RFI_-_On_Call_Smokejumper_Flight_Svcs_1.docx

This Public Notice is not a Solicitation, but instead for the purpose of providing industry an opportunity to submit comments and propose improvements on below draft Government requirement. The Government will not award a contract based on this Public Notice, the information received, nor reimburse participants for information they provide. Information provided is strictly voluntary. This Public Notice is for market research and planning purposes only and to allow industry the opportunity to verify reasonableness and feasibility of the requirement, obtain proposed improvements from industry, as well as promote future competition.

The Government has begun preliminary planning for On Call Smokejumper Flight Services single award IDIQ. At this point, the Government is still developing the requirement and the number of guaranteed days are unknown at this time. The Government is also requesting baseline pricing for market research purposes. Please provide a budgetary estimate on both Daily Availability (AV) and Flight Time (FT) rates utilizing the attached RFI Estimated Price Schedule (Attachment 1). These rates are strictly for market research purposes and the Government understands that estimated rates submitted are not binding.

Comments, proposed improvements, and pricing need to be submitted in the following format to ensure they are properly identified and responded to:

· E-mail Subject Line: On Call Smokejumper Public Notice Comments – (Insert Vendor Name)

· Each comment shall be numbered individually

· Identify specification sections applicable to the comment (example B6.1.5)

· Brief rationale supporting any proposed improvements to specifications

· All comments and proposed improvements shall be submitted in a single Microsoft Word document titled “On Call Smokejumper Flight Services Public Notice Comments – (Insert Vendor Name)” and estimated rates shall be submitted by completing the attached Microsoft Excel RFI Estimated Price Schedule (Attachment 1) also titled “On Call Smokejumper Flight Services Public Notice Comments – (Insert Vendor Name)” sent via email.

If after submission, an interested party identifies additional comments, proposed improvements, or revised estimated rates within the open period, they may submit revised documents titled as follows:

· E-mail Subject Line: On Call Smokejumper Public Notice Comments – (Insert Vendor Name) Rev 1

· Word document titled “On Call Smokejumper Public Notice Comments – (Insert Vendor Name) Rev 1”

· Excel spreadsheet (RFI Estimated Price Schedule – Attachment 1) titled “On Call Smokejumper Public Notice Comments – (Insert Vendor Name) Rev 1”

Responses should be emailed to Sonja Crockett at sonja_crockett@ibc.doi.gov.

SCHEDULE OF SUPPLIES/SERVICES

A1 – Item Requirement The Department of Interior (DOI), Bureau of Land Management (BLM), intend to request information from industry for Smokejumper Aircraft Services contracts on an on-call basis. The aircraft will be used for transporting and dropping smokejumpers, transporting, and dropping paracargo, reconnaissance, testing of parachutes, and other aerial equipment, transportation of personnel and cargo in support of fire suppression activities, search and rescue, natural resources missions, and other administrative and related resources activities as directed by the Government. Each aircraft will be fully-contractor-operated, and contractor-maintained. The contractor will provide both scheduled and nonscheduled maintenance as required to keep the aircraft airworthy in with Federal Aviation Administration (FAA) regulations and DOI policy.

The designated base of operations for the aircraft is Boise, Idaho; however, the aircraft will be subject to dispatch anywhere in the contiguous United States and Alaska. Should an RFP be generated based on responses to this RFI the resulting Indefinite Delivery, Indefinite Quantity (IDIQ) contract’s performance period will be a base year with four one-year option periods. The Contractor shall be required to respond and commence operations at Boise, ID, or other locations as mutually agreed upon within a maximum of 24 hours from the time the Government contacts the Contractor.

Performance Period:

Minimum Aircraft Requirements:

Must have a Standard Airworthiness Certificate.

Aircraft certified under Civil Air Regulation Part 3, 14 CFR 23 or 25.

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

VFR/IFR, Day/Night. Aircraft certified for IFR flight only with cargo door installed are acceptable.

Payload of 3,300 pounds with 2.25 hours of fuel plus a 30 minute fuel reserve, 200 pounds per pilot, and 25 pound survival kit when equipped for smokejumper operations as required per Section B.

Capable of operating as configured above from 3,000-foot gravel runway at 2000 feet pressure altitude and 25º Celsius.

Minimum seating for six smokejumpers on Simula seats or other approved seats for smokejumpers.

Side-facing exit aft of main landing gear with FAA approval for aircraft operation with door removed or in-flight opening of this exit door.

Interagency Smokejumper Aircraft Screening and Evaluation Subcommittee (SASES) approved.

REQUEST FOR INFORMATION – ON CALL SMOKEJUMPER FLIGHT SERVICES

GENERAL REQUIREMENTS

B1 Scope of Contract B1.1 The intent of this contract is to obtain one fully contractor-operated and maintained on call (OC) fixed wing Smokejumper platform within the contiguous 48 States and Alaska. Contractor services include provisions of an airplane, pilot(s), fuel, aircraft maintenance support, and all other associated equipment, as prescribed in this solicitation. Aircraft will be used for transporting and dropping smokejumpers, transporting and dropping paracargo, reconnaissance, testing of parachutes, and other aerial equipment, transportation of personnel and cargo in support of fire suppression activities, search and rescue, natural resources missions, and other administrative and related resources activities as directed by the Government.

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 mission are an integral element of this relationship.

B1.3 The Government has interagency and cooperative agreements with other Federal agencies, State agencies, and private landholders and may dispatch aircraft under this contract for such cooperative use.

B1.4 Aircraft may be dispatched to or from Alaska. Because deployment to or from Alaska usually requires transit through Canada, contractor personnel are required to possess current passports if transiting through Canada. For additional Alaska-specific equipment and/or operational requirements, refer to the Alaska Airplane Supplement Exhibit (see Section C).

B1.5 During any task order period, aircraft furnished shall be subject to the exclusive use of the Government.

B1.6 This aircraft may be dispatched to Alaska. For the Alaska-specific equipment and/or operational requirements, refer to the Alaska Supplement Exhibit (see Section C).

B2 Certification The Contractor must obtain and keep current all the following required certificates and must ensure that contract aircraft are operated and maintained in compliance with those certificates at all times:

B2.1 A Title 14 of the Code of Federal Regulations (CFR) Air Carrier Certificate or Operating 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).

B2.2 The aircraft must be carried on the list required by 14 CFR Part 135.63 or Operations Specifications Part D, "Aircraft Listing," as appropriate.

B2.3 The contract aircraft must have a Standard Airworthiness Certificate and have engineering support for continued air worthiness from the current type certificate holder or supplemental type certificate holder. Installation of any equipment required by this contract must be FAA approved.

B2.4 The Contractor must have Operations Specifications that permit all Contiguous United States and Alaska operations.

B2.5 The aircraft must have a Standard Airworthiness Certificate issued under 14 CFR 21.183.

B2.6 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. This includes Government-furnished equipment (GFE): Simula seats. The contractor may offer an alternative to the side facing Simula bench seat. (See B6.5) B2.7 The aircraft may also have a restricted airworthiness certificate issued under 14 CFR 21.25 and 21.185 to include the special purpose of forest and wildlife conservation (fire suppression) work. Aircraft with a restricted airworthiness certificate must also have a standard airworthiness certificate. Multiple Airworthiness Certificates are issued in accordance with 14 CFR 21.187.

B2.7.1 When the aircraft is configured for smokejumper operations it may be operated in the restricted airworthiness category.

B2.7.2 Installation of Government Simula seats and operations with an open door may necessitate the aircraft to be operated in the restricted category.

B2.7.3 If the aircraft is to be operated with a restricted airworthiness certificate the Contractor must have a certificate of waiver or authorization issued from the FAA to the Contractor authorizing operation of a Restricted Category aircraft over densely populated areas. The specific regulation required to be waived is: 14 CFR 91.313(e)(1)(2) and (3).

B2.8 For contracts less than 90 days, the Contractor must have a certificate of waiver or authorization issued from the FAA to the Contractor authorizing operations at less than minimum safe altitudes as prescribed in 14 CFR 91.119 (a)(b) and c). Paracargo operations are conducted between 150 feet AGL and 400 feet AGL. Paracargo is dropped in congested areas, other than congested areas and in sparsely populated areas as required to support firefighting operations.

B2.9 A Contractor from the lower 48 dispatched to Alaska needs to have Operations Specifications that permit Alaska operations.

B2.10 See Exhibit 8, Alaska Supplement 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) DOI OAS Office of Aviation Services supplements and/or exhibits incorporated by reference; (iii) 14 CFR incorporated by reference; (iv) aircraft manufacturer's specifications; (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 are 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 The internal cabin area near the exit door and the external fuselage aft of and below the exit door shall be free of protrusions and sharp edges. The Government will install a jump door "boot" (i.e., fiberglass/Teflon fairing) that covers the aft and bottom edges of the door opening. Protrusions and sharp edges that cannot be removed shall be adequately protected to prevent snagging or chaffing of equipment.

B5.4 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 one fully compliant aircraft that is equipped as shown below:

B6.1 Standard equipment.

B6.1.1 A first aid kit containing items specified in the First Aid and Survival Kits Exhibit shall be installed in the cabin.

B6.1.2 A survival kit containing items specified in the First Aid and Survival Kits Exhibit shall be carried aboard the aircraft on all flights and shall be included in weight and balance/load calculations.

B6.1.3 Fire extinguisher(s), as required by 14 CFR Part 135, 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) Manual 10, Standards for Portable Fire Extinguishers or the Contractor’s 135 operations manual.

B6.1.4 FAA-approved seats, seatbelts, and shoulder harnesses for the pilot and copilot.

B6.1.5 The aircraft must be approved for at least nine (9) passengers. Standard seating configuration is four government installed two person Simula bench seats and one contractor provided single person passenger seat at the right side most aft position. The contractor must provide one additional passenger seat for the left side of the passenger compartment. Contractor provided seats must be FAA-approved seats and must be removable to allow for a cargo configuration.

B6.1.6 Federal Aviation Administration-approved anti-collision lighting to include at least one high visibility strobe light.

B6.1.7 High visibility, pulsating, forward-facing, conspicuous light.

B6.1.8 FAA-approved cargo restraints, cargo nets, and cargo straps for cargo tiedown in cabin and baggage compartment areas. (DO-228 only).

B6.1.9 Cabin heater.

B6.1.10 The aircraft must be equipped in accordance with 14 CFR Parts 91 and 135 for carrying passengers day and night, VFR and IFR.

B6.1.11 Reserved B6.1.12 DHC-6 only: Long Nose” configuration with a compartment volume of 38 cubic feet.

B6.2 Contractor-furnished specialized equipment.

B6.2.1 A horizontally mounted parachute static line attach cable or track constructed and installed in accordance with National Technology & Development Program (NTDP) drawings and FAA STC, or manufacturer’s specifications (as applicable).

B6.2.2 A vertically mounted parachute static line attach cable with support strut constructed and installed in accordance with NTDP drawings and FAA STC.

B6.2.3 An external step and step attachment constructed and installed in accordance with NTDP drawings, applicable to the aircraft with a door height less than 52 inches.

B6.2.4 A handrail of smooth contour that shall encircle the entire top and the upper half of the forward side of the left side jumper exit/paracargo door opening. The handrail shall be designed and installed so as not to restrict the size of the door opening and not to hinder the opening or removal of the door. The handrail must be constructed and installed in accordance with NTDP drawings or manufacturer’s specifications.

Note: Upon request, the Government will provide drawings for appropriate aircraft showing specifications, locations, and general installation details. Two static line attach anchors may not be required in all aircraft. Some aircraft will not need the jump-step or anchor points.

B6.2.5 A sheath knife (minimum blade length 4.5 inches) easily accessible, securely mounted on the bulkhead or cabin sidewall aft of the exit door.

B6.2.6 Reserved B6.2.7 Heavy-duty floor stressed to 200 pounds per square foot or installed wooden or metal deck plating as necessary to achieve this load capacity.

B6.2.8 Placards. The aircraft must have placards which denote prescribed smokejumper drop speed and flap setting. The placard must be permanent with letters 3/8-inch minimum height. The placard shall be clearly visible at the pilot-in-command position and the spotter station.

B6.2.9 For a DHC6:

B6.2.9.1 Standard Douglas (Brownline) - type seat track and a minimum of 12 cargo tiedown rings and two ratcheting type cargo straps (6,000-pound minimum capacity at least 15 feet long) to adequately secure multiple bundle cargo loads.

B6.2.9.1.1 The standard Douglastype seat track will be installed over the left and right under floor seat rails from passenger compartment forward bulkhead rearward to most aft bulkhead (or station 266 on DHC6).

B6.2.9.1.2 The left track will be installed in sections with openings between sections to permit the legs of the fold-up utility seats to engage the cutouts in the aircraft floor.

B6.2.9.1.3 In addition to the floor-mounted seat track, tracks of the same specifications will be installed along each cabin side-wall directly below the fold-up seat attach fittings and extend from the forward most factory-installed nut plate location to the location of the most rearward fold-up seat attach fittings on each side. This seat track may be "notched" as necessary immediately below each seat fitting to allow structural clearance for parts of the seat assembly. (See MTDC drawing 805.) The nut plates are part of the De Havilland customer option package MOD 6/1225.

B6.2.9.1.4 Aft track segment for use with smoke-jumper restraint system must be installed. (See paragraph 6.5.4, MTDC Smokejumper Aircraft Accessories Equipment Drawings List, drawing MTDC 805.)

B6.2.10 Any aircraft other than the DHC6 offered:

B6.2.10.1 Aircraft must have the same capability, FAA approved, as referenced in paragraph B6.2.9. The seat track arrangement is similar to that used for mounting standard commuter seats and is intended for cargo tiedown rings.

B6.3 Side Door Requirements.

B6.3.1 Minimum dimensions: height 36 inches, width 25 inches.

B6.3.2 Must be aft of the main landing gear.

B6.3.3 Must be constructed and insulated to reduce heat loss and reduce wind noise in flight.

B6.3.4 Must be a utility/cargo-type door (not airstair door) approved for standard operations, passenger and cargo.

B6.3.5 Must be FAA approved for in-flight opening or removable. A jump door "boot" (i.e., fiberglass/Teflon fairing) must be installed to cover the aft and bottom edges of the door opening.

Note: B6.3.4 and B6.3.5 may be to the same door or two separate doors that are interchangeable.

B6.3.6 An external fabric door may be used for security and weather when the aircraft is parked but may not be used for flight.

B6.3.7 No protrusions are permitted between the jump door and the tail of the aircraft that might interfere with the parachute deployment or retrieval of static lines and deployment bags.

B6.4 A complete set of current aeronautical charts covering the expected area of operations.

Note: Electronic flight bags are acceptable if authorized by the FAA in the company’s operation specifications B6.4.1 Complete set of current aeronautical charts and navigation publications covering areas of operation within Alaska and Canada when in transit.

B6.5 Government Equipment and Drawings. To be furnished to Contractor prior to use or at a mutually agreed upon time.

B6.5.1 Smokejumper side-facing seats, Simula seats. A Government accepted vendor provided alternative may be used in lieu of the Simula seats.

B6.5.1.1 The contractor may provide FAA approved side facing bench style seats with storage space under them for at least eight (8) smokejumpers, in lieu of GFE-Simula seats.

B6.5.2 The Professional Smokejumper Pilot and Spotter video program,

a) Part One: https://www.youtube.com/watch?v=q0Lg7GdrBQ8&feature=youtu.be

b) Part Two: https://www.youtube.com/watch?v=cWzt8ip9dls&feature=youtu.be

c) Part Three: https://www.youtube.com/watch?v=K--MEfjgAQc&feature=youtu.be

d) Part Four: https://www.youtube.com/watch?v=_aENhhaPsxc&feature=youtu.be B6.5.3 Spotters’ helmets.

B6.5.4 Drawings necessary for smokejumper aircraft accessories (when requested). The following drawings are available:

B6.5.4.1 Primary vertical anchor, secondary horizontal anchor jump-step, step attachment, and other accessories. Drawings for these items are available from the USDA Forest Service, National Technology and Development Program (NTDP), 5785 Hwy 10 W, Missoula, Montana 59808, Attention: NTDP Smokejumper Equipment Specialist, telephone 406-329-3900.

B6.5.5 Door boot. (See B5.3) B6.5.6 If an inflight door is not installed, a 1½- to 2-inch safety strap across the door opening that may be easily and swiftly connected/disconnected in flight.

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(FS/OAS_A24F) (copies available upon request from OAS Avionics, or the most recent list may be found online at: https://www.nifc.gov/resources/NIICD/niicd-documents .)

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 Although the contract aircraft may not be certified for flight under instrument flight rules (IFR), the aircraft's static pressure system, altimeter instrument system, and automatic pressure altitude reporting system must be maintained in accordance with the IFR requirements of 14 CFR Part 91.411 and inspected and tested 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 are monitoring 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 Communications Systems.

B7.3.1 One automatic-fixed Emergency Locator Transmitter (ELT), certified under TSO-C126 (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-C126 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 Two panel-mounted VHF-AM (VHF-1, VHF-2) aeronautical transceivers, each with a minimum of 760 channels covering 118.000 to 136.975 MHz. The transceivers must have channels selectable in no greater than 25 kHz increments and a minimum of 5 watts carrier output power. The transceivers’ operational controls must be mounted so they are readily visible and accessible to the pilot. Although not required by Federal Aviation Regulations, the aircraft’s radio call sign (normally the aircraft registration number) must be displayed on the instrument panel, in view of the flight crew.

B7.3.3 Two P25-compliant VHF-FM transceivers. Each transceiver (FM-1, FM-2) must provide selection of narrowband analog (12.5 kHz) or narrowband digital (12.5kHz) operation on each of a minimum of 100 channels. Each transceiver’s operational controls must be located and arranged so that the pilot and observer/copilot, when seated, have full and unrestricted movement of each control without interference from their clothing, the cockpit structure, or the flight controls.

B7.3.3.1 Each VHF-FM transceiver’s operational frequency range must include the band of 136.0000 MHz to 173.9975 MHz. The operator(s) must be able to program any usable channels within that band, along with any required CTCSS tones, National Access Codes (NAC’s), or Talk Group ID’s (TGID’s), while in flight. Each VHF-FM transceiver must also incorporate a separate, programmable GUARD receiver, with accompanying GUARD transmit capability. Unless instructed by the Government for use on a specific project, all frequencies programmed for use under this Contract must be in the narrowband analog mode.

B7.3.3.2 Carrier output power for each VHF-FM transceiver must be 10 watts nominal value (original design specification). Each transceiver must be capable of displaying receiver and transmitter operating frequency, alpha-numeric channel labels, and must provide both receiver and transmitter activation indicators for MAIN and GUARD. Simultaneous monitoring of both MAIN and GUARD receivers is required. Scanning of the GUARD frequency is not acceptable.

B7.3.3.3 Prior to acceptance under this contract, at least one VHF-FM transceiver must be programmed with the narrowband analog GUARD receive and transmit frequencies of 168.625 MHz, with a 110.9 Hz CTCSS tone on transmit only.

B7.3.3.4 The following VHF-FM aeronautical transceivers are known to meet the above requirements:

Technisonics: TDFM-136, TDFM-136A, TDFM-136/NV, TDFM-136A/NV, TDFM-136B, TDFM-136B/NV Cobham (formerly NAT): NPX-136D-070 B7.3.3.5 Each required VHF-FM transceiver must be equipped with a conveniently located programming port, to facilitate programming via a government-owned laptop computer. The port(s) must be protected from accidental damage via contact, be hard-wired to the transceiver(s), not require switching of any cables for utilization, and must be conveniently located for ease of use. The Contractor must also furnish appropriate cables of adequate length, and/or any necessary adapters, to interconnect the aircraft programming ports to the serial and/or USB port(s) of the Government laptop computers as required.

NOTE: The “DIN” type connector receptacle on the front panel of some TDFM-136-series radios is part of an encryption feature and may not function as a programming port connector. This connector can be utilized for channel programming on model TDFM-136A, serial numbers FDA1200 and higher, and model TDFM-136B ONLY.

B7.3.4 Provisions for Auxiliary VHF-FM (AUX-FM) portable radio B7.3.4.1 Interface for installing and properly operating an auxiliary VHF-FM portable radio through the aircraft's audio control system(s). The interface must consist of the appropriate wiring from the audio control system, terminated in an ITT/Cannon type MS3112E1210S 10-pin connector conveniently located for use by the observer/copilot, and utilizing the contact assignments as specified by drawing FS/OAS A-17 in Exhibit 8.

B7.3.4.2 One weatherproof, external, broadband antenna covering the 150-174 MHz band, with associated RG-58A/U (or equivalent) coaxial cable and connector, terminated in a bulkhead-mounted, female BNC connector (type UG-290A), conveniently located for use by the observer/copilot adjacent to the above 10-pin connector (Comant model CI-177 or equal).

B7.3.4.3 Mounting facilities for securely installing the auxiliary VHF-FM portable radio in the cockpit in accordance with the FAA AC 43.13-2B specifications. Locate and arrange the mounting facilities so that a seated observer/copilot has full and unrestricted movement of the radio's controls, without interference from the 18-inch adapter cable, clothing, cockpit structure, or flight controls.

B7.3.4.4 Positive-polarity microphone excitation voltage provided to the AUX-FM system from the aircraft DC power system through a suitable resistor network. A blocking capacitor must be provided to prevent the portable radio microphone excitation voltage from entering the system. Sidetone for the AUX-FM must also be provided (NAT model AA34-300, Premier model PA-34, or equivalent).

B7.3.4.5 The Contractor must provide an auxiliary FM adapter cord assembly to interface the connectors and circuits necessary to operate the BK KNG-P150/KNG-P150S/KNG2-P150 radio through the MS 3112E-12-10S connector in the aircraft. The FS/OAS drawing A-15 in Exhibit 6 is provided as one possible interface.

B7.3.4.6 In lieu of the above AUX-FM requirements, the Contractor may substitute an additional VHF-FM aeronautical transceiver (FM-3) which meets the requirements for the VHF-FM aeronautical transceiver(s) as detailed above.

B7.3.5 Automated Flight Following (AFF) Program B7.3.5.1 One satellite-based aircraft tracking hardware for each aircraft offered, compatible with the government’s 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 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 always tracked in these locations. 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.

B7.4. Navigation Systems – VFR GPS Systems B7.4.1 At least one of the following VFR navigations systems must be installed:

B74.1.1 One permanently installed, panel-mounted GPS system utilizing an approved, fixed external aircraft antenna. The navigational databases must be updated at least annually.

B7.4.1.2 One portable Aviation GPS unit (Garmin GPS 660 or 760 etc..) utilizing aviation-based software providing overhead orientation. Unit must be connected to remote antenna separate from GPS unit. Navigational databases must be updated at least annually.

B7.4.1.3 One tablet or mobile device, minimum size of 3.0 inches wide x 1.5 inches high, utilizing aviation application software (Foreflight, Gamin Pilot etc..) that incorporates overhead orientation and georeferencing of aircraft position on the map. The display must show aircraft position in relation to airspace boundaries, including military, controlled, and restricted areas. Application software must allow for disabling of internal GPS sourcing and allow for sourcing of external remote GPS antenna signal. Application software subscription must be current.

B7.4.2 All GPS systems must allow for continuous application of aircraft electrical power through circuit protected source.

B7.4.3 All GPS Systems must use WGS-84 datum and reference latitude and longitude coordinates in degrees, minutes, decimal minutes mode.

B7.4.4 All GPS Systems must ensure secure mounting and shall be located in a position to provide the PIC a clear view of aircraft panel and the unit display and unrestricted access to aircraft and unit controls.

B7.4.5 Portable Aviation GPS units, GPS tablets, or mobile GPS device systems will not be used for aircraft primary navigation in aircraft conducting IFR operations.

B7.4.6 All GPS Systems must be able to display, in real time the GPS tracks of all flights. This data must be transferable to the Government upon request by the Government. All transferred data must include the date of each flight, along with a graphical overlay of the flight track on an aeronautical chart covering the area of operations.

B7.4.7 Reserved B7.4.8 For panel mounted GPS display only. The display may also be configured to display the TCAS/TAS/TCAD data described in B7.6.2.

B7.4.9 The aircraft must be equipped with the navigational equipment required for IFR operations as specified in 14 CFR 135.165, including, but not limited to, the following:

B7.4.9.1 Two VHF, VOR/LOC aeronautical navigation receivers with indicators (NAV-1, NAV-2), each with a minimum of 100 navigation receive channels.

B7.4.9.2 One glideslope (GS) system, with a minimum of 40 receive channels.

B7.4.9.3 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.

B7.4.5 One 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 GPSs above are operable.

B7.4.6 One Distance Measuring Equipment (DME) system, with a minimum of 200 channels.

B7.4.7 One Horizontal Situation Indicator (HSI) or equivalent digital instrument system. The CDI must be interfaced to other aircraft systems to display VOR/LOC and GPS information on the CDI.

B7.4.7 One Horizontal Situation Indicator (HSI) or equivalent digital instrument system., which is fully integrated to the autopilot, equipped with a Course Deviation Indicator (CDI) which provides selection of both VOR/LOC or GPS information.

B7.4.8 One 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.

B7.4.9 Three-axis auto-pilot system, integrated with the HSI One Horizontal Situation Indicator (HSI) or equivalent digital instrument system as required by B7.4.7.

B7.5 Audio Systems B7.5.1 Three audio control systems must be provided for use by the pilot, observer/copilot and the two aft spotters. Each system must provide separate controls for selection of receiver audio outputs and transmitter microphone/PTT audio inputs for all installed transceivers, the ICS, and PA systems. Each system must also provide separate audio level controls for adjustment of both the ICS and the receiver audio output levels.

B7.5.1.1 Transmitter selection and operation. Separate transmitter selection controls must be provided for the microphone/PTT inputs at each of the three stations. The systems must be configured so that each of the three users may simultaneously select and utilize a different transmitter or the PA system via their respective microphone/PTT. Whenever a transmitter is selected, the companion receiver audio must 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 each user to select audio from one or any combination of available receivers. 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 controls of the audio system(s) must be located and arranged so that each user when seated, has full and unrestricted movement of each control without interference from their clothing, the aircraft 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, observer/copilot, and all aft cabin 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, PTT's, 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 type M87/AIC with CE 100 TR preamplifier, or equivalent) must be furnished at all required positions.

B7.5.3.1 Reserved.

B7.5.3.2 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.

B7.5.3.3 Push-to-talk (PTT) operation: separate PTT switches must be provided for radio transmitter and ICS microphone operation at the pilot, copilot/observer, and each of the two aft spotter positions. The pilot's PTT switches must be mounted on the control yoke. NOTE: PTT switches other than those mounted on the flight controls must be furnished at the copilot/observer position. The PTT switches for each of the two spotter positions must be mounted on the cord to the earphone/microphone connector. A cord of coiled construction, capable of stretching to a length of 20 feet, must be furnished for use at one spotter position. The Contractor must furnish an additional spare PTT switch/cord assembly for the spotter positions.

B7.5.3.4 Public Address (PA) system. The pilot, copilot/observer, and spotters 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 include the following:

e) An amplifier with output adequate to convey intelligible messages to all cabin occupants, including fully outfitted smokejumpers, while in flight at cruise speed with open jump door.

f) One or more cabin speakers, as necessary.

g) 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.

h) A PA audio level control at the spotter position 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 91.215 (a) and (b) and inspected and tested every 24 months in accordance with 14 CFR 91.413.

B7.6.2 The aircraft must be equipped with an FAA Technical Standard Order (TSO) approved traffic awareness and avoidance system (TCAS/TAS/TCAD/etc.) 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 enter 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 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.

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.

B7.6.2.2 The following systems are known to meet the above requirements:

TCAS: Any TSO’ d system which provides a range selection of 2 nautical miles or less.

TAS: Bendix-King KTA 870, Goodrich Skywatch HP TCAD: Avidyne TAS600/605/615/620 (formerly Ryan International TCAD 9900BX) only when a separate, approved Multi-Function Display (MFD) is used to display threat aircraft data.

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.

B7.6.3 Reserved B7.6.4 Reserved B7.6.5 Terrain Awareness and Warning System (TAWS). Any aircraft furnished must be equipped with a TAWS meeting, as a minimum, the requirements specified in 14 CFR 91.223 for six to nine passenger seats, regardless of any exceptions for status as a Public Aircraft operation or firefighting operation. Additionally, the system must be equipped with a feature, selectable or de-selectable in flight, which inhibits the system’s aural warning.

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, use diversity antennas on both the top and bottom of the aircraft, 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.

B7.6.7 Each aircraft must be equipped to meet the Radar Altimeter (RAD ALT) requirements of 14 CFR 135.160, where applicable. Radar Altimeter (RAD ALT), indicator must display of a minimum of from 20 to 2000 feet, variable decision height selection, and both visual (indicator light) aural (via the audio control systems) alert of arrival at decision height.

B7.6.8 The aircraft must be equipped with one permanently installed circuit breaker-protected, dual USB charging port for powering Electronic Flight Bags (EFBs), GPS devices, tablets, etc. The ports must be approved under TSO-C71, each be equipped with USB-A connectors, each providing a maximum of 2.1A power at 5VDC and mounted in a location convenient to the pilot and copilot/observer positions. (Cigarette lighter adapter is not acceptable).

B8 Reserved

PERSONNEL REQUIREMENTS

B9 Pilot Requirements B9.1 The Contractor must furnish a flight crew for each day the aircraft is required to be available. A flight crew is one pilot-in-command (PIC) and, if required by the aircraft offered, one second-in-command (SIC).

B9.2 The PIC must be familiar with this contract and all applicable task orders issued under this contract.

B9.2.1 The PIC must be able to provide contract and/or task order information to the COTR, OAS inspector, COR, project inspector (PI), or Government manager as requested.

B10 Pilot Qualifications B10.1 General.

Pilot flight hours will be verified from an employer certified pilot log. Further verification of flight hours may be required at the COR’s discretion.

B10.2 Minimum Qualifications.

The Contractor must provide a pilot(s) who meets the following minimum qualifications and who possesses the required certificates and evidence of having satisfactorily passed the evaluations for the required tasks:

B10.2.1 An FAA commercial pilot certificate or higher with airplane category, appropriate class(es) and instrument rating for offered airplane.

B10.2.2 A minimum of a current second-class medical certificate, issued in accordance with 14 CFR Part 67.

B10.2.3 A current FAA competency check completed in accordance with 14 CFR 135.293(a and b) in the same make and model as the contract aircraft, a current 14 CFR 135.299 line check, and a current 14 CFR 135.297 instrument proficiency check or 14 CFR 121 equivalents.

B10.2.4 Pilots assigned as PIC must have previously possessed an interagency smokejumper and paracargo pilot-in-command card or demonstrate proficiency to an interagency Inspector Pilot. Smokejumper pilots are required to demonstrate to an interagency Inspector Pilot, per the Interagency Airplane Pilots Practical Test Standards Guide, their proficiency annually and prior to being accepted as pilot-in-command. The flight evaluation will be in an aircraft supplied by the Contractor, at no expense to the Government. The satisfactory completion of the evaluation flight will not substitute for any of the total flight hour requirements listed in this contract. Pilots without previous smokejumper and paracargo experience may be qualified for smokejumper and paracargo missions by accomplishing the SMJ PIC trainee requirements.