Combined_Synopsis_Solicitation_140D0426Q0468.pdf

This is a combined synopsis/solicitation for commercial products or commercial services prepared in accordance with FAR Part 12. This announcement constitutes the only solicitation. Quotes are being requested and a separate written solicitation will not be issued.

Solicitation Number 140D0426R0468 is hereby issued as a Request for Quote (RFQ) for commercial aviation services in support of the U.S. Wildland Fire Service (USWFS) for the transportation of personnel, goods, and cargo between the Contiguous U.S. (Lower 48) and Alaska, with the Contractors’ primary base of operations located in Boise, Idaho.

This requirement is being issued by the United States Department of the Interior (DOI), Interior Business Center (IBC), Acquisition Services Directorate (AQD) in accordance with Federal Acquisition Regulation (FAR) Parts 12.

This acquisition provides full and open competition, it is not set-aside for small business concerns. The solicitation incorporates provisions and clauses by reference. The full text of provisions and clauses may be accessed electronically at www.acquisition.gov.

The North American Industry Classification System (NAICS) code applicable to this requirement is 481211, Nonscheduled Chartered Passenger Air Transportation. The size standard for the applicable NAICS is 1500 employees. The product service code (PSC) code is V221 “Transportation/Travel/Relocation- Travel/Lodging/Recruitment – Passenger Air Charter.”

A list of items and quantities are provided in Section A.2, Schedule of Services and Prices.

The aircraft requirements are provided in Section A.1, Item Requirement and Section B, Technical Specifications.

A list of solicitations provisions that apply to this acquisition are provided in Section E, Offeror’s Representations and Certifications.

A list of contract clauses that apply to this acquisition are provided in Section C, Contract Terms and Conditions.

Quotes are due no later than 4:00 PM Mountain Time, June 1, 2026. Quotes shall be emailed to Stephanie Mccullough, Contracting Officer, at stephanie_mccullough@ibc.doi.gov

Questions. Questions related to this RFQ must be submitted via email to Stephanie_Mccullough@ibc.doi.gov, no later than 4:00 PM Mountain Time, May 27, 2026. All questions must be received in writing – No oral questions will be accepted. All e-mail inquiries must have “Questions – RFQ 140D0426R0468” in the subject line.

**Funds are not presently available for this effort. The Governments issuance of this RFQ is subject to the availability of funds and the Government reserves the right not to make an award.** http://www.acquisition.gov/ mailto:Stephanie_Mccullough@ibc.doi.gov

SECTION A – REQUIREMENTS AND PRICES

USWFS FW Point to Point 1 Solicitation #140D0426Q0468 Boise, Idaho

Contents

SECTION A - REQUIREMENTS AND PRICES

A1 ITEM REQUIREMENT

A2. SCHEDULE OF SERVICES AND PRICES

A2.1 ON CALL PRICING SCHEDULE FOR AIRCRAFT ADDRSSED IN SECTION A.1. DESIGNATED BASE:

BOISE, ID

A2.2 EXCLUSIVE USE PRICING SCHEDULE FOR AIRCRAFT ADDRSSED IN SECTION A.1.

DESIGNATED BASE: BOISE, ID

A3 ADDITIONAL PAY ITEMS (Time & Materials IAW FAR 52.212-4 Alt 1)

A3.1 ADDITIONAL PAY ITEMS SCHEDULE

SECTION B – TECHNICAL SPECIFICATIONS

GENERAL REQUIREMENTS

B1 Scope of Contract B2 Certification B3 Order of Precedence - Specifications B4 Contracts and Task Orders

EQUIPMENT REQUIREMENTS

B5 Condition of Equipment B6 Aircraft Equipment Requirements B7 Avionics Requirements B8 Reserved

PERSONNEL REQUIREMENTS

B9 Pilot Requirements B10 Pilot Qualifications B11 Personnel Duty Limitations B12 Flight Crewmembers Duty and Flight Limitations B13 Mechanic Requirement B14 Mechanic Qualifications B15 Mechanic Duty Limitations

OPERATIONS

B19 Pilot Authority and Responsibility B20 Flight Operations B21 Security of Aircraft and Equipment B22 Reserved B23 PPE for Ground Operations B24 Transportation of Hazardous Materials

AIRCRAFT MAINTENANCE REQUIREMENTS

B26 General - Maintenance B27 Airworthiness Directives (ADs) and Manufacturer’s Mandatory Service Bulletins (MMSBs) B28 Manuals/Records B29 Maintenance

USWFS FW Point to Point 2 Solicitation #140D0426Q0468 Boise, Idaho

B30 Maintenance Test Flight B31 Time Between Overhaul (TBO) and Life-Limited Parts B32 Weight and Balance

SECTION C – CONTRACT TERMS AND CONDITIONS

CONTRACT CLAUSES

52.252-2 Clauses Incorporated by Reference (Feb 1998) Clauses Incorporated by Reference Clauses Incorporated by Full Text

ADDENDA TO CONTRACT TERMS AND CONDITIONS

FAR 52.212-4(a) Inspection/Acceptance

Inspection Scheduling and Process Equipment Personnel Substitute Personnel, Aircraft, or Equipment Reinspection Expenses

FAR 52.219-14 Limitations on Subcontracting (Deviation Jan 2026) FAR 52.252-6 Authorized Deviations in Clauses (Nov 2020) DIAR 1452.201-70 Authorities and Delegations (Sep 2011) DIAR 1452.228-71 Aircraft and General Public Liability Insurance (Mar 1989)

GENERAL CONTRACT TERMS AND CONDITIONS

C1 Invoices - Aircraft Use Reports (AUR) C2 Electronic Invoicing and Payment Requirements – Invoice Processing Platform (IPP) (Feb 2021) C3 Contractor Personnel Security Requirements C4 Contractor Performance Assessment Reporting System (Dec 2015) C5 Post-Award Conference / Prework Meeting

CONTRACT PERIOD

C6 Contract Period C7 Exclusive Use Period C8 Extension of Exclusive Use Period

ADMINISTRATIVE MATTERS

C9 Government Representatives and POCs

C9.2 AOM Technical Inspector C9.3 The AOM Aviation Safety Manager

C10 Personnel Conduct C10.1 Replacement of Contractor Personnel C10.2 Suspension of Pilot

C11 Safety C11.1 Safety and Accident Prevention C11.2 Safety Management System (SMS)

C12 Mishaps C13 Reserved

AVAILABILITY REQUIREMENTS

C14 Availability

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C15 Schedule of Operations and Reaction Time C16 Maintenance During Availability Period C17 Unavailability and Damages

C18 MEASUREMENT AND PAYMENT

C18.1 Measurement and Payment (On Call) C19 Measurement and Payment (Exclusive Use) C19.1 Daily Availability C19.2 Flight Time C20 Mobilization/Demobilization (Applies to the beginning and the end of each Exclusive Use period) C21 Additional Pay Items (from Schedule of Items)

EXHIBITS

Exhibit 1 Unacceptable Aircraft Lap Belt and Shoulder Harness Conditions Exhibit 2 Safety Management System (SMS), Flight Time, Accident History, and FAA Violation Questionnaire (Pre-Award Ver. 6.3 – 2026) Exhibit 3 Civil Aircraft Certificate of Insurance, DD FORM 2400 Exhibit 4 Civil Aircraft Landing Permit, DD FORM 2401 Exhibit 5 Civil Aircraft Hold Harmless Agreement, DD FOrm 2402 Exhibit 6 Unavailability Conversion Chart Exhibit 7 Aircraft Questionnaire Exhibit 8 Aircraft Information Form

SECTION D – INSTRUCTIONS TO OFFERORS

D1 General Information D2 North American Industry Classification System (NAICS) and Small Business Size Standard D3 Offers D4 Offer Contents

Volume I Offer Volume II Technical Capability Volume III Organizational Safety Volume IV Past Performance

D5 Special Notice to Offerors D6 Evaluation—Commercial Items (52.212-2) (Deviation Mar 2026) tailored D8 Evaluation Factors D9 Technical Capability D10 Organizational Safety D11 Past Performance D12 Total Evaluated Price D13 Inquiries Regarding the Solicitation

SECTION E – OFFEROR’S REPRESENTATIONS, CERTIFICATIONS, AND OTHER STATEMENTS

52.252-1 Solicitation Provisions Incorporated by Reference (FEB 1998) 52.252-5 Authorized Deviations in Provisions (NOV 2020) Provisions Incorporated by reference 52.209-7 Information Regarding Responsibility Matters (Deviation May 2026)

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EXHIBITS

Exhibit E-1 Offeror’s Miscellaneous Information Exhibit E-2 Past Performance Questionnaire Exhibit E-3 Aircraft Questionnaire

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CONTRACT ACRONYMS

AC Advisory Circular ACETA Aerial Capture Eradication and Tagging of Animals AIRS Aviation Invoice Reporting Support Application AD Airworthiness Directive AOM Aviation Operations and Management A&P Airframe and Powerplant APCO Association of Public-Safety Communications Officials AQD Acquisition Services Directorate ASM Aviation Safety Manager ASTM American Society for Testing and Material ATC Air Traffic Control AUR Aircraft Use Report CFR Code of Federal Regulations CO Contracting Officer COR Contracting Officer’s Representative CTCSS Continuous Tone Coded Squelch System CFR Code of Federal Regulations CTCSS Continuous Tone Coded Squelch System DM Degrees/minutes/Decimal Minutes DOI Department of the Interior DOT Department of Transportation ELT Emergency Locator Transmitter EPA Environmental Protection Agency ERG Emergency Response Guidebook FAA Federal Aviation Administration FAR Federal Acquisition Regulations FS Forest Service FTR Federal Travel Regulations GVW Gross Vehicle Weight GPM Gallons Per Minute GPS Global Positioning System HIGE Hover-in-Ground Effect HOGE Hover-out-of-Ground Effect

HOGEJ Hover-out-of-Ground Effect, Jettisonable IAT Interagency Aviation Training IBC Interior Business Center ICAO International Civil Aviation Organization ICS Intercom System IFR Instrument Flight Rules IP Institute of Petroleum IPP Invoice Processing Platform MMSB Manufacturer’s Mandatory Service Bulletins NFPA National Fire Protection Association NTSB National Transportation Safety Board NWCG National Wildfire Coordinating Group PA Public Address System PA Pressure Altitude PFD Personal Flotation Device PIC Pilot-in-Command PPE Personal Protective Equipment PSD Plastic Sphere Dispenser PSI Pounds per Square Inch PTT Push to Talk RPM Revolutions per Minute SFI Safety Foundation Incorporated STEP Single-skid, Toe-In and Hover Exit/Entry Procedures TBO Time Between Overhaul TERO Tribal Employment Rights Ordinances TSO Technical Service Order UL Underwriter’s Laboratory USDA United States Department of Agriculture USWFS United States Wildland Fire Service VFR Visual Flight Rules VNE Velocity Never Exceed VOX Voice Activation VSWR Voltage Standing Wave Ratio

USWFS FW Point to Point 6 Solicitation #140D0426Q0468 Boise, Idaho

SECTION A - REQUIREMENTS AND PRICES

A1 ITEM REQUIREMENT

The purpose of this contract is for a Contractor to provide commercial aviation services in support of the U.S.

Wildland Fire Service (USWFS) for the transportation of personnel, goods, and cargo between the Contiguous U.S.

(Lower 48) and Alaska, with the Contractors’ primary base of operations located in Boise, Idaho. Contractor services include provisions of an airplane(s), pilot(s), fuel, aircraft maintenance support, and all other associated equipment, as long as the aircraft capabilities and terms and conditions of the contract are not affected.

Flight Crew. The contractor shall provide sufficient flight crew(s) for the aircraft offered. The contractor shall provide flight crew certified to operate contract aircraft under this item requirement and the Government shall schedule its operations accordingly.

ITEM DESCRIPTION

Designated Base: Boise, Idaho

Bureau: U.S. Wildland Fire Service (USWFS)

Aircraft Required: Multi engine turboprop or turbojet powered, extended over water fixed wing aircraft, equipped as specified in Section B.

Crew Compliment Required: Pilot-in-Command (PIC) and Second-in-Command (SIC).

Flight attendant(s) per 14 CFR 121.391

Minimum Aircraft Requirements:

• Must have a Standard Airworthiness Certificate.

• Aircraft certified under 14 CFR 25.

• An aircraft make and model for which engineering and logistical support, for continued airworthiness, is provided from the current type certificate holder or a supplemental type certificate holder.

• Pressurized aircraft with environmental controls. Heater and air conditioner. IFR/VFR, day/night known icing

• Insured seating for minimum 50 passengers and 100 pounds of cargo per passenger.

• Capable of operating Boise, ID to Anchorage, AK with one fuel stop that is located within the boundaries of the Contiguous U.S. or Alaska.

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A2. SCHEDULE OF SERVICES AND PRICES

IMPORTANT INFORMATION:

The contract price includes all applicable Federal, State, and local taxes and duties as per the Federal Acquisition Regulation (FAR) 52.212-4(k) Taxes.

Offerors shall use A2.1 to quote On Call services and A2.2 to quote Exclusive Use services. Funding availability will determine whether the contract award is made for On Call Services or Exclusive Use services. At this time, the Government anticipates awarding the contract for On-Call services; however, if sufficient funding becomes available, the Government may award the contract for Exclusive Use services.

The contract period is 60 days, anticipated to begin June 29, 2026, through August 28, 2026, with an option to extend for 30 days at the quoted rates.

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A2.1 ON CALL PRICING SCHEDULE FOR AIRCRAFT ADDRSSED IN SECTION A.1. DESIGNATED

BASE: BOISE, ID

CONTRACTOR’S BASE OF

OPERATION

CONTRACT

PERIOD

June 29, 2026 – August 28, 2026.(estimated)

AIRCRAFT FOR THIS

PRICING SCHEDULE

FAA Registration

OFFEROR NAME

ITEM

00010

DESCRIPTION

PAY

CODE

QUANTITY

UNIT

UNIT PRICE

EXTENDED

AMOUNT

Estimated Flight Hours (Dry without Fuel) Price per flight hour.

FD Estimated

FLIGHT

HOURS

Standby Rate Price per standby hour when the pilot is held in a ready status.

SB Estimated

HOURS

Additional pay items (T&M line item) The additional pay item estimated amount is calculated by the agency and is for funding purposes only. The amount implies no guarantee.

See Additional Pay Items Schedule NTE $10,000

ESTIMATED SUBTOTAL

A2.2 EXCLUSIVE USE PRICING SCHEDULE FOR AIRCRAFT ADDRSSED IN SECTION A.1.

DESIGNATED BASE:

BOISE, ID

CONTRACTOR’S BASE OF

OPERATION

EXCLUSIVE

PERIOD

June 29, 2026 – August 28, 2026

AIRCRAFT FOR THIS

PRICING SCHEDULE

FAA Registration

OFFEROR NAME

00010

CODE

QUANTITY

UNIT

UNIT PRICE

EXTENDED

AMOUNT

DAILY AVAILABILITY PRICE PER DAY – GUARANTEED SUBJECT TO BEING AVAILABLE

Daily Availability Guaranteed days per aircraft subject to availability

AV Guaranteed

DAYS

Estimated Flight Hours (Dry without Fuel)

FD Estimated

FLIGHT

HOURS

Additional pay items (T&M line item) The additional pay item estimated amount is calculated by the agency and is for funding purposes only. The amount implies no guarantee.

See Additional Pay Items Schedule NTE $10,000

ESTIMATED SUBTOTAL

A2.3 Flight hours are estimated and not guaranteed. The contractor shall not exceed the estimated hours or funding identified for additional pay items without approval from the Contracting Officer.

USWFS FW Point to Point 9 Solicitation #140D0426Q0468 Boise, Idaho

A2.4 Fuel will be furnished by the Government. All fuel not otherwise furnished by the Government must be purchased by or charged to the Contractor. The purchase must be approved by the Contracting Officer. Fuel related costs shall be recorded as a line entry (i.e., date, fuel charge, dollar amount, and use-item code fuel charge [FC]), and shall be supported by paid legible, itemized invoices from the supplier. Certified true copies may be submitted in lieu of the original invoice.

A2.5 Rates for flight hours shall be in whole dollars. If the unit prices are adjusted during the life of the contract, they will be adjusted to a whole dollar as follows: amounts of 50 cents or less will be rounded down and amounts of 51 cents or more will be rounded up.

USWFS FW Point to Point 10 Solicitation #140D0426Q0468 Boise, Idaho

A3 ADDITIONAL PAY ITEMS (TIME & MATERIALS IAW FAR 52.212-4 ALT 1)

A3.1 ADDITIONAL PAY ITEMS SCHEDULE

ITEM

CODE

QUANTITY UNIT UNIT PRICE

Unavailability UA Indefinite Hour $0.00

Non-Revenue Flights NR Indefinite Hour $0.00

Extended Standby – Pilot EP Indefinite Hour

Extended Standby – Driver ET Indefinite Hour

Fuel Servicing Vehicle – Mileage (750-1,499 gal) SML Indefinite Mile

Fuel Charge FC Indefinite Gallons Actual Cost

Subsistence Allowance (Per Diem) PD Indefinite Overnight Standard or High GSA Rate

Special Charge for Miscellaneous Allowable Expenses (i.e., rental car expenses, tie downs, Dept. of

Transportation fees, etc.)

SC Indefinite Each Actual Cost

See C21

SECTION B – TECHNICAL SPECIFICATIONS

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SECTION B – TECHNICAL SPECIFICATIONS

GENERAL REQUIREMENTS

B1 Scope of Contract

B1.1 The overall purpose of this contract is to obtain exclusive use aircraft services for the transportation of personnel, goods, and/or cargo in support of natural resource management activities to support the U.S. Wildland Fire Services between the Contiguous U.S. (Lower 48) and Alaska. Alaska Contractor services include provisions of an airplane/s, pilot(s), fuel, aircraft maintenance support, and all other associated equipment, as long as the aircraft capabilities and terms and conditions of the contract are not affected.

B1.1.1 The primary purpose of the contract is to provide aircraft services operating between Boise, ID and various locations in Alaska. The vendor must provide aircraft services in support of USWFS needs scheduled by the Government. Occasionally contracted aircraft will be dispatched from locations in the Contiguous U.S. other than Boise, ID.

B1.1.2 Primary destinations will be in Alaska and include: Anchorage, Palmer, McGrath, Fairbanks, Ft. Yukon, and Galena. Given the capability, aircraft may also fly into Soldotna, Kotzebue, Delta Junction, North Way, Nome, Unalakleet, Ruby, Ambler, Holly Cross, Dillingham, King Salmon, and Eagle on the rare occasion.

B1.2 The Government and Contractor must establish an effective working relationship to successfully complete this contract. The Contractor’s employees’ cooperation, professionalism, and positive attitude toward aviation safety and accomplishment of the USWFS' mission are an integral element of this relationship.

B1.3 The Government has interagency and cooperative agreements with other Federal agencies, and State agencies and may dispatch aircraft under this contract for such cooperative use. A new task order will be issued in these instances.

B1.4 Cargo. The loading and unloading of cargo for flights to and from Alaska is conducted by ramp personnel.

B2 Certification

The Contractor must obtain and keep current all of the following required certificates. The Contractor must ensure that contract personnel and aircraft are maintained in compliance with these certificates at all times.

B2.1 A Federal Aviation Administration (FAA) Air Carrier Certificate which authorizes the Contractor to operate in the category and class of aircraft and under flight conditions required by this contract (e.g., airplane, multiengine, visual flight rules (VFR), instrument flight rules (IFR), day/night, passengers, and cargo, Class II Navigation, carriage of hazardous materials (Will Carry), and authorization to operate a turbo jet aircraft on an other than hard surface runway, specifically compacted coral).

B2.2 Aircraft shall be identified as required by 14 CFR Part 121.135(7) or 135.63 or Operations Specifications Part D, “Aircraft Listing,” as appropriate. Aircraft shall be fully equipped to carry the number of passengers offered in accordance with the standards of 14 CFR Part 121 or 135, as appropriate.

B2.3 The contract aircraft must have engineering support for continued airworthiness from the current type certificate holder or supplemental type certificate holder.

B2.4 The aircraft must have a Standard Airworthiness Certificate issued under 14 CFR 21.183.

B2.5 The installation of any special equipment called for by this contract must be FAA-approved. Approval may be in accordance with an STC or FAA field approval.

USWFS FW Point to Point 12 Solicitation #140D0426Q0468 Boise, Idaho

B3 Order of Precedence - Specifications

In the event of inconsistencies within the technical specification, the following order shall be used in such resolution:

(i) Typed provisions of these specifications; (ii) USWFS Aviation Operations and Management (AOM) supplements and/or exhibits incorporated by reference; (iii) 14 CFR incorporated by reference; (iv) aircraft manufacturer's specifications; and (v) other documents incorporated by reference.

B4 Contracts and Task Orders

B4.1 The Contractor must maintain a complete, current copy of the contract, modifications, and task orders (if applicable) in each contract aircraft throughout the performance period.

B4.2 The pilot must have task order information (i.e., task number, performance period) in his/her possession prior to any flights under this contract and make this information available to government representatives on request.

B4.3 Electronic copies of contracts and task orders may be used. The contractor must ensure that the contract is current including all modifications and is uploaded on an appropriate viewing device (e.g., laptop or tablet), which must be charged and made available at the aircraft for reference by government representatives upon request.

Further, the contractor must agree to hold the government harmless for any inadvertent or accidental damage to the device.

EQUIPMENT REQUIREMENTS

B5 Condition of Equipment

The Contractor-furnished aircraft and all other required equipment must be operable, free of damage, and in good repair. Aircraft systems and components shall be free of leaks except where specified by the manufacturer.

B5.1 Prior to inspection and acceptance, the Contractor must permanently repair or replace all windows and windshields that have been temporarily repaired. All windows and windshields must be maintained at all times and must be clean and free of scratches, cracks, crazing, distortion, repairs, or tinting which hinder visibility.

B5.2 The aircraft interior must be clean and neat with no unrepaired tears, rips, or other damage. The exterior finish, including the paint, must be clean, neat, and in good condition. Any corrosion must be within manufacturer or FAA acceptable limits.

B5.3 See the Unacceptable Lap Belt and Shoulder Harness Conditions Exhibit for examples of lap belt and shoulder harness conditions that are not acceptable.

B6 Aircraft Equipment Requirements

The Contractor must provide a minimum of one fully compliant aircraft that is equipped as shown below:

B6.1 Current paper or electronic aeronautical charts covering the area of operations. Electronic Flight Bags (EFBs) are authorized but must be so through OpSpec A061.

B6.2 A first aid kit and Emergency Medical Kit required by 14 CFR Part 121 Appendix A or 14 CFR Part 135.177 as applicable.

B6.3 Emergency equipment: Extended overwater operations required by 14 CFR 135.167 or CFR 121 as applicable.

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B6.3.1 A survival kit containing at least the items specified in Alaska Statute Sec. 02.35.110. This survival kit and the life raft equipment required in B6.15 can be one and the same so long as both DOI and FAA standards are satisfied.

B6.4 Fire extinguisher(s) required by 14 CFR Part 135 or 121 for the purposes of this contract must be a handheld bottle, minimum 2-B:C rating, mounted and accessible to the flight crew while seated. The fire extinguisher must be maintained in accordance with National Fire Protection Association (NFPA) 10, Standards for Portable Fire Extinguishers, or the Contractor’s operations manual.

B6.5 Cabin heater/air conditioner with windshield defogger.

B6.6 Aircraft shall have FAA-approved shoulder harness equipped with inertia reel for both front seat positions.

Shoulder straps and lap belt shall fasten with metal-to-metal, single-point, quick-release mechanism.

B6.7 One set of individual lap belts for each occupant.

B6.8 Two high visibility strobe lights (one above and one below the fuselage) or a wingtip and tail strobe system.

This system will be independent of the anti-collision light and on a separate switch.

B6.9 Aircraft shall have approved lighting for night operation in accordance with 14 CFR 91, including instrument lights.

B6.10 The aircraft shall be equipped with FAA-approved cargo tiedown provisions, cargo straps, and cargo tiedowns for cargo operations.

B6.10.1 Cargo restraint installation shall secure cargo from shifting or slipping through or under restraint.

B6.10.2 Cargo tiedown provisions shall conform to Advisory Circular (AC) 43.13-2A or other approved data.

B6.11 If required by 14 CFR Parts 135 or 121, all aircraft furnished shall be equipped with a cockpit voice recorder and a flight data recorder.

B6.12 Reserved

B6.13 A personal floatation device (PFD) shall be provided for each passenger in the aircraft.

B6.14 Reserved

B6.15 Life raft. The life raft(s) specified by 14 CFR Part 135.167 or Part 121.339 shall be approved under TSO- C70a Type I and shall be a multiple tube design that provides full floor support in case of a failure of one of the tubes. The rated capacities shall be equal to or greater than the total number of occupants (pilots and passengers) required by the mission. A raft or rafts shall be carried in the main passenger cabin, readily accessible to the passengers; for deployment from the main cabin door. All first aid and survival equipment should be located together in the aircraft, making it easier for passengers and crew members to locate and deploy in an emergency.

B6.15.1 Each life raft shall contain 406MHz survival type ELT (ELT/S).

B7 Avionics Requirements

B7.1 General

B7.1.1 The Contractor must provide, install, and maintain the following systems in accordance with the manufacturer's specifications and the installation and maintenance standards of Section B7. Detailed avionics systems performance requirements are listed in Avionics Operational Test Standards (copies available upon request

USWFS FW Point to Point 14 Solicitation #140D0426Q0468 Boise, Idaho from AOM Avionics, or the most recent list may be found online at: https://www.nifc.gov/resources/NIICD/niicd-documents.

B7.1.2 All aircraft must meet any FAA requirements for the aircraft type, the route(s) to be flown, and the requirements specified in 14 CFR Part 135.165, Radio and Navigation equipment: 14 CFR 135.167 Extended over water and 14 CFR 135.163 Equipment requirements: Aircraft carrying passengers under IFR operations.

B7.2 Avionics Installation and Maintenance Standards

B7.2.1 Strict adherence to the recommendations in the following FAA Advisory Circulars is required: AC 43.13-1B Chapter 11, "Aircraft Electrical Systems," and Chapter 12, "Aircraft Avionics Systems”; AC 43.13-2B Chapter 1, "Structural Data," Chapter 2, "Communication, Navigation, and Emergency Locator Transmitter System Installations," and Chapter 3, "Antenna Installation."

B7.2.2 All avionics systems requiring an antenna must be installed with a properly matched, aircraft-certified antenna, unless otherwise specified. Antennas must be polarized as required by the avionics system and must have a voltage standing wave ratio (VSWR) of 3.0 to 1 or better.

B7.2.3 The Contractor must maintain the aircraft's dual static pressure system, altimeter instrument system, and automatic pressure altitude reporting system in accordance with the IFR requirements of 14 CFR Part 91.411 and must inspect and test said systems every 24 calendar months as specified by 14 CFR Part 43, appendices E and F.

B7.2.4 Transmitters shall not open squelch on, or interfere with, other AM or FM transceivers in the aircraft which monitor different frequencies. So-called “Transmit Interlock” functions shall not be used with communication transceivers.

B7.2.5 All installed transceivers must be placarded with designations matching the transmitter/receiver controls on the installed audio control system(s).

B7.3 Communication Systems.

B7.3.1. One automatic-fixed Emergency Locator Transmitter (ELT), certified under TSO-C126b (or newer) which must be installed in a conspicuous or marked location, and meet the same requirements as those detailed for aircraft in 14 CFR 91.207 (excluding section f). If not powered by its own, integral battery, the ELT remote switch/light must be powered by unswitched aircraft power. ELT antennas must be mounted externally to the aircraft unless installed in a location approved by the aircraft manufacturer. TSO-C126b and newer ELTs require documentation of current registration with the National Oceanic and Atmospheric Administration (NOAA), or the national civil aviation authority with which the aircraft is registered.

B7.3.2 VHF-AM aeronautical transceivers. Two VHF/AM (VHF-1, VHF-2) aeronautical transceivers, each operating in the 118.000 MHz to 135.975 MHz band, with a minimum of 720 channels in 25 kHz increments, and a minimum five watts carrier power output.

B7.3.3 Two HF-SSB/AM (HF-1, HF-2) transceiver systems, meeting the requirements of 14CFR135.165, and complying with the requirements for flights in airspace governed by the International Civil Aviation Organization (ICAO). The following frequencies must be available:

B7.3.3.1 As with all other installed communication systems, the HF/SSB’s must be integrated into the aircraft’s audio control systems. The aircraft must be equipped with SEL/Call.

B7.3.4 Radio equipment must comply with 14 CFR part 121.345

B7.3.5 Automated Flight Following (AFF) Program

B7.3.5.1 One satellite-based aircraft tracking hardware compatible with the government’s Automated Flight https://www.nifc.gov/resources/NIICD/niicd-documents https://www.nifc.gov/resources/NIICD/niicd-documents

USWFS FW Point to Point 15 Solicitation #140D0426Q0468 Boise, Idaho

Following (AFF) Program (https://www.aff.gov). Not all available satellite-based tracking systems are compatible with the Government’s AFF Program, nor meets AFF’s requirements. The contractor must ensure that the aircraft hardware offered is compatible with AFF.gov. For questions about current compatibility requirements, select the “HELP” button at https://www.aff.gov.

B7.3.5.2 The AFF aircraft hardware for each aircraft offered, must be powered by the aircraft’s electrical system, installed per the manufacturer’s installation manual, and operational in all phases of flight. AFF aircraft hardware must utilize as a minimum: Satellite communications, an externally or internally mounted antenna, provide data to the Government’s AFF viewing software, use aircraft power via a dedicated circuit breaker for power protection, and be mounted so as to not endanger any occupant from AFF aircraft hardware during periods of turbulence.

Antennas should be placed where they have the best view of the overhead sky as possible. Externally mounted antennas are recommended to improve system performance. Any visual indicators for remotely installed units must be mounted so that they can be easily viewed by the pilot.

B7.3.5.3 AFF communications must be always fully operational in all areas of operation. . Contractors working in or accepting dispatches to the State of Alaska, Southern Canada, or Western Canada must have an AFF system capable of being tracked in these locations at all times. Not all manufacturers’ AFF equipment communication links will operate effectively in all geographic areas.

B7.3.5.4 The contractor must maintain a subscription service through the AFF aircraft hardware provider allowing AFF position reporting for satellite tracking via the Government AFF viewing software. The position-reporting interval must be every two minutes while the aircraft is in flight. The contractor must register their AFF aircraft hardware with the Government through https://www.aff.gov providing complete tail number; manufacturer and serial number of the AFF transceiver; aircraft make and model; and contractor contact information. If the contractor relocates previously registered AFF aircraft hardware into another aircraft, then the contractor must contact the government’s AFF Program making the appropriate changes prior to aircraft use. In all cases, the contractor must ensure that the correct aircraft information is indicated within AFF. The contractor must notify the Government of system changes, scheduled maintenance, and planned service outages.

B7.3.5.5 Registration contact information, a web accessible feedback form, and additional information is available at: https://www.aff.gov.

B7.3.5.6 Prior to the aircraft’s annual contract inspection, the contractor must ensure compliance with all AFF systems requirements. The contractor must additionally perform an operational check of the system. As a minimum, the operational check must consist of confirming the aircraft being tested is displayed in AFF.gov (indicating it is currently transmitting data to AFF.gov) and that all information displayed in AFF.gov is current. A username and password are required to access AFF.gov. Log on to the AFF website at https://www.aff.gov to request a username and password.

B7.3.5.7 If AFF becomes inoperable/unreliable the aircraft may, at the discretion of the Government, remain available for service utilizing radio/voice system for flight following. The contractor will return the AFF system to full operational capability within 72 hours after the inoperative/unreliable unit is first discovered as defective.

B7.3.5.8 AFF Systems must comply with supplemental requirements contained in Specification Section Supplement document available at: https://www.aff.gov/support/Specification_Section_Supplement.pdf.

B7.3.5.9 Flight Following Ground Equipment and Coverage

B7.3.5.9.1 All base stations must have the necessary communications capability with the Contractor's central dispatch office to relay flight plans and to initiate search and rescue actions. All base stations must be manned continuously during flight operations. All base station operators must be fully trained in flight following emergency operations, and search and rescue coordination. All communications equipment must be properly maintained and kept in good repair.

B7.3.5.9.2 The areas of flight operations for this contract include areas of the Pacific Ocean

B7.3.5.9.3 Flight following procedures to be performed by the pilot for each flight include:

https://www.aff.gov/ https://www.aff.gov/ https://www.aff.gov/ https://www.aff.gov/ https://www.aff.gov/support/Specification_Section_Supplement.pdf

USWFS FW Point to Point 16 Solicitation #140D0426Q0468 Boise, Idaho

B7.3.5.9.3.1 Within no more than 15 minutes prior to departure, the pilot must file a flight plan with the appropriate Contractor's manned base station including: the aircraft call sign, the pilot's name, the number of passengers, the point and time of departure, the flight route, the destination, expected time of arrival, and the hours of fuel on board.

B7.3.5.9.3.2 Update the flight plan enroute as necessary.

B7.3.5.9.3.3 Close the flight plan within 15 minutes after arrival at the destination.

B7.3.5.9.3.4 For each flight the operators of the Contractor's manned base stations must:

B7.3.5.9.3.5 Record the flight plan as initially filed for each flight and modify the flight plan when requested by the pilot for enroute changes.

B7.3.5.9.3.6 Track the progress of the flight at 2-minute intervals during the flight and record all enroute position reports.

B7.3.5.9.3.7 Close the flight plan at the termination of the flight.

B7.3.5.9.3.8 In the event of failure to receive a scheduled position report, the base station operator must take the following actions:

B7.3.5.9.3.9 Within five minutes, attempt to communicate with the overdue aircraft directly, through any other base stations, any aircraft in the vicinity of the overdue flight, and all other available means.

B7.3.5.9.3.10 Should the operator be unable to communicate with the aircraft within an additional fifteen minutes, the Contractor must institute search and rescue operations for the aircraft and notify AOM, the U.S. Coast Guard and the, FAA. In any case, an air search must be initiated if a aircraft remains overdue 20 minutes beyond its report time or estimated time of arrival.

B7.3.5.10 Part 121 operators complying with CFR14 Subchapter G Part 121 Subpart F §121.125 will be considered fulfilling AFF requirements.

B7.3.6 Satellite Telephone (SatPhone) System

B7.3.6.1 One Iridium-network based Satellite Telephone (Satphone) system. The installation must be in accordance with 14 CFR 43.

B7.3.6.2 The satphone handset, or remote dialer, must be mounted in a convenient location in the cockpit. The location must provide ready and unencumbered access to its controls by both front seat occupants.

B7.3.6.3 The satphone system audio must be permanently interfaced to the aircraft audio system in the same manner as the aircraft radios, so that the pilot and observer/copilot can utilize the satphone via their headsets. It is preferred that all occupants of the aircraft be able to converse over the satphone through their headsets, though keypad access may be limited to the two front seat occupants.

B7.3.6.4 The satphone system must provide the capability to pre-program at least six (6) telephone numbers that can be quickly selected by either front seat occupant while in flight.

B7.3.6.5 A TSO C-129a L-band antenna, acceptable to the manufacturer of the Sat Phone system, must be installed on top of the fuselage, giving as much a view of the overhead hemisphere as possible.

B7.3.6.6 The Sat Phone system may be integrated into the Automated Flight Following system (see B7.3.5) using either the same Iridium communicator or a separate Iridium communicator. In the former case, it is acceptable for phone calls to interrupt the transmission of AFF position reports for brief periods of time, and flight crews must be instructed as to this conflict.

USWFS FW Point to Point 17 Solicitation #140D0426Q0468 Boise, Idaho

B7.4 Navigation Systems.

B7.4.1 Two permanently installed, panel-mounted, Global Positioning System (GPS 1, GPS 2). The GPS(s) must be certified to TSO-C146 for IFR operations using the Wide-Area Augmentation System (WAAS), utilize the WGS-84 datum, reference latitude and longitude coordinates in the degrees/minutes/decimal minutes (DM) mode for aircraft positioning; utilize an approved, fixed, external aircraft antenna; and be powered by the aircraft electrical system.

All GPS(s) systems must allow for continuous application of aircraft electrical power through circuit protected source. GPS(s) must incorporate Wi-Fi and Bluetooth connectivity capabilities for entering flight plans and updating databases. The GPS(s) navigation database must always be current and cover all areas of operation. The GPS(s) installation must be FAA approved (or approval pending). Handheld, portable, and/or marine type equipment is not acceptable. Portable Aviation GPS units, GPS tablets, or mobile GPS device systems will not be used for primary navigation in aircraft conducting IFR operations.

B7.4.2 Additional Navigational Systems. The aircraft must be equipped with the navigational equipment required for IFR operations as specified in 14 CFR 121 subpart K 301-359, including, but not limited to, the following:

B7.4.2.1 Two VHF, VOR/LOC aeronautical navigation receivers (NAV-1, NAV-2) with indicators, each with a minimum of 100 navigation receive channels.

B7.4.2.2 One glideslope (GS) system, with a minimum of 40 receive channels.

B7.4.2.34 One marker beacon receiver system with three-light indicator must be installed. The audio warning must be provided to the flight crew’s earphones. The marker beacon receiver system is not required, if the aircraft is equipped with approved substitute equipment as described 14 CFR 91.175 (k).

Note: 14 CFr 91.175 (k) Approved substitute equipment is described as compass locator; precision approach radar (PAR) or airport surveillance radar (ASR); DME, VOR, or nondirectional beacon fixes authorized in the standard instrument approach procedure; or a suitable RNAV system in conjunction with a fix identified in the standard instrument approach procedure.

B7.4.2.4 Automatic Direction Finder (ADF) receiver system, with indicator, covering the frequency range of 200 to 1,699 kHz as a minimum.

Note: The ADF system is not required when both IFR GPS’s above are operable.

B7.4.2.5 Distance Measuring Equipment (DME) system, with a minimum of 200 channels.

B7.4.2.6 Horizontal Situation Indicator (HSI) or equivalent digital instrument system. The CDI must be interfaced to other aircraft systems so as to display VOR/LOC and GPS information on the CDI.

B7.4.2.7 Radio Magnetic Indicator (RMI) or equivalent digital instrument presentation incorporated with NAV- 1/ADF/GPS on single needle, and NAV-2/ADF/GPS on double needle.

B7.5 Audio Systems

B7.5.1 Two separate audio control systems (which may be combined in a single unit) for the pilot and observer/co-pilot to select receiver audio outputs and transmitter microphone/push to talk (PTT) audio inputs for all installed radios and public address (PA) systems. Each system must also allow the pilot and observer/copilot to independently adjust both the intercommunications system (ICS) and the receiver audio output levels.

B7.5.1.1 Transmitter selection and operation. Separate transmitter selection controls must be provided for both the pilot’s and observer/copilot’s microphone/PTT inputs. The system must be configured so the pilot and observer/copilot may each simultaneously select and utilize a different transmitter (or PA system when installed) via their respective microphone/PTT. Whenever a transmitter is selected, the companion receiver audio must

USWFS FW Point to Point 18 Solicitation #140D0426Q0468 Boise, Idaho automatically be selected for the corresponding earphone. Transmitter sidetone audio must be provided for the user as well as for cross-monitoring via the corresponding receiver selection switch on the other audio control system.

B7.5.1.2 Receiver selection and operation. Separate controls must be provided for both pilot and observer/copilot to select audio from one or any combination of available receivers. The ICS-equipped aft passenger positions must monitor the receiver(s) as selected by the observer/copilot. The receiver audio output must be free of excessive distortion, hum, noise, and crosstalk, and must be amplified sufficiently to facilitate ease of use in a noisy cockpit/cabin environment.

B7.5.1.3 The audio system(s) controls must be located and arranged so that both the pilot and observer/copilot, when seated, have full movement of their respective controls without interference from their clothing, the cockpit structure, or the flight controls. Labeling and marking of controls must be clear, understandable, legible, and permanent. Electronic label maker marking is acceptable.

B7.5.2 An ICS for the pilot and observer/copilot positions. ICS audio must mix with, but not mute, selected receiver audio. An ICS audio level control must be provided for each position above. Adjustment of the ICS audio level at any position must not affect the level at any other position. A "hot mic" capability, controlled via an activation switch or voice activation (VOX), must be provided for the pilot and copilot/observer positions. ICS sidetone audio must be provided for the earphones corresponding with the microphone in use. The ICS audio output must be free of excessive distortion, hum, noise, and crosstalk and must be amplified sufficiently to facilitate ease of use in a noisy cockpit/cabin environment.

B7.5.3 Earphones, microphones, PTTs, and jacks designed for operation with 600-ohm earphones and carbon-equivalent, noise-canceling boom type microphones (Gentex electret type Model 5060-2, military dynamic typeM-87/AIC with CE-100 TR preamplifier, or equivalent) must be furnished at all required positions.

B7.5.3.1 J-033 and J-034 type connector jacks must be provided at all required positions in the aircraft to accept the PJ-055B and PJ-068 type connector plugs as utilized with the headset/ microphone.

B7.5.4 Public Address (PA) system. The pilot, copilot/observer, and cabin crew must be able to convey messages to the occupants of the cabin by means of a PA system which utilizes the same microphone as utilized for radio and ICS communications. The PA system must comply with 14 CFR part 135.150. The PA system must include the following:

a) An amplifier with output adequate to convey intelligible messages to all cabin occupants.

b) One or more cabin speakers, as necessary.

c) Audio system controls which enable routing of transmit and receive audio, from one or any combination of required radios, as well as ICS messages from the pilot, copilot/observer, or spotter positions, through the cabin speakers.

d) A PA audio level control at the audio control panel which enables adjustment of the audio level on all cabin speakers.

B7.6 Other Avionics.

B7.6.1 One air traffic control (ATC) transponder and altitude reporting system meeting the requirements of 14 CFR Part 121.345 and TSO C-112, maintained in accordance with the IFR requirements of 14 CFR Part 91.413 and inspected and tested every 24 calendar months.

B7.6.2 The aircraft must be equipped with a FAA Technical Standard Order (TSO) approved Traffic Alert and Collision Avoidance System (TCAS II) Airborne Equipment per 14 CFR 121.356 and TSO C-119b unless otherwise authorized by the FAA administrator, featuring active interrogation of threat aircraft. The system’s antennas must be mounted on the aircraft to minimize airframe shadowing and provide 360-degree coverage. The system must also incorporate visual alerts for both pilot and co-pilot and an aural alerting feature which announces an alert of threat aircraft whenever such aircraft enters a zone of a programmable size with range selections from no more than two nautical miles to at least ten nautical miles around the aircraft. The audio alert output must be interconnected to

USWFS FW Point to Point 19 Solicitation #140D0426Q0468 Boise, Idaho the aircraft's audio system in such a manner that all ICS-equipped positions will receive the alert. If the aircraft is equipped with a Multi-Function Display (MFD), GPS, or other system capable of displaying threat aircraft output data, the system must also be interfaced to such. The airplane flight manual required by shall contain the following information on the TCAS II system required by this section:

(1) Appropriate procedures for:

(i) The use of the equipment; and

(ii) Proper flight crew action with respect to the equipment operation.

(2) An outline of all input sources that must be operating for the TCAS II to function properly.

B7.6.2.1 The system must be installed in accordance with an STC, or FAA Field Approval based upon an existing STC and the manufacturers installation manual. Installation of the system must be accomplished by a certified avionics repair station which has been approved for such by the system’s manufacturer. The system must be maintained for continued airworthiness but may be listed in an approved Minimum Equipment List (MEL), provided the MEL does not permit the system to be inoperable for a period exceeding 15 days.

B7.6.2.3 Satellite-based Traffic Information Systems (TIS), and Automatic Dependent Survey Type “B” (ADS-B) systems do not meet the above requirements.

B7.6.2 Reserved.

B7.6.3 One radar altimeter with indicator, having a minimum altitude range of from 20 to 2000 feet, variable decision height selection, and decision height arrival aural warning

B7.6.4 Reserved

B7.6.5 Reserved

B7.6. 6 Automatic Dependent Surveillance – Broadcast (ADS-B)

B7.6.6.1 All aircraft must be equipped to meet the ADS-B OUT requirements of 14 CFR 91.225. ADS-B OUT systems must be approved to either TSO-C154c (978MHz Universal Access Transceiver [UAT]) or TSO-C166b (1090MHz Extended Squitter [1090ES]). Aircraft operating outside of the United States must be equipped with systems approved to TSO-C166b.

B7.6.6.2 ADS-B IN system is required, system furnished must be TSO-approved, receive both UAT and 1090ES, and be interfaced to a multifunction display (MFD) or tablet or mobile device, minimum size of 3.0 inches wide x 1.5 inches high capable of displaying TIS-B traffic and FIS-B weather.

B7.6.6.3 All ADS-B systems installed in aircraft that are required to transition between the contiguous United States and Alaska through Canadian airspace must follow Canadian ADS-B Out Performance Requirements Mandate which may include a diversity transponder system and this system must be TSO-approved with diversity antennas on both the top and bottom of the aircraft.B7.6.7 One Terrain Awareness and Warning System class A (TAWS-A) or Enhanced Ground Proximity Warning System (EGPWS) ensuring they are operational and maintained per manufacturer guidelines.

TAWS-A or EGPWS installations will comply with applicable regulations in the Code of Federal Regulations (CFR), specifically 14 CFR 121.354, and TSO-C151c. The audio alert output must be interconnected to the aircraft's audio system in such a manner that flight crew positions will receive the alert. The aircraft must include an approved terrain situational awareness display such as a Multi-Function Display (MFD), GPS, or other system capable of displaying TAWS/EGPWS output data. The aircraft flight manual must include:

a. Procedure for using the TAWS

b. Proper flight crew reaction to TAWS audio and visual warnings

USWFS FW Point to Point 20 Solicitation #140D0426Q0468 Boise, Idaho

B7.6.7.1 The Contractor shall also install a pilot-controlled TAWS inhibit switch in the aircraft. This switch must enable the flight crew to temporarily disable TAWS alerts under specific conditions where the alerts may not be applicable. The following requirements apply:

a. The switch must be clearly labeled and easily accessible to the pilot.

b. The system must provide visual or audible confirmation when the inhibit function is activated.

c. The switch must comply with all relevant regulatory standards and guidance.

B7.6.7.2 The Airplane Flight Manual (AFM) shall contain appropriate procedures for: The use of the terrain awareness and warning system; and proper flight crew reaction in response to the terrain awareness and warning system audio and visual warnings.

B7.6.8 The aircraft must be equipped with two permanently installed circuit-breaker protected, dual USB charging ports. The ports must be approved under TSO-C71, providing a maximum of 2.1A power at 5VDC and mounted in a location convenient to the pilot…