D15PS00165_-_EU_Helicopter_NPS.docx

SECTION E – REPRESENTATIONS AND CERTIFICATIONS

Table of Contents

SECTION A - REQUIREMENTS AND PRICES

SECTION A – REQUIREMENTS AND PRICES

CONTRACT ACRONYMS

SECTION A – REQUIREMENTS AND PRICING

SCHEDULE OF SUPPLIES/SERVICES

A1. ITEM REQUIREMENT:

The intent of this contract is to obtain a fully Contractor operated and maintained exclusive use helicopter for 120 calendar days to support project/resource work, fire management and search and rescue for the National Park Service and other agencies in the Pacific Northwest to include, but not limited to: Mount. Rainier, Olympic and North Cascade National Parks. This contract has a Base Year with four 1-year Option Years.

ITEM DESCRIPTION

1. Aircraft Required: One light helicopter

Crew Compliment Required: Pilot-in-Command (PIC) with relief pilot, fuel service vehicle driver with relief driver, and mechanic with relief mechanic. The Contractor may provide a mechanic that is also the fuel service vehicle driver.

Fuel Servicing Vehicle Requirement: Each item: One vehicle equipped as specified in Section B8.

Additional Fuel Trailer Requirement: An additional fuel cache trailer is required for this contract. This is in addition to fuel truck required (See B8.5)

Minimum Helicopter Requirements:

Seating: Five (5) insured passenger seats not including pilot, but including copilot seat in an aircraft, normally single-pilot operated.

Payload: Non-jettisonable payload (HOGE) of 450 pounds at 0 degrees Celsius at 14,000 feet pressure altitude using a pilot weight of 200 pounds, a 25-pound survival kit and fuel for 40 minutes of flight plus 20 minutes reserve.

Powerplant: Turbine engine

Certification Basis: 14 CFR 27

Airspeed: 155 knots Vne at sea level

Landing gear: Skid Type

(Payload amounts shall be computed by using the Government’s Standard Interagency Load Calculation Method and Form and the Helicopter Fuel Consumption and Weight Reduction Chart included under Section B Exhibits along with the offered aircraft’s applicable Hover Ceiling Charts, weight and balance report and equipment list that you provide).

An AS350B3 or equivalent may typically fulfill the above minimum and/or target requirements.

NOTE: All Exhibits applicable to this solicitation are included at the end of Section C.

A2. ITEM 1 – PRICING

(Complete shaded areas only)

DESIGNATED REPORTING BASE:

Mount Rainier Helibase

EXCLUSIVE USE PERIOD

120 calendar days

EXCLUSIVE USE PERIOD:

May 14, 2015 to September 09, 2015

OFFEROR NAME

AIRCRAFT FOR THIS

PRICING SCHEDULE

Make/Model

FAA Registration #

CONFIRMED

PAYLOAD

Aircraft payload is an element of your offer and will be confirmed by the Government that the payload shown ABOVE can be achieved at the solicitation’s minimum aircraft requirement. The confirmed payload will be made a part of the awarded contract and will be verified by DOI Aviation Management inspectors during inspection of the aircraft.

CLIN

DESCRIPTION

PAY ITEM

CODE

QUANTITY

UNIT

UNIT PRICE

EXTENDED AMOUNT

2015 – BASE YEAR – Exclusive Use Period - May 14, 2015 through September 09, 2015

1a

Daily availability (guaranteed)

AV

DAYS

1b

Flight time (estimated)

FT

FLIGHT

HOURS

As requested by the COR to be located at Marblemount WA. (C8.5.2)

1d

see schedule

NTE

$ 13,364.00

1e

MUTUAL EXTENSION

(OPTIONAL) Price per day for AVAILABILITY During Extension Period (C21)

AV

NTE

DAYS

same as 1a

1f

MUTUAL EXTENSION

(OPTIONAL) Price per FLIGHT HOUR During Extension Period

FT

EST

FLIGHT

HOURS

same as 1b

2015 – ITEM 1 ALL ITEMS - ESTIMATED TOTAL COST

Complete shaded areas only. Evaluation of options shall not obligate the Government to exercise the option(s).

DESCRIPTION

PAY ITEM

CODE

QUANTITY

UNIT

UNIT PRICE

PAY ITEM

CODE

QUANTITY

UNIT

UNIT PRICE

2016 – 1st Option Year – Exclusive Use Period - May 14, 2016 through September 09, 2016

2a

AV

DAYS

2b

FT

FLIGHT

HOURS

As requested by the COR to be located at Marblemount WA. (C8.5.2)

2d

see schedule

NTE

2e

MUTUAL EXTENSION

same as 2a

2f

MUTUAL EXTENSION

FLIGHT

HOURS

same as 2b

2016 – ITEM 1 ALL ITEMS - ESTIMATED TOTAL COST

Complete shaded areas only. Evaluation of options shall not obligate the Government to exercise the option(s).

DESCRIPTION

PAY ITEM

CODE

QUANTITY

UNIT

UNIT PRICE

2017 – 2nd Option Year – Exclusive Use Period - May 14, 2017 through September 09, 2017

3a

AV

DAYS

3b

FT

FLIGHT

HOURS

As requested by the COR to be located at Marblemount WA. (C8.5.2)

3d

see schedule

NTE

3e

MUTUAL EXTENSION

same as 3a

3f

MUTUAL EXTENSION

FLIGHT

HOURS

same as 3b

2017 – ITEM 1 ALL ITEMS - ESTIMATED TOTAL COST

Complete shaded areas only. Evaluation of options shall not obligate the Government to exercise the option(s).

DESCRIPTION

PAY ITEM

CODE

QUANTITY

UNIT

UNIT PRICE

2018 – 3rd Option Year – Exclusive Use Period - May 14, 2018 through September 09, 2018

4a

AV

DAYS

4b

FT

FLIGHT

HOURS

As requested by the COR to be located at Marblemount WA. (C8.5.2)

4d

see schedule

NTE

4e

MUTUAL EXTENSION

same as 4a

4f

MUTUAL EXTENSION

FLIGHT

HOURS

same as 4b

2018 – ITEM 1 ALL ITEMS - ESTIMATED TOTAL COST

Complete shaded areas only. Evaluation of options shall not obligate the Government to exercise the option(s).

DESCRIPTION

PAY ITEM

CODE

QUANTITY

UNIT

UNIT PRICE

2019 – 4th Option Year – Exclusive Use Period - May 14, 2019 through September 09, 2019

5a

AV

DAYS

5b

FT

FLIGHT

HOURS

As requested by the COR to be located at Marblemount WA. (C8.5.2)

5d

see schedule

NTE

5e

MUTUAL EXTENSION

same as 5a

5f

MUTUAL EXTENSION

FLIGHT

HOURS

same as 5b

2019 – ITEM 1 ALL ITEMS - ESTIMATED TOTAL COST

TOTAL ESTIMATED COST ITEMS 1 THRU 5 (BASE YEAR W/FOUR OPTION YEARS)

A3. ADDITIONAL PAY ITEMS

SUB-ITEM

PAY ITEM CODE

QUANTITY

UNIT

UNIT PRICE

(1) Funding will not be obligated under the contract. Each year the Contracting Officer will issue an order for aircraft services for the obligation of funds during the exclusive use period. Any extensions to an order’s exclusive use period and obligations of additional funding will be accomplished under modifications to an order.

(2) The Minimum Guarantee under the contract, as required by contract clause 52.216-22, is the total amount for Daily Availability during the Exclusive Use Period under the first year’s task order; however, the guaranteed quantity for daily availability is subject to reductions due to unavailability (see C28). The estimated quantity for daily availability during an extension of the exclusive use period is not guaranteed and also is subject to reductions due to unavailability.

(3) The start for services may be changed by the issuance of a Notice-to-Proceed letter in accordance with paragraph C22.

THIS PAGE FOR GOVERNMENT USE ONLY – PLEASE DO NOT COMPLETE

This section will be completed at time of award and again when fuel adjustments are made

Requested and Effective Date This Adjustment

Type Aircraft

|X| Jet Fuel |_| Av Gas

Fuel Source Location

Pierce County Airport-Thun Field, Renton, or Olympia

(Self-Service) Base Price

$ x.xx (includes Tax)

Reference Price

Effective Date

Upon Award

Source Document

ORIGINAL CONTRACT

Source Document

Difference

$ X consumption rate of

Increase Due

Old Flight Rate

New Flight Rate

Re-established Base Price

SECTION B – TECHNICAL SPECIFICATIONS

GENERAL REQUIREMENTS

B1 Scope of Contract

B1.1 The intent of this contract is to obtain fully Contractor operated and maintained exclusive use helicopter flight services to transport personnel and/or cargo in support of Government natural resource missions. Contractor services include provision of a helicopter, personnel, fuel servicing vehicle, fuel, and all other associated equipment as prescribed in this solicitation. Missions will include, but are not limited to, short-haul, search and rescue, STEP (single-skid, toe-in, hover entry/exit procedures) landings, fire suppression, fire monitoring, initial attack, prescribed fire and aerial ignition, law enforcement limited to nonthreatening surveillance and reconnaissance, and other administrative and related resource activities. The Government will direct aircraft to support its missions and objectives.

B1.2 Law enforcement missions include but are not limited to, transporting Federal personnel to a law enforcement location, short-haul into grow sites, low-level reconnaissance or surveillance flying, and prisoner transport. Law enforcement officers will fly with loaded firearms on-board the aircraft and may enter areas of potential contraband activity. Firearms will be transported in accordance to policy and guidance contained in the IHOG and Interagency Aviation Transport of Hazardous Material. The pilot and air crew will jointly conduct risk assessments for all missions to determine the risk and hazards. No mission will be flown that presents a high level of risk.

B1.3 During the exclusive use period and any subsequent extension, aircraft furnished shall be subject to the exclusive use and control of the Government 24 hours per day, 7 days per week.

B1.4 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 accomplishment of the mission and aviation safety are an integral element of this relationship.

B1.5 The Government has interagency and cooperative agreements with other Federal and State agencies and private landholders and may dispatch aircraft under this contract for such cooperative use.

B2 Certifications

The Contractor must hold and keep current all of 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 Federal Aviation Administration (FAA) Air Carrier 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., rotorcraft, visual flight rules (VFR) day/night, passengers, and cargo).

B2.2 A Title 14 of the Code of Federal Regulations (CFR), Part 135 Air Carrier certificate. These 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 A 14 CFR, Part 133, "Rotorcraft External Load Operations" certificate which authorizes Class B loads, as a minimum.

B2.4 A 14 CFR, Part 137, "Agricultural Aircraft Operations" certificate.

B2.5 The contract aircraft must have a Standard Airworthiness certificate. Installation of any equipment required by this contract must be FAA-approved.

B3 Order of Precedence (Specifications)

In the event of inconsistencies within the technical specification, the following order will be used in such resolution: (1) typed provisions of these specifications; (2) DOI Office of Aviation Services (OAS) supplements and/or exhibits incorporated by reference; (3) 14 CFR incorporated by reference; (4) aircraft manufacturer's specifications; and (5) other documents incorporated by reference.

B4 Contracts

B4.1 The Contractor must maintain a complete, current printed copy of the contract and all contract modifications 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. Following receipt of a printed task order, the pilot will carry a hard copy of the task order in the aircraft.

B4.3 Electronic copies of contracts and task orders may be used, however an electronic copy of the contract does not cancel the requirement to keep a printed copy of the contract and contract modifications in the aircraft.

EQUIPMENT REQUIREMENTS

B5 Condition of Equipment

The Contractor-furnished helicopter, fuel servicing vehicle, and all other required equipment must be operable, free of damage, and in good repair. Aircraft systems and components must 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 lap belt and shoulder harness conditions that are not acceptable.

B5.4 Military or other similar low visibility paint schemes are unacceptable. The Contracting Officer’s Technical Representative (COTR) may approve high visibility enhancements.

B6 Aircraft Equipment Requirements

The Contractor must provide one fully compliant helicopter that is equipped as shown below for each item:

B6.1 A complete set of current aeronautical charts covering the expected area of operations.

B6.2 One digital hour meter installed in a location visible by the pilot and front seat observer while seated. The meter must be wired in series with a switch on the collective control, and a switch activated by engine or transmission oil pressure or by equivalent means, to record flight time only.

B6.3 Free air temperature gauge.

B6.4 One set of individual lap belts for each installed seat.

B6.5 Double strap shoulder harness with automatic or manual locking inertia reel for each front seat occupant. Shoulder straps and lap belts must fasten with one single-point metal-to-metal, quick-release mechanism. Heavy-duty (military-style) harnesses with fabric loop connecting the shoulder harness to the male portion of the lap belt buckle are acceptable.

B6.6 Shoulder harnesses equipped with inertia reel (either single-strap or double-strap) for each aft cabin occupant. Shoulder harness straps and lap belts must fasten with a single-point, metal-to-metal, quick-release mechanism.

B6.7 Fire extinguisher(s), as required by 14 CFR, 135, must be a handheld bottle, minimum 2-B:C rating, mounted and accessible to the flight crew while seated. (See the fire extinguisher maintenance instructions in Section B29.)

B6.8 Dual controls for initial pilot performance evaluation. (May also be required for interim or recurrent pilot performance evaluations at the option of the Government.)

B6.9 Aircraft lighting for night operation in accordance with 14 CFR 91.205(c), including instrument lights.

B6.10 A strobe light (with either a white, or half-white/half-red lens) or a flashing LED (red or white), mounted on top of the aircraft or otherwise visible from above, with an independent activating switch. A red strobe or rotating beacon does not satisfy this requirement.

B6.11 High visibility, pulsating, forward-facing, conspicuity lighting.

B6.12 High visibility markings on main rotor blades as specified by the Acceptable Paint Schemes Exhibit.

B6.13 High-skid-type landing gear if manufactured for make and model.

B6.14 Personnel access steps for aircraft with a floor height greater than 18 inches to ensure safe entrance and exit from each door.

B6.15 Locking cap(s) on all fuel inlet ports.

B6.16 Cabin heater and window defogger.

B6.17 Wire strike protection system (mechanical). (Note: If manufactured for the make and model of helicopter.)

B6.18 Main rotor brake.

B6.19 Snow/tundra pads (Note: To be installed when requested by the Government.)

B6.20 Internal Litter Kit (Note: Litter to be installed and/or removed when requested by the Government.)

B6.21 Cargo compartment, internal and external capable of accommodating 58-inch long shovels, rakes, and other tools as specified below:

For internal:

B6.21.1 15-cubic-foot baggage compartment within the aircraft fuselage specifically designed to carry cargo separate from the cabin. (Note: Requires rear bulkhead modification required on some models of aircraft.)

For external:

B6.21.2 Cargo basket. An externally side-mounted basket constructed with tubular frame and expanded metal incorporating a locking lid to secure cargo. Basket/rack must be quick attach/detach. All construction methods must be as prescribed by Advisory Circulars 43.13-1B and 43.13-2B or other FAA approval.

Note: AS350 aircraft must be equipped with a cargo basket such as the Dart Heli-Utility basket model D350-607-045 (57”length) or equivalent.

B6.22 Cargo restraint system for aircraft manufactured with a parcel/storage area behind the rear passenger seats.

B6.23 An accessory power source consisting of an MS 3112E-12-3S three-pin connector, accessible in the aft cabin. Pin B must be airframe ground; pin A must be +28VDC (for 28-volt aircraft); and pin C must be +14VDC (for 14-volt aircraft). The circuit must be protected by a 5-amp circuit protection.

B6.24 A first aid kit containing items specified in the First Aid and Survival Kits Exhibit (see Section C) must be carried aboard the aircraft on all flights.

B6.25 A survival kit containing items specified in First Aid and Survival Kits Exhibit (see Section C) must be carried aboard the aircraft on all flights and must be included in weight and balance/load calculations.

B6.26 A convex mirror for the pilot to observe the sling load.

B6.27 One keeperless cargo hook (On-Board Systems keeperless cargo hook or equal) that may be loaded and locked in a single motion with one hand and is rated at the maximum lifting capacity of the aircraft. This hook shall incorporate both an electrically activated release and a secondary mechanically activated release. The electric release shall be activated by a switch on the cyclic. The switch must be guarded/protected to minimize the possibility of inadvertent activation. The secondary mechanical release must incorporate a hydraulically activated release if available for the make and model of helicopter. (See the cargo hook maintenance requirements in Section B29.)

B6.28 Cockpit-mounted external load indicator with readout of weight carried on the cargo hook.

B6.29 One collapsible, variable capacity water/retardant bucket. See the Water Bucket Use Procedures Exhibit (see Section C). The bucket must have a manufacturer's capacity adjustment commensurate with the maximum lifting capability (HOGE-J) of the contract aircraft at 5,000 feet pressure altitude (PA), 30˚ Celsius with a 200-pound pilot, 25-pound survival kit, and 1.5 total hours of fuel. The bucket must be capable of being operated with all increments of the longline; i.e., 50, 100, 150 feet.

B6.30 A second collapsible, variable capacity water/retardant bucket. See the Water Bucket Use Procedures Exhibit (see section C). The bucket must have a manufacturer's capacity adjustment commensurate with the maximum lifting capability (HOGE-J) of the contract aircraft at 9,000 feet PA, 20˚ Celsius with a 200-pound pilot, 25-pound survival kit, and 1.5 total hours of fuel. The bucket must also be capable of being operated with all increments of the longline; i.e., 50, 100, 150 feet.

Note: The bucket combinations provided in B6.29 and B6.30 must provide adjustments that allow the widest range of altitude/temperature combinations (subject to the limitations of the bucket manufacturer’s available sizes) for the maximum lifting capability of the helicopter beginning at 5,000 feet PA at 30˚ Celsius extending upward to 9,000 feet PA at 20˚ Celsius and above.

B6.31 A remote operating switch for the water/retardant bucket and/or remote hook clearly marked for "open" and "closed" and mounted on the collective control to avoid confusion with the airframe cargo hook release. The switch must be of a different design and must be mounted so as to not easily be confused with the RPM Control [Beep Range] switch.

B6.32 Part number MS 3101E-24-11S, nine-pin connector, for use as the power source for a helitorch or remote cargo hook. Pin D must be airframe ground. Pin E must be switched 28VDC, protected by a manually operable, 50-amp circuit breaker. The water bucket/tank open switch must also activate this circuit.

B6.32.1 A lanyard to support the connector and mounted within 12 inches of the cargo hook.

B6.32.2 This connector must have multiple circuit capacity sufficient to provide power and control for Contractor-furnished equipment. The longline remote hook, fixed tank, or water bucket must be wired through this connector. A list of water buckets with required pin wiring can be found in the USDA Forest Service/DOI OAS Drawing A16 Exhibit (see Section C). Wiring diagrams for various equipment configurations are available from the U.S. Department of the Interior, Office of Aviation Services, 300 E. Mallard Drive, Suite 200, Boise, ID 83706, or USDA Forest Service, 3833 S. Development Avenue, Boise, ID 83705-5354.

B6.33 One remote cargo hook with related cabling and release system complying with the following specifications:

B6.33.1 Electrically activated remote cargo hook that may be loaded and locked in a single motion with one hand and that is rated at the maximum lifting capacity of the aircraft.

B6.33.2 The remote hook must be protected by a metal ring or cage that does not interfere with the use or function of the hook.

B6.33.3 Synthetic rope meeting the requirements of the Helicopter Synthetic Longline Requirements Exhibit (see Section C).

B6.33.4 Three ropes are required; one each in 50, 100 and 150 foot lengths.

B6.33.5 Electrical cables must be protected from pinching by hooks or shackles and from damage caused by stretching of the line. The electrical wire must be long enough at the aircraft cargo hook end to prevent a swinging load from unplugging the electrical connector.

B6.33.6 All fabrication and installation methods must comply with 14 CFR 133 and Advisory Circular 43.13–1B.

B6.33.7 Operating switch for the remote hook. (See B6.31 for specification. Only 1 switch required)

B6.34 Short-haul configuration. Helicopter to be equipped for short-haul operations that must meet the following specifications:

B6.34.1 Sliding or hinged door on side which can be opened while in flight. Door locks shall be provided to ensure that the door remains in closed and open positions. Doors may also be removed from the helicopter to meet these requirements provided the aircraft manual authorizes such removal.

B6.34.2 Windows available for the spotter to view the surrounding area without the necessity of opening doors.

B6.34.3 Capability for installation of a Government provided secondary external load safety retainer manual release for a Government owned and provided secondary short-haul retainer. The manual release lanyard, a steel sheathed Teleflex cable, will be secured and routed from adjacent to the cargo hook to the cockpit for pilot activation. Movement of the cargo hook shall not inadvertently release the safety retainer. The release handle shall be located so as to be accessible to the pilot-in-command (PIC), not interfere with pilot operations, and the system cannot be inadvertently activated.

B6.34.3.1 The Contractor shall ensure that the Government-furnished property is installed for short-haul activities and ensure any modifications and/or installations to the helicopter shall be accomplished in accordance with the Contractor’s FAA air carrier or operating certificate.

B6.34.4 A Supplemental Type Certificated (STC’d) rappelling fixture (floor mounted) (used for short-haul spotter and aerial recon anchor) appropriate to the make and model offered. This anchor shall be maintained in accordance with the manufacturer’s instructions for continued airworthiness.

B6.35 Helicopter flooring must be light weight, not fabric, and easily cleaned. (Note: Bare metal floor with non-slip protective covering is permissible.)

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 from OAS Avionics, or the most recent list may be found online at: http://www.nifc.gov/NIICD/docs/avionics/FSAMD_A24E.pdf .

B7.2 Avionics Installation and Maintenance Standards

B7.2.1 Strict adherence to the recommendations in the following FAA Advisory Circulars is required: AC 43.131B Chapter 11, "Aircraft Electrical Systems," and Chapter 12, "Aircraft Avionics Systems”; AC 43.132B 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.

B7.3 Communications Systems.

B7.3.1 One automatic-portable/automatic-fixed or automatic-fixed Emergency Locator Transmitter (ELT) certified to either Technical Standard Order (TSO)-C91a or TSO-C126, installed per the ELT manufacturer’s instructions in a conspicuous or marked location, and meeting the same requirements as those detailed for airplanes in 14 CFR, Part 91.207 (excluding section f). ELT antennas must be mounted externally to the aircraft unless installed in a location approved by the aircraft manufacturer. TSO-C126 and newer (406 MHz) ELTs must include a 121.5 MHz homing beacon, and 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.

B7.3.3 One P25-compliant VHF-FM transceiver. The transceiver (FM-1), must provide selection of narrowband analog (12.5 kHz), wideband analog (25.0 kHz), or narrowband digital (12.5 kHz) operation on each of a minimum of 100 channels. The 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 clothing, the cockpit structure, or the flight controls.

B7.3.3.1 The 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. The 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 the transceiver must be 10 watts nominal value (original design specification). The 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, the 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.

B7.3.4 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/AMD-17 in the exhibits.

B7.3.4.2 One weatherproof, external, broadband antenna covering the 150174 MHz band, with associated RG58A/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 CI177 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 In lieu of the above AUX-FM requirements, the Contractor may substitute an additional VHF-FM aeronautical transceiver (FM-2) which meets the requirements for the VHF-FM aeronautical transceiver(s) as detailed above.

B7.3.5 One satellite-based aircraft tracking hardware compatible with the government’s Automated Flight Following (AFF) Program (https://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. For questions about current compatibility requirements contact the AFF Program Manager listed under contacts at: https://www.aff.gov.

B7.3.5.1 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.

B7.3.5.2 AFF communications must be fully operational in all 50 states. 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.

B7.3.5.3 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 contact the Government of system changes, scheduled maintenance, and planned service outages.

B7.3.5.4 Registration contact information, a web accessible feedback form, and additional information is available at: https://www.aff.gov. The Fire Applications Support Desk (FASD) can be reached at (866) 224-7677 or (360) 326-6002.

B7.3.5.5 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 (indicating it is currently transmitting data to AFF) and that all information displayed in AFF is current. A username and password are required to access AFF. Log on to the AFF website at https://www.aff.gov to request a username and password, or contact the FASD.

B7.3.5.6 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.

B7.3.5.7 This clause incorporates Specification Section Supplement available at: https://www.aff.gov/contractspecs with the same force and affect as if they were presented as full text herein.

B7.4 Navigational Systems.

B7.4.1 One permanently installed, panel-mounted global positioning system (GPS-1) utilizing an approved, fixed external aircraft antenna and powered by the aircraft electrical system or an aviation portable GPS unit (Garmin GPS Map 296/396/496 or equivalent) provided the portable unit is securely mounted, is equipped with a remote (i.e., not part of the GPS unit) antenna, and presents information from an overhead orientation (not a drive-along-the-road type), and is powered by the aircraft electrical system. The GPS (permanently installed or portable) must utilize the WGS-84 datum and reference latitude and longitude coordinates in the degrees/minutes/decimal minutes (DM) mode for aircraft positioning. The primary GPS must also have near real-time weather downlink capability.

B7.4.1.2 A GPS data port connector must be installed for the purposes of external data retrieval by a GIS laptop computer from the above GPS. The connector must be a DB-9F type D sub-connector, must be wired for RS-232C serial format for laptop computers (pin 2=transmit data, pin 3=receive data [if applicable], and pin 5=ground) and must be mounted in a location convenient to the front seat observer.

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 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.

B7.5.1.1.1 The two aft cabin exit positions must be equipped to transmit on the radio(s). Whenever a radio (or PA, when so equipped) microphone input is selected at the observer/copilot's audio control panel, the aft cabin passengers' radio microphone inputs must automatically be connected to the same radio, and they must then be capable of transmitting on that radio via their respective radio transmit PTT switches.

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, observer/copilot, and all aft cabin exit 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 50602, military dynamic type M87/AIC with type CE100 TR preamplifier, or equivalent) with U174/U (single/male) type connector plug. The pilot position only may be configured for low impedance (dynamic) operation.

B7.5.3.1 All earphone/microphone jacks in the aircraft (except the pilot's) must be U-92A/U (single/female) type, which will accept U-174/U type plugs.

B7.5.3.2 Separate PTT switches for radio transmitter and ICS microphone operation must be provided at the pilot, observer/copilot, and any other positions required above to be furnished with both radio transmitter and ICS operation. The pilot's PTT switches must be mounted on the cyclic control. The observer/copilot's and any other required position’s PTT switches must be mounted on the cord to the earphone/microphone connector. The aft cabin positions must be furnished with cord-mounted ICS PTT switches.

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 One APCO Project 25 compliant (P25) VHF-FM "multi-mode" two-way mobile radio, with a matched broad-band antenna, must be mounted in the fuel-servicing vehicle. The radio's operational bandwidth must include the 150 MHz to 174 MHz frequency band, with user-programmable (in the field) channels. Selection of wideband (25.0 kHz) analog, narrowband (12.5 kHz) analog, or digital (12.5 kHz) spacing is required on each channel. The radio must be frequency-synthesized, equipped with the lowest 32 CTCSS sub-audible tones, and must develop a minimum of 30 watts carrier output power. Use of appropriate portable VHF-FM radios with suitable output power booster units is permissible.

The following radio models are known to meet the above requirements:

Datron G25RMV100, G25RMV110, G25ASU001 Kenwood TK-5710, TK-5720 Midland STM-1050B, STM-1055B, STM-1115B Relm(BK) Radio: DMH5992 with Smartmic, DMH5992X HP with…