HI_Helo_On-Call_140D8121R001_Re-Open_7_09_2024_0004.docx

Table of Contents

SECTION A – REQUIREMENTS AND PRICES

CONTRACT ACRONYMS

Officials

Procedures

SCHEDULE OF SUPPLIES/SERVICES

A1. General Information

This multiple award indefinite delivery/indefinite quantity type contract is for On Call Turbine and/or Small Reciprocating Engine Helicopter Services on an as needed basis for transportation of Government personnel, cargo, or both using aircraft operated and maintained by the Contractor. Services under this contract are limited to those operators who are authorized to conduct flight services in Hawaii and maintain a Hawaii Base of Operations.

A2. Item Requirement

All equipment, facilities, and personnel required under this contract shall be delivered to and removed from various location(s) as ordered and needed. Contractor designated base location(s) are identified on the following pricing pages.

Aircraft Requirement:

Small helicopters (12,500-pound or less certified maximum gross weight) equipped as specified in Section B; plus, any additional mission specific requirements (if offered) as listed in the exhibits.

Crew Requirements:

Pilot-in-Command (PIC).

Minimum Helicopter Requirements (see item descriptions 1-8 for specific performance and seating)

HOGE-J For turbine engine helicopters offered: Payload calculations for the item descriptions below shall be computed using a pilot weight(s) of 200 pounds, a survival kit weight of 25 pounds and a total fuel load for 1.5 hours of flight at 5,000 feet PA with a temperature of 30 degrees Celsius.

HOGE-J For reciprocating engine helicopters offered: Payload calculations for Item 8 below shall be computed using a pilot weight(s) of 200 pounds, a survival kit weight of 25 pounds and a total fuel load for 1.5 hours of flight at 2,000 feet PA with a temperature of 20 degrees Celsius.

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 the Exhibits (see Section C) along with the offered aircraft’s applicable Hover Ceiling Charts, weight and balance report, and equipment list that you provide. NOTE: Refer to the ACETA Exhibit 12 for performance requirements when offering ACETA capability.

Small or medium turbine engine helicopters such as the AS 350 Series, BH 206 series, R66, MD500 series, EC 130, BH 407, BH205, BH212, UH-1, or similar other models may fulfill the minimum requirements for items 2-7. A UH12E, BH-47G3B-1, BH47G3B-2, R-44 I or II or equivalent model may typically fulfill the minimum requirements for item 8. However, offerors should ensure their specific helicopter is capable of meeting the minimum requirements listed.

AIRCRAFT ITEM DESCRIPTIONS:

Item #1 Description Minimum Guarantee-Initial OAS Inspection/Test of Contractor Aircraft and Pilot(s).

Item #2 Description

Item #3 Description

Item #4 Description

Item #5 Description

Item #6 Description

Item #7 Description

Item #8 Description

SECTION A – SCHEDULE OF SUPPLIES/SERVICES

On-Call Helicopter Services for Hawaii 1 Solicitation 140D8121R0001

A3. Item 0001-0008 Pricing

Item #1 Description – Initial OAS Inspection/Test of Contractor Aircraft and Pilot(s). When the Government requires supplies or services covered by this contract, a minimum of one Government-provided inspection for aircraft and pilot as described in Section C2 will be provided. This line item is not separately priced and is the minimum quantity the Government intends to order (also known as the minimum guarantee) under any resulting contract(s) as required by Federal Acquisition Regulation (FAR) 16.504 and FAR 52.216-22.

Item #2 Description

OFFEROR ‘S

NAME:

BASE

OF OPERATION:

Each aircraft shall have only one pricing schedule (D4.3.2)

MAKE/MODEL/CONFIGURATION

(aircraft identified must be at the same rates)

FAA REGISTRATION

NUMBER

INSURED PAX SEATS

MINIMUM PAYLOAD

HOGE-J

N

N

N

HOUR

Standby Rate

SB

Standby Rate

Standby Rate

ACETA PROGRAM ITEMS, DEFINITIONS AND PROFILES – Please refer to ACETA Exhibit 12.

Item #3 Description

OFFEROR ‘S

BASE(s)

Each aircraft shall have only one pricing schedule (D4.3.2)

MAKE/MODEL/CONFIGURATION

(aircraft identified must be at the same rates)

FAA REGISTRATION

NUMBER

INSURED PAX SEATS

MINIMUM PAYLOAD

N

N

Standby Rate

Standby Rate

Standby Rate

Item #4 Description

equivalent.

in an aircraft normally single pilot operated.

OFFEROR ‘S

BASE(s)

Each aircraft shall have only one pricing schedule (D4.3.2)

MAKE/MODEL/CONFIGURATION

(aircraft identified must be at the same rates)

FAA REGISTRATION

NUMBER

INSURED PAX SEATS

MINIMUM PAYLOAD

N

N

Standby Rate

Standby Rate

Standby Rate

Item #5 Description

seat in an aircraft normally single pilot operated.

OFFEROR ‘S

BASE(s)

Each aircraft shall have only one pricing schedule (D4.3.2)

MAKE/MODEL/CONFIGURATION

(aircraft identified must be at the same rates)

FAA REGISTRATION

NUMBER

INSURED PAX SEATS

MINIMUM PAYLOAD

N

N

Standby Rate

Standby Rate

Standby Rate

Item #6 Description

OFFEROR ‘S

BASE(s)

Each aircraft shall have only one pricing schedule (D4.3.2)

MAKE/MODEL/CONFIGURATION

(aircraft identified must be at the same rates)

FAA REGISTRATION

NUMBER

INSURED PAX SEATS

MINIMUM PAYLOAD

N

N

Standby Rate

Standby Rate

Standby Rate

Item #7 Description

OFFEROR ‘S

BASE(s)

Each aircraft shall have only one pricing schedule (D4.3.2)

MAKE/MODEL/CONFIGURATION

(aircraft identified must be at the same rates)

FAA REGISTRATION

NUMBER

INSURED PAX SEATS

MINIMUM PAYLOAD

N

N

Base

Standby Rate

Standby Rate

Standby Rate

Item #8 Description

OFFEROR ‘S

BASE(s)

Each aircraft shall have only one pricing schedule (D4.3.2)

MAKE/MODEL/CONFIGURATION

(aircraft identified must be at the same rates)

FAA REGISTRATION

NUMBER

INSURED PAX SEATS

MINIMUM PAYLOAD

N

N

Standby Rate

Standby Rate

Standby Rate

A3.1 Funding will not be obligated under the Indefinite-Delivery Indefinite-Quantity (IDIQ) contract. The Contracting Officer will issue task orders for services which will obligate funding for the payment of aircraft services.

A4. Additional Pay Items Additional Pay Items Schedule (Reimbursed as Time & Materials IAW FAR 52.212.4 ALT1)

SCHEDULE SUB-ITEM

ADDITIONAL PAY ITEMS

PAY ITEM CODE

QUANTITY

UNIT

UNIT PRICE

(Per Diem)

Actual cost for lodging - receipt(s) required;

M&IE authorized daily rate

(averaged over length of hire)

Note: See Section C33 regarding Additional Pay Items. Receipts are required for verification of ALL claimed items, except for meals and incidentals when they are authorized.

FOR GOVERNMENT USE ONLY – DO NOT WRITE IN THIS AREA

Contracting Officer will complete at time of award and again when fuel adjustments are made Requested and Effective Date This Adjustment

Type Aircraft

|_| Jet Fuel |X| Av Gas

Base Price

$ 5.74

Reference Price

Effective Date

Contract Award

Source Document

ORIGINAL CONTRACT

Source Document

Difference

$ X consumption rate of

Increase/Decrease 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 on-call helicopter flight services to transport personnel and/or cargo in support of Government natural resource missions in Hawaii or the Commonwealth Area of the Pacific. Contractor services include provisions of a helicopter, personnel, and all other associated equipment, as prescribed in this solicitation. Missions will include, but are not limited to, fire management program support such as fire suppression, fire monitoring, initial attack, prescribed fire and aerial ignition, rehabilitation seeding, search and rescue (SAR), aerial capture, eradication and tagging of animals (ACETA), overwater, platform and vessel landings, and law enforcement limited to nonthreatening surveillance, and other administrative and related natural resource activities. The Government will direct aircraft to support its missions and objectives. During the availability period and any subsequent extension, aircraft furnished shall be subject to the exclusive use and control of 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 and State agencies and private landholders and may dispatch aircraft under this contract for such cooperative use.

B1.4 Aircraft furnished under this contract must be operated and maintained by the Contractor.

B1.5 Aircraft furnished under this contract must be subject to the exclusive use and control of the Government, 24 hours per day, 7 days per week throughout the periods specified under Section A when ordered. The aircraft must not be operated except as directed by the Contracting Officer or an authorized representative of the Contracting Officer.

B1.6 ACETA, Basic Fire, Offshore, Vessel Landings, and Extended Overwater flight activities are permitted under this contract if offered and awarded by the Government (see section C exhibits). Award will be discretionary by the Government.

B1.7 Operators who list a Hawaii or Commonwealth Area of the Pacific as their base of operations may be requested to perform within any of the Hawaiian Islands or Commonwealth Area of the Pacific.

B2 Certification

The Contractor must obtain 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 D085, "Aircraft Listing," as appropriate.(Note: Not applicable for aircraft issued a Restricted Airworthiness Certificate only.)

B2.3 A 14 CFR Part 133 "Rotorcraft External Load Operations" certificate which authorizes Class A and/or B loads, as a minimum.

B2.4 A 14 CFR Part 137 “Agricultural Aircraft Operations” certificate. (Required for all fire operations and any other operations conducted under part 137)

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

B2.6 The contractor must notify in writing OAS of any changes in the Director of Operations, Chief Pilot, and Director of Maintenance positions, plus any additional positions approved under 14 CFR 119.69(b).

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, OAS supplements and/or exhibits incorporated by reference; (3) 14 CFR incorporated by reference; (4) aircraft manufacturer's specifications; (5) other documents incorporated by reference.

B4 Contract Documents

B4.1 The Contractor must maintain a complete, current copy of the contract, all 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. However, the contractor is responsible for ensuring that the documents 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

B5.1 The Contractor-furnished helicopter(s) 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.

B5.2 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.

B5.3 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.

B5.4 See the Unacceptable Lap Belt and Shoulder Harness Conditions Exhibit (section C exhibits) for lap belt and shoulder harness conditions that are not acceptable.

B6 Aircraft Equipment Requirements

The Contractor must provide at least one small Reciprocating Engine, (not more than 7,000 pounds approved gross weight) or one turbine (not more than 12,500 pounds approved gross weight), fully compliant helicopter that meets the minimum aircraft requirements specified in Section A and is equipped as identified herein.

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

B6.2 One digital hour meter installed in a location visible by the pilot and front seat observer while seated. Location of meter is optional for aircraft with limited panel space (R44, R66 and MD500). Meter must be able to be observed without removal of panels and from a location at or forward of the cockpit doors. 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 (inertia reel, if manufactured for the make and model of aircraft offered), 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 Part 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 B29.5.)

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 Part 91.205(c), including instrument lights.

B6.10 Flight instruments for low visibility flight conditions, including gyroscopic bank and pitch indicator (ADI), directional gyro, vertical speed indicator and rate of turn indicator or skid/slip indicator or inclinometer.

Note: In lieu of these listed instruments, a single, new generation electronic instrument providing combined data meeting at minimum the following TSO's: C3e, C4c and C113A.

B6.11 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.

B6.12 High visibility, pulsating, forward facing, conspicuity lighting, if manufactured for make and model of aircraft offered.

B6.13 High visibility markings on main rotor blades as specified by the Acceptable Paint Schemes Exhibit (see section C exhibits).

B6.14 High-skid-type landing gear, if manufactured for make and model.

B6.15 Personnel access steps for aircraft with a floor height greater than 18 inches, to ensure safe entrance and exit from each door.

B6.16 Locking fuel cap(s) (if manufactured for the make and model of aircraft offered) on all fuel inlet ports.

B6.17 Cargo restraint system for aircraft manufactured with a parcel/storage area behind the rear passenger seats.

B6.18 One permanently installed, and circuit protected dual auxiliary power charging receptacle (USB) (cigarette lighter adapter is not acceptable).

B6.19 A first aid kit containing items specified in the First Aid and Survival Kits Exhibit (see section C exhibits) must be carried aboard the aircraft on all flights.

B6.20 A survival kit containing items specified in First Aid and Survival Kit Exhibits. Must be carried aboard the aircraft on all flights and must be included in weight and balance/load calculations. (see section C exhibits)

B6.21 A convex mirror for the pilot to observe the sling load. The convex mirror is not required for aircraft equipped and modified for vertical reference external load operation (i.e., door gauges, modified seat, alternate cargo hook release positions, and bubble window) or for aircraft where direct vertical reference is possible. A Video camera and monitor may be installed on aircraft with a limited or obscured view of external operations. Installation must be FAA approved.

B6.22 One cargo hook that may be loaded and locked in a single motion with one hand and is rated at the maximum lifting capacity of the aircraft. (See the cargo hook maintenance requirements in Section B29.6.) (not required for reconnaissance only aircraft)

B6.23 Aircraft Security Equipment. See Section B21.1.2 for required locking devices.

B6.24 Applicable to Robinson R44I or II models only. An exhaust heat shield kit (factory #KI 165) must be installed or an FAA approved equivalent.

Optional Equipment (if offered)

B6.25 Cargo compartment. (if offered)

Note: Internal storage compartments or passenger seats of the helicopter cannot be used for any cargo transport unless the seat is unoccupied or the material in the internal storage compartment is soft (e.g., coats).

B6.25.1 Small reciprocating helicopter

B6.25.1.1 External Cargo Rack/Basket: A side mounted external rack/basket attached to the aircraft. The rack/basket(s) must have at a minimum a horizontal surface of approximately 36 by 15 inches. Cargo carried in the rack must be secured with tie-down net, straps, bungees or any other method approved by the STC.

-OR-

B6.25.1.2 External Cargo Pod: An externally side mounted pod of either fiberglass or Kevlar construction that secures the cargo with a locking lid and is weatherproof. Examples: Simplex Helipod, Simplex VII Ski Pod, Helipod Slimline II, or equal.

B6.25.2 Turbine helicopter (not applicable to restricted category aircraft)

B6.25.2.1 Internal: 15-cubic-foot baggage compartment within the aircraft fuselage specifically designed to carry cargo separate from the cabin. This compartment must be capable of accommodating 58-inch long shovels, rakes, and other tools (requiring rear bulkhead modification of baggage compartment of some models).

-OR-

B6.25.2.2 External Cargo Rack: A side mounted external rack attached to the aircraft. The racks must have at a minimum a horizontal surface of approximately 48 by 15 inches, with a depth of 2.5 inches. Cargo carried in the rack must be secured with tie-down net, straps, or bungees. Examples: Alaskan Skycraft-style transporters and Garlick cargo racks.

-OR-

B6.25.2.3 External Cargo Pod: An externally side-mounted pod (or belly pod for the MD500) of either fiberglass or Kevlar construction that secures the cargo with a locking lid and is weatherproof. Examples: Heli-Composites Canada Star pod and DART Heli-Utility-Pod.

-OR-

B6.25.2.4 External Cargo Basket: An externally side mounted basket constructed with tubular frame and expanded metal and incorporating a locking lid or tie-down net, straps, or bungees to secure cargo. Examples: DART Heli-Utility- Basket and Aeronautical Accessories utility cargo basket.

Note: All construction methods must be as prescribed by Advisory Circular (AC) 43.13-1B (Revision 1) and 43.13-2B or other FAA approval.

B6.26 Barrel slings or cargo net to accommodate up to two 55- gallon drums of fuel as the aircraft weight and balance will allow. (if offered)

B6.27 Auxiliary fuel tank(s). (if offered)

B6.27.1 For Bell medium tank(s), see the Bell Medium Helicopter Exhibit (section C exhibits).

B6.27.2 For the MD500, an internal auxiliary fuel tank similar to the Fargo (21.0 gallons, U.S. capacity) when requested.

B6.27.3 For Bell 206B3s, an approved range extender (applicable only to the 76-gallon capacity tank).

B6.28 Pop out or standard floats for the aircraft. (if offered)

B6.29 Longline/remote cargo hook equipment (if offered).

If a long line is offered as an equipment option, the long line must be counter wound or rotation resistant wire rope with swaged fittings having a minimum breaking strength of 3.75 times the working load with appropriate placards and/or synthetic rope meeting the requirements of the Helicopter Synthetic Long Line Requirements in the Exhibit.

B6.29.1 The external load must be capable of being operated with all increments of the long line; i.e., 50, 100, 150 feet.

B6.29.2 A lanyard installed within 12 inches of the cargo hook to support any external remote longline electrical cabling.

B6.30 Other equipment may be required for special use missions as offered and specified in the Schedule of Items and accepted by the Government.

B6.30.1 Offshore, vessel landings, and extended overwater flight (if offered), see requirements identified in the Helicopter Offshore, Vessel Landings, and Extended Over Water Exhibit (section C exhibits).

B6.30.3 Basic fire (if offered), see requirements listed the Basic Fire Equipment Exhibit. (section C exhibits).

B6.30.4 ACETA operations (if offered), see requirements listed in the ACETA Exhibit 12 (section C exhibits).

B7 Avionics Requirements

B7.1 General All installed transceivers must be placarded with designations matching the transmitter/receiver controls on the installed audio control system(s).

B7.1.1 The Contractor must provide, install, and maintain the following systems in each aircraft offered 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:

https://www.nifc.gov/sites/default/files/NIICD/docs/avionics/FSOAS_A24F.pdf

B7.2 Avionics Installation and Maintenance Standards for all Helicopters:

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.

B7.2.3.1 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.

B7.2.4 Avionics equipment mounting location and installation must not interfere with passenger safety, space, and comfort. Avionics equipment must not be mounted under seats designed for deformation during energy attenuation. In all instances, the designated areas for collapse must be protected. Avionics equipment normally operated by both pilot and observer/copilot must be mounted in the optimum location for the make, model, and series of aircraft offered. Mounting(s) which offers full and unrestricted movement of each control to both pilot and observer/copilot, when seated, without interference from clothing, cockpit structure, or flight controls, must be a goal in the selection of location.

B7.2.5 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.

B7.3 Communications Systems

B7.3.1 One automatic-fixed Emergency Locator Transmitter (ELT), certified under TSO-C126 (or newer) which must be installed per the ELT manufacturer’s instructions in a conspicuous or marked location, and meet the same requirements as those detailed for airplanes 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 One panel-mounted VHF-AM (VHF-1) aeronautical transceiver, with a minimum of 760 channels covering 118.000 to 136.975 MHz. The transceiver must have channels selectable in no greater than 25 kHz increments and a minimum of 5 watts carrier output power. The transceiver’s 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 Reserved

B7.3.4 Reserved

B7.3.5 One satellite-based aircraft tracking hardware for each aircraft offered, compatible with the government’s Automated Flight 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.

Note: The following is a current list of AFF units that are compatible with the USFS aff.gov system at the time of the issuance of this solicitation:

Blue Sky Network, Guardian Mobility, Latitude Technologies, Outer Link, Sky Connect (will be changed to Troo Trax), Sky Trac, Spider Tracks, Trac Plus Global.

For questions about current compatibility requirements, contact the AFF Help Desk at https://www.aff.gov/help.aspx or 866-224-7677.

Portable ISAT systems may be used, if compatible with https://www.aff.gov. However, the system must be powered by the aircraft’s electrical system, operational in all phases of flight, be mounted so as to not endanger any occupant during periods of turbulence and have an antenna placement which ensures consistent GPS/Satellite reception and communication with the Iridium constellation. Any manufacturer-required pilot display(s) or control(s) must be visible and selectable by the pilot(s). Remote equipment having visual indicators must be mounted in such a manner that it is visible from the PIC position.

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 areas of operation, at all times. Contractors working in or accepting dispatches on all islands of Hawaii 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.

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

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/documents/Specification_Section_Supplement.pdf 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 GPSMap 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 GPS navigation database must be updated annually covering the geographic areas where the aircraft will operate.

B7.5 Audio Systems

B7.5.1 One audio control system must be provided for the pilot and copilot/observer. The system must provide controls for selection of receiver audio outputs and transmitter microphone/PTT audio inputs for any installed radios and PA systems. The system must also provide controls for adjustment of both Inter-Communication System (ICS) and receiver audio output levels. (different requirements for Fire see section C Exhibit)

B7.5.1.1 Transmitter selection and operation. Transmitter selection controls must be provided for the microphone/PTT inputs of pilot or copilot/observer. The system must be configured so that the pilot or copilot/observer may select and utilize transmitters (or PA/siren 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 side-tone audio must be provided for the user.

B7.5.1.2 Receiver selection and operation. Controls must be provided for selection of audio from one or any combination of available receivers. Any ICS-equipped passenger positions must monitor the receiver(s) as selected. 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 both the pilot and copilot/observer, when seated, have full and unrestricted 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 marking is acceptable.

B7.5.2 An intercommunications system (ICS) must be provided for the pilot, observer/copilot, and any additional required crewmember positions. ICS operation may be via either voice-activation (VOX) or push-to-talk (PTT). If PTT, the pilot’s PTT switch(es) must be mounted on the flight controls (helicopter cyclic or airplane control yoke), with cord-mounted PTT switches at any other required positions. ICS audio must mix with, but not mute, selected receiver audio. An ICS audio level control must be provided. 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. (different ICS requirements for Basic Fire and ACETA, see section C Exhibits)

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 A single U-92A/U type connector jack, which will accept a U-174/U type plug, and provide the ICS and radio functions as specified above, must be furnished at each required station.

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

B7.6 Other Avionics

B7.6.1 Automatic Dependent Surveillance – Broadcast (ADS-B) 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

B7.6.2 Each aircraft must be equipped to meet the Radar Altimeter requirements of 14 CFR 135.160, or have a current FAA Letter of Deviation Authority.

B7.6.3 Other avionics are required for special use missions as offered and specified in the Schedule of Items and accepted by the Government.

See the following exhibits for addition avionics requirements:

· Exhibit 11 Arial Capture Eradication and Tagging of Animals

· Exhibit 12 Offshore, Vessel Landing, and Extended Over Water

· Exhibit 13 Basic Fire

B8 Fuel Servicing Equipment Requirements

B8.1 Fuel servicing equipment must meet all applicable requirements identified in NFPA 407: Standard for Aircraft Fuel Servicing and ATA 103: Standard for Jet Fuel Quality Control at Airports.

B8.2 The Contracting Officer’s Technical Representative (COTR) may conduct an inspection annual.

PERSONNEL REQUIREMENTS

B9 Pilot Requirements and Authority

B9.1 The Contractor must furnish a pilot for each day the aircraft is required to be available. The pilot must have the authority to represent the Contractor in all matters except changes in price and time, unless the Contracting Officer (CO) is notified otherwise, in writing, prior to performance.

B9.1.1 For a pilot that has not been previously inspected and approved by the OAS or USDA Forest Service, the Contractor will be required to provide a signed statement that they have verified the pilot’s flight time qualifications and experience. The COTR will provide the Contractor a form to document this verification. This will be required prior to pilot inspection by OAS.

B10 Pilot Qualifications

B10.1 General

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

B10.2 Minimum Qualifications

The Contractor must provide a pilot(s) who meets the following minimum qualifications and who possesses the…