copeland Anti-kickback Act— 18 USC§874.1 Airport Sponsors Assurances Page 2 of 19 3-05-0020-057-2026 v. National Environmental Policy Act of 1969—42 USC§4321, et seq.' w. Wild and Scenic Rivers Act, P.L. 90-542, as amended—16 USC§ 1271, et seq. x. Single Audit Act of 1984—31 USC§ 7501,et seq.2 y. Drug-Free Workplace Act of 1988—41 USC §§8101 through 8105. z. The Federal Funding Accountability and Transparency Act of 2006, as amended (P.L. 109-282, as amended by section 6202 of P.L. 110-252). aa. Civil Rights Restoration Act of 1987, P.L. 100-259. bb. Infrastructure Investment and Jobs Act, P.L. 117-58,Title VIII. cc. Build America, Buy America Act, P.L. 117-58,Title IX. dd. Endangered Species Act— 16 USC 1531, et seq. ee. Title IX of the Education Amendments of 1972, as amended—20 USC 1681-1683 and 1685- 1687. ff. Drug Abuse Office and Treatment Act of 1972, as amended—21 USC 1101, et seq. gg. Alcohol Abuse and Alcoholism Prevention,Treatment and Rehabilitation Act of 1970, P.L. 91- 616, as amended—42 USC§4541, et seq. hh. Alcohol Abuse and Alcoholism Prevention,Treatment and Rehabilitation Act of 1970, P.L. 91- 616, as amended—42 USC§4541, et seq. ii. Appropriated Funds to Influence Certain Federal Contracting and Financial Transactions—31 USC§ 1352. EXECUTIVE ORDERS a. Executive Order 11990—Protection of Wetlands b. Executive Order 11988—Floodplain Management c. Executive Order 12372—Intergovernmental Review of Federal Programs d. Executive Order 12699—Seismic Safety of Federal and Federally Assisted New Building Construction' e. Executive Order 14005—Ensuring the Future is Made in all of America by All of America's Workers f. Executive Order 14149—Restoring Freedom of Speech and Ending Federal Censorship g. Executive Order 14151—Ending Radical and Wasteful Government DEI Programs and Preferencing h. Executive Order 14154—Unleashing American Energy i. Executive Order 14168—Defending Women from Gender Ideology Extremism and Restoring Biological Truth to the Federal Government j. Executive Order 14173—Ending Illegal Discrimination and Restoring Merit-Based Opportunity Airport Sponsors Assurances Page 3 of 19 3-05-0020-057-2026 FEDERAL REGULATIONS a. 2 CFR Part 180—OMB Guidelines to Agencies on Governmentwide Debarment and Suspension (Nonprocurement). b. 2 CFR Part 200 and 1201—Uniform Administrative Requirements, Cost Principles, and Audit Requirements for Federal Awards. 3'4'5 c. 2 CFR Part 1200—Nonprocurement Suspension and Debarment. d. 14 CFR Part 13—Investigative and Enforcement Procedures. e. 14 CFR Part 16—Rules of Practice for Federally-Assisted Airport Enforcement Proceedings. f. 14 CFR Part 150—Airport Noise Compatibility Planning. g. 28 CFR Part 35—Nondiscrimination on the Basis of Disability in State and Local Government Services. h. 28 CFR § 50.3-U.S. Department of Justice Guidelines for the Enforcement of Title VI of the Civil Rights Act of 1964. i. 29 CFR Part 1—Procedures for Predetermination of Wage Rates.' j. 29 CFR Part 3—Contractors and Subcontractors on Public Building or Public Work Financed in Whole or in Part by Loans or Grants from the United States.' k. 29 CFR Part 5—Labor Standards Provisions Applicable to Contracts Covering Federally Financed and Assisted Construction (Also Labor Standards Provisions Applicable to Nonconstruction Contracts Subject to the Contract Work Hours and Safety Standards Act).' I. 41 CFR Part 60—Office of Federal Contract Compliance Programs, Equal Employment Opportunity, Department of Labor(Federal and Federally-assisted contracting requirements).' m. 49 CFR Part 20—New Restrictions on Lobbying. n. 49 CFR Part 21—Nondiscrimination in Federally-Assisted Programs of the Department of Transportation - Effectuation of Title VI of the Civil Rights Act of 1964. o. 49 CFR Part 23—Participation by Disadvantage Business Enterprise in Airport Concessions. p. 49 CFR Part 24—Uniform Relocation Assistance and Real Property Acquisition for Federal and Federally-Assisted Programs.'' 2 q. 49 CFR Part 26—Participation by Disadvantaged Business Enterprises in Department of Transportation Financial Assistance Programs. r. 49 CFR Part 27—Nondiscrimination on the Basis of Disability in Programs or Activities Receiving Federal Financial Assistance.' s. 49 CFR Part 28—Enforcement of Nondiscrimination on the Basis of Handicap in Programs or Activities Conducted by the Department of Transportation. t. 49 CFR Part 30—Denial of Public Works Contracts to Suppliers of Goods and Services of Countries That Deny Procurement Market Access to U.S. Contractors. u. 49 CFR Part 32—Governmentwide Requirements for Drug-Free Workplace (Financial Assistance). Airport Sponsors Assurances Page 4 of 19 3-05-0020-057-2026 v. 49 CFR Part 37—Transportation Services for Individuals with Disabilities (ADA). w. 49 CFR Part 38—Americans with Disabilities Act(ADA)Accessibility Specifications for Transportation Vehicles. x. 49 CFR Part 41—Seismic Safety. FOOTNOTES TO ASSURANCE(C)(1) 1 These laws do not apply to airport planning sponsors. 2 These laws do not apply to private sponsors. 3 2 CFR Part 200 contains requirements for state and local governments receiving federal assistance. Any requirement levied upon state and local governments by this regulation shall apply where applicable to private sponsors receiving federal assistance under Title 49, United States Code. 4 Cost principles established in 2 CFR Part 200 subpart E must be used as guidelines for determining the eligibility of specific types of expenses. 5 Audit requirements established in 2 CFR Part 200 subpart F are the guidelines for audits. SPECIFIC ASSURANCES Specific assurances required to be included in grant agreements by any of the above laws, regulations or circulars are incorporated by reference in this Grant Agreement. 2. Responsibility and Authority of the Sponsor. a. Public Agency Sponsor: It has legal authority to apply for this grant, and to finance and carry out the proposed project; that a resolution, motion or similar action has been duly adopted or passed as an official act of the applicant's governing body authorizing the filing of the application, including all understandings and assurances contained therein, and directing and authorizing the person identified as the official representative of the applicant to act in connection with the application and to provide such additional information as may be required. b. Private Sponsor: It has legal authority to apply for this grant and to finance and carry out the proposed project and comply with all terms, conditions, and assurances of this Grant Agreement. It shall designate an official representative and shall in writing direct and authorize that person to file this application, including all understandings and assurances contained therein; to act in connection with this application; and to provide such additional information as may be required. 3. Sponsor Fund Availability. It has sufficient funds available for that portion of the project costs which are not to be paid by the United States. It has sufficient funds available to assure operation and maintenance of items funded under this Grant Agreement which it will own or control. 4. Good Title. a. It, a public agency or the Federal Government, holds good title, satisfactory to the Secretary,to the landing area of the airport or site thereof, or will give assurance satisfactory to the Secretary that good title will be acquired. Airport Sponsors Assurances Page 5 of 19