DRAFT_SOW_POSTING_AG-024B-S-15-9016_AFUE.pdf

Solicitation AG-024B-S-15-9016 U.S. Forest Service Exclusive Use AFUE Mission Support Aircraft National Office

SECTION B

SCHEDULE OF SUPPLIES OR SERVICES AND PRICE

B.3 SCOPE OF CONTRACT

(a) The intent of this solicitation and the resulting contract is to obtain a fully contractor operated and maintained aviation services to perform fire mapping on initial attack, extended attack, and large fire in support of the Aerial Firefighting Use and Effectiveness (AFUE) study and nationwide wildland firefighting operations. AFUE is tasked with objectively documenting and developing a consolidated approach, metrics, and system to evaluate the use and contributions of firefighting aircraft in support of wildland fire incident objectives.

(1) The aircraft, sensors, hardware, software, training, associated equipment, and personnel described within are to be utilized in support of the Aerial Firefighting Use and Effectiveness study

(2) This platform may be utilized at any location in the Continental United States or Alaska in which aerially delivered suppressants are being utilized. The general mission profile, excluding ferry, consists of 30-45 minutes to and from the fire, maximum on station time over the incident for data collection over the fire (2-3 hours). Total daily fight times could exceed eight (8) hours with an additional crew. The crew is generally comprised of the contractor pilot, one AFUE provided aerial supervisor or aerial observer occupying the co-pilot station and an aft crew station which may be staffed by an AFUE provided instructor, trainee, observer, or sensor operator. Data collection consists of the recording of incident radio communications, documenting and processing overall fire behavior (rate of spread, intensity, etc.), targeted repeated observations of aerially delivered suppressant footprints, coverage and continuity, and targeted fire behavior before, during, and after interactions with suppressants.

(3) The airplane will be operated within the mountainous orographic turbulent environment associated with average altitudes varying from 7,000 AGL to 12,500 ft.

AGL.

(b) The contractor will provide airplane(s), pilots, training on the offered mapping systems, and all maintenance and system support.

(c)The aircraft furnished will be used for support of the AFUE Study described above as well as and administrative services.

(d) The Government has interagency and cooperative agreements with other Federal and State Agencies and private landholders. Aircraft may be dispatched under this contract for such use.

B.4 CERTIFICATIONS

(a) Contractors shall hold a current Federal Aviation Administration (FAA) Air Carrier or Operating Certificate under 14 CFR part 135. Aircraft offered shall be listed by make; model, series, and registration number on the Contractor’s 14 CFR 135 Operating specifications at the time of offering and for the duration of the contract.

(b) Aircraft shall conform to its approved type design, be maintained and operated in accordance with the requirements of the 14 CFR 135 notwithstanding the aviation regulations of the States in which the aircraft may operate except those requirements specifically waived by the CO.

(1) All passenger-carrying flights shall be conducted in accordance with the Contractor’s/Operator’s 14 CFR part 135 operation specifications, and all FAA approved and accepted manuals.

B.5 AIRCRAFT

(a) The aircraft furnished shall have certified power plant and airframe log books and other necessary papers substantiating the maintenance, overhaul, and airworthiness history.

(b) Aircraft Requirements.

(1) Minimum Aircraft Requirements

Payload: --750 pound payload when fully equipped and with 3 hours plus 30 minute reserve.

Speed: --Cruise speed of 165 knots True Airspeed (TAS) @ 8000 ft. – ISA plus 20o C.

Endurance: --Cruise endurance of 4 hours @ 8000 ft – ISA plus 20O C plus a 30 minute reserve.

Powerplant: --Single-Engine or Multi-Engine, Turbine or jet powered aircraft.

--All aircraft operations achieve performance described within 14 CFR 23 with the following more restrictive additions: Aircraft shall achieve a minimum positive single engine climb rate when equipped per the contract of 200 ft/nautical mile at 5,000 ft MSL at 30o C

--Single engine aircraft shall have a power loading of not more than

13.5 pounds per horse power.

--Multi engine aircraft shall be capable of at least 200 horse power per engine; any engine developing less than 240 horse power shall be turbo/super charged.

Environmental:--Pressurized aircraft with environmental controls.

(c) Aircraft Condition. The aircraft shall be in airworthy condition throughout the performance period. All equipment required for original certification shall be installed and operable or be deferrable by an FAA approved Minimum Equipment List (MEL).

(1) All aircraft and installed equipment furnished under this contract shall be operable, free of damage, and in good repair. Aircraft systems and components shall be free of leaks, except within limitations specified by the manufacturer.

(2) The aircraft interior shall be clean and neat. There shall be no un-repaired tears, rips, cracks, or other damage to the interior. All interior materials must meet FAA standards.

(3) The aircraft exterior finish, including the paint, shall be clean, neat, and in good condition (i.e. no severe fading or large areas of flaking or missing paint etc.).

High visibility paint schemes are desired. Any corrosion shall be within manufacturer or FAA acceptable limits.

(4) All windows and windshields shall be clean and free of scratches, cracks, crazing, distortion, or repairs, which hinder visibility. Repairs such as safety wire lacing and stop drilling of cracks are not acceptable as permanent repairs. Prior to acceptance temporarily repaired windows and windshields shall have permanent repairs completed or shall be replaced.

(d) Each aircraft shall carry current copies of the following:

(1) Contract and all modifications.

(2) Aeronautical charts covering area of operation.

(3) Exemption DOT-E-9198.

(4) Aviation Transportation of Hazardous Materials Guide.

(5) DOT Emergency Response Guide (ERG).

B.6 AIRCRAFT EQUIPMENT REQUIREMENTS

(a) Aircraft shall be equipped as required by 14 CFR Part 135 for VFR, IFR, night flights, flights above 10,000 feet, and flights in Class A and B Airspace. In addition, each aircraft shall have:

(1) Hour meter recorder to record actual flight time from take-off to landing, reading in hours and tenths, and activated by an air switch or equivalent system. Recorder shall be observable by pilot and observer in flight.

(2) One strobe light mounted on top of the aircraft, plus a second mounted on the belly; or one white strobe light mounted on each wingtip and on the tail.

(3) Shoulder harness for each front seat (including pilot).

(4) Manuals and other documents referenced under 14 CFR Part 91.

(5) All radio/electronics items including: wiring, antennas, connectors/adapters and hardware, specified herein, except for Government-furnished property.

(6) In pressurized, aircraft and Pilots shall meet 14 CFR Part 135 Oxygen Requirements.

(7) Fire extinguishers, as required by CFR 135.155, shall be hand-held bottle(s), with a minimum of 1.5 lb. capacity and 2-B: C rating. Fire Extinguishers shall be maintained in accordance with current NFPA 10 standards and mounted with a quick release attachment accessible to the flight crew while seated.

(8) FAA approved workstation for front seat and rear seat sensor and system operation.

(9) Cargo Restraint. The Contractor shall furnish tie downs, net(s), or cargo straps meeting requirements of Federal Aviation Regulations to restrain cargo while in flight.

(10) Safety Belts. The aircraft furnished under this contract shall have safety belts meeting requirements of Federal Aviation Regulations for all occupants (See Exhibit 02). All occupants shall wear safety belts during takeoffs and landings, when flying within 1,000 feet of the ground, and at other times as specified by the pilot. Front seats shall have FAA approved shoulder harnesses.

(11) First Aid Kit (Aeronautical). First aid kit shall be in a dust-proof and moisture-proof metal or heavy plastic container. The kit shall be readily accessible to the pilot and passengers. The contents will include the following minimum items:

Item Description Quantity

Adhesive bandage compresses (3 inches long) 8

Antiseptic or alcohol wipes (packets) 10

Bandage compresses, (4 inches) 4

Triangular bandage compresses, 40 inch (sling) 2

Roller bandage, 4 inch x 5 yards (gauze) 2

Adhesive tape, 1 inch x 5 yards (standard roll) 1

Bandage scissors 1

Body Fluids Barrier Kit: Includes list below 1

2-pair of latex gloves

1-face shield

1-mouth-to-mouth barrier

1-protective gown

2-antiseptic towelettes

1-biohazard disposal bag

Notes: Splints are recommended if space permits.

Kits may be commercially available types which are FAA approved for the appropriate numbers of crew and passengers carried.

(12) Survival Kit. Aircraft will have sufficient equipment to sustain personnel for a 24-hour period. As a minimum, the survival kit will include the following:

Item Item

Knife Signal Mirror

Aviation Type Signal Flares (6-each) Matches (2-small boxes in waterproof containers)

Space Blanket (1-per occupant) Water (1-quart per occupant {not required when operating over areas with adequate drinking water)

Food (2-days emergency rations per occupant)

Candles

Collapsible Water Bag Whistle

Magnesium Fire Starter Nylon Rope or Parachute Cord (50 feet)

Suggested Survival Kit Items Dependent upon Terrain and Climate

Item Item

Container w/carrying Handle or Straps Individual First Aid Kit

Large Plastic Bags Signal Panels

Flashlight with Spare Batteries Hand Saw or Wire Saw

Collapsible Shovel Sleeping Bag (1-per two occupants)

Survival Manual (Arctic/Desert) Snowshoes

Insect Repellant Axe or Hatchet

Insect Head net (1-per occupant) Gill Net/Assorted Fishing Tackle

Personal ELT Sunscreen

B.7 SENSOR EQUIPMENT REQUIREMENTS

(a) All required technology offered for this platform in (a) through (h) below must be:

(1) Original Equipment Manufacturer (OEM) installation,

(2) Under a Supplemental Type Certificate (STC)

(3) Approved for installation by an FAA From 8110-3 with all DER supporting engineering substantiation documentation attached, or

(4) Field Approved for installation with supporting FAA Form 8110-3 and all DER supporting engineering substantiation documentation attached.

(b) All data pertinent for these installations shall be available for review by the Forest Service prior to contract award. Installations of the technology requirements are not acceptable as a minor alteration. FAA Field Approvals are authorized provided the following:

(1) Field Approvals based on previously approved installations must match Make and Model.

(2) Field Approvals using previously approved "generic" Field Approvals are not acceptable, i.e. a Field Approval for a King Air, based on a previously approved similar installation for an Aero Commander, would not be acceptable.

(c) Primary Sensor. Primary Sensor equipment provided by the Contractor shall meet the following requirements:

(1) FAA approved, multi-axis stabilized gimbal, wide area infra-red (IR) fire mapping camera system which is capable of providing motion imagery (temporal and spatial data) on wildland fire incidents to collect fire spread, aerial delivered suppressant footprints, and suppressant/fire interaction during daytime environmental conditions associated with wildfire activities.

(2) Must conform to the Motion Imagery Standards Board (MISB) standards. Standards can found at: http://www.gwg.nga.mil/misb/

(3) When flying at 10,000 -12,500 ft. AGL the IR system/sensor shall achieve the following:

(i) Produce a coverage area of one (1) square mile or greater.

(ii) Achieve an average Ground Sample Distance (GSD) of two (2) meter or less.

Within this document GSD is used when referring to the collection GSD of the raw image, assuming near-vertical imagery. The actual GSD of each pixel is not uniform throughout the raw image and varies significantly with terrain height and other factors. Within this document, GSD is assumed to be the value computed using the calibrated camera focal length and camera height above average horizontal terrain.

(iii) Minimum capture frame rate of 1 Hertz

(iv) Sensor shall be capable of detecting, differentiating, and monitor the following:

(A) Aerially delivered suppressant’s footprint and surface coverage (continuity, gaps, scalloping.)

(B) Active flaming edge and spread fire.

(C) Spot fire of 1 meter diameter and at a minimum temperature of 600 degrees Celsius (C).

(D) Ability to detect (track) suppressant delivery aircraft.

(E) Shall be calibrated in a manner (spectrum, gain, etc.) to minimize/filter out 80% of false positives.

(F) Accurately capture distances between objects of interest, i.e. fire front and suppressant drop footprint over time.

Source Temperature (C) Nominal Wavelength Background 25 10 Fuel Ignition 275 5

Glowing 550 4 Cool Fire 725 3 Hot Fire 1200 2 http://nirops.fs.fed.us/docs/upload/Infrared_Field_Users_Guide_November_2014.pdf

(4) Mounted in a manner that allows for an unobstructed 360 degree continuous pan from 10 degrees below the lowest horizontal plane of the aircraft, and throughout downward pointing angle(s) to the earth’s surface directly (perpendicular) below the aircraft at level (0o) pitch, roll, and yawl. I.E. aircraft can maneuver in both right and left hand orbits without degrading data acquisition quality/capability of the target scene.

(5) Detector cooling (if applicable) shall be a closed-loop, self-contained system, and not require charging prior to flight.

(d) Sensor’s Operational Graphic User interface (software)

(1) While in operation, possess a continuously visible view of the user selected live motion images at a scale and resolution in which viewer/operator can easily identify suppressant drops, fire behavior, and situational targets under variable lighting and environment conditions associated with the mission.

(2) While in operation, possess continuously visible moving map in which aircraft location and sensor FOV footprint is displayed and recorded along with sensor metadata over a base map. Required base maps are 1:150k and 1:24 scales, seamless, USGS topographical and NAIP imagery for Alaska and the continental United States (CONUS).

Base maps may be provided through map service only if the service is fully functional when operating in areas without an internet connection.

(3) Capable of extracting/exporting, geo-referenced mosaics within a user defined temporal and spatial binding areas. Resulting in imagery stacks within a user defined temporal and spatial parameters which are horizontally accurate in the X and Y plan at an 95% confidence level (489.5 cm) utilizing Root Mean Square Error statistics;

American Society of Photogrammetry and Remote Sensing (ASPRS) 2014 200 cm class or equivalent to the legacy ASPRS 1990 standard of Class 2 for one (1) meter orthoimagery pixels. http://www.asprs.org/PAD-Division/Map-Accuracy-Standards- Working-Group.html

(4) User shall be able to ingest, create, attribute, and distribute vector data meeting GSTOP standard (http://gis.nwcg.gov/documents/gstop/documents/gstop.pdf) as an overlay on the moving map and sensor imagery. Example of such would include but not limited to: suppressant drops, fire edge, and constructed firelines. Vector data must be exportable along with the sensor raster imagery.

(5) Targeted Deliverable Products:

(i) Raw mission Imagery, audio, and vector data

(ii) Extracted suppressant drop rater imagery of singular drop events.

(A) Fire location relevant to suppressant at time of delivery.

(B) Location of suppressant and footprint.

(C) Fire and suppressant interaction (temporally and spatially).

(D) Outcomes of fire/suppressant interaction.

(iii) Attributed vector data which describes associated drop and fire imagery.

Upon award, government will provide attribute feature classes and domains.

(6) Ability to snapshot still, geo-referenced images and save them to an incident specific directory.

(7) Ability of operator to select/adjust sensor detection characteristics and image display characteristics to facilitate optimization of the image based on terrain, day/night, smoke/haze, fire intensity.

(e) Data Recording and Storage

The US Forest Service is the sole owner of any data (documents, imagery, audio, etc.) collected during any contracted mission and maintains complete control of use and distribution. All external uses must be preapproved and expressed in writing.

(1) On-board digital recording of motion imagery and all active radio bands (FM/AM/ICS). The resulting product shall be a time stamped (UTC), geo-coded, recoding of the sensor’s FOV, which is synchronized with radio audio. Radio communications shall be recoded in a manner in which playback supports all bands being played simultaneously or individually isolated.

(2) Motion imagery must be stored in a codec or have the ability to export to a nonproprietary or open source codec that can be ingested by Geospatial Information Systems (GIS) such as ESRI’s ArcMap suite. Additionally delivered codec must support playback in standard media players such as Window Media Player (imagery and audio).

(f) Data link

(1) Self-forming peer-to-peer routing, IP based, mobile ad hoc (MANET) local area network (LAN) node capable of supporting wide area network (WAN) connection among neighboring nodes using any-to-any connectivity logic. Data link node shall be integrated with onboard sensor in a manner that supports motion imagery streaming, product ingest/dissemination, and off aircraft sensor operation. Data Link antenna(s) shall be located in a manner to minimize signal shadowing while in the data collection flight profile across a line of sight twenty (20) mile radius from the aircraft and to the ground.

(i) five 10/100 MBPS Ethernet port (IP67 rated)

(ii) Integrated serial-to-Ethernet

(iii) Throughput of 37 Mbps UDP and 27 Mbps TCP

(iv) Dynamic Link exchange protocol certified

(v) IPV4 and IPV6 compatible

(vi) 802.11 a/b/g AP compatible

(vii) FIPS 140-2 level security validation

(2) Alternate Communication system, such as a satellite phone or voice capable AFF device, which allows for in flight voice communications, coordination and re-tasking.

Systems must support both sending and receiving calls while in flight and possess an in headset audio tone indicating incoming or lost alternate communications.

(g) Training

(1) Technical documents shall validate full system capabilities and integration of sensor, software, data link and system use. How-to and troubleshooting documents shall support quick reference on the operational utilization, including aircrew coordination to and over targets, (ConOps) and data processing of the ISR system and directly support hands-on training of agency provided operator(s). All Training Material shall be provided electronically. In the event that hardware or software systems are modified after the initial training, the Contractor shall provide updated training and electronic training material at no cost to the Government.

(2) Training shall be provided to10-15 agency employees at the beginning of contact period and be comprised of both classroom and hands-on (ground school and inflight) covering:

(i) Capabilities and limitations of the sensor system.

(ii) Operation of the sensor and troubleshooting

(iii) Aircrew (pilot/observer) coordination, targeting, and communications to and over mission objective

(iv) Detailed instruction of data is capture, storage, processing, and extraction workflow and processes

(v) Detailed training on data-link usage, configuration, trouble shooting and limitations

(vi) Utilization the software interfaced during operation and extraction/manipulation of data products.

(vii) General Aircraft familiarization and safety (for provided aircraft)

(3) Training costs in Missoula, MT shall be included in the cost of the Sensors for each sensor option offered. Training shall be conducted one time for the primary sensor and at a maximum of one time per optional sensor systems if ordered.

(h) Optional and Replacement Equipment:

Options described within this section may be offered as optional equipment when the equipment exceeds or is in addition to, the above minimum requirements or may be added through the contract modification process.

(1) REPLACEMENT SYSTEM 1: FAA approved, multi-axis stabilized gimbal, wide area fire mapping Infra-Red (IR) and EO (electro optical) camera system which is capable of providing motion imagery on wildland fires incidents to collect fire spread, aerial delivered suppressant footprints, and suppressant/fire interaction.

(i) When flying at 10,000-12,500 ft. AGL with an orbital radius of one and one half (1.5) nautical miles, the EO system/sensor shall achieve the following:

(A) Produce a coverage area of two (2) square miles or greater.

(B) Achieve an average Ground Sample Distance (GSD) of 0.5 meter or less

(C) Minimum Capture frame rate of 1 Hertz

(ii) Under the same flight profile, the IR system/sensor shall achieve the following:

(A) Produce a coverage area of one (1) square mile or greater.

(B) Achieve an average Ground Sample Distance (GSD) of 1 meter or less

(C) Minimum capture frame rate of 1 Hertz

(D) Detector cooling (if applicable) shall be a closed-loop, self-contained system, and not require charging prior to flight. Color with EO

(2) REPLACEMENT SYSTEM 2: FAA approved, multi-axis stabilized, enhanced IR/EO gimbal camera system which is capable of providing full motion imagery on wildland fire incidents to collect fire spread, aerial delivered suppressant footprints, and suppressant/fire interaction.

(i) Enhanced IR/EO gimbal camera meeting High definition (HD) standard

(ii) Multiple bands of IR (SWIR and MWIR) in addition to EO

(iii) Sensor Imagery fusion

(iv) Laser range finder

(v) Derived raster imagery shall be in alignment with NAIP imagery registration in the same Datum.

(vi) Detector cooling (if applicable) shall be a closed-loop, self-contained system, and not require charging prior to flight.

(vii) Object Tracking and Sensor Pointing.

(viii) Geographic Pointing – Applicable payloads shall have the ability point at a specified geographic location (latitude/longitude) within the payload’s field of regard (FOR).

(ix) Fixed Pointing - Applicable payloads shall be able to continuously point at a fixed surface target while aircraft is in motion.

(x) Marker Targeting – Applicable payloads shall have the ability to point to user defined surface target within the FOR.

(xi) Fixed Stare – Applicable payload shall be able to hold a fixed azimuth and pointing angle while aircraft is in motion (strip profile).

(xii) Object Tracking – track moving objects, such as aircraft and vehicles, based on image matching with the user adjustable target box.

(3) REPLACEMENT SYSTEM 3: FAA approved, multi-axis stabilized, Hyperspectral or multispectral sensor camera system which is capable driveling products centered on detecting fire spread and behavior (intensity), suppressants (water and chemically enhanced), fuels (loading, continuity, and arrangement).

(4) OPTIONAL INTERNET 1: Satellite Internet or other broadband WAN inflight internet, hardware and service, WAN hardware/service must integrate with LAN data link provide a WAN gateway to device connect to the LAN date link.

(5) OPTIONAL INTERNET 2: On board WiFi LAN wireless network router which is integrated with LAN data link system and supports the connection of mobile devices.

(6) OPTIONAL EQUIPMENT 1: Three dimensional (3D) surface elevation sensor, model creations software, and training. Sensor must be available in conjunction with imaging sensors offered. Resulting surface models (elevation model) is utilized to precisely position AFUE raster and vector data in complex topography and describe vegetative structure.

(7) OPTIONAL EQUIPMENT 2: Enhanced auto-pilot which supports maintaining data acquisition flight profile and minimize pilot fatigue such as flying an orbital radius of one and one half (1.5) nautical miles for prolonged missions.

(8) OPTIONAL EQUIPMENT 3: Installation and service plan of Government provided real-time weather collection sensor, such as Tropospheric Aircraft Meteorological Data Relay (TAMDAR)

(i) Optional Services:

(1) OPTIONAL SENSOR OPERATOR: Contractor provided sensor operator which may be mobilized within 24 hours of request on an as needed basis or throughout the duration of platform contacted availability. Operator is considered essential aircrew and must follow agency work/rest regulations, sensor operator is entitled and/or restricted to the same travel (per diem) regulations as the platforms pilot.

(2) OPTIONAL ADDITIONAL PILOT: Contractor provided additional pilot which may be mobilized within 24 hours of request on an as needed basis or throughout the duration of critical fire activity/vents. Additional Pilot is of facilitate double crewing the aircraft during high fire activity and of extended burn periods which would result in consecutive mission being flow in a single duty day or consecutive days. Additional pilot must follow agency work/rest regulations and is entitled and/or restricted to the same travel (per diem) regulations as the platforms primary pilot.

B.8 AVIONICS

(a) MINIMUM REQUIREMENTS

All avionics used to meet this agreement shall comply with the requirements of paragraph B.9 (AVIONICS SPECIFICATIONS) and paragraph B.10 (AVIONICS INSTALLATION AND MAINTENANCE STANDARDS). The following are the minimum avionics which shall be installed. Additional avionics may be required in section B of this agreement.

(1) Point to Point Aircraft – Reserved (Not applicable to this solicitation)

(2) Back Country Aircraft – Reserved (Not applicable to this solicitation)

(3) Resource Reconnaissance Aircraft - Reserved (Not applicable to this solicitation)

(4) Fire Reconnaissance Aircraft - Reserved (Not applicable to this solicitation)

(5) Air Tactical Aircraft

(i) Type I Reserved

(ii) Type 2 – (minimum acceptable equipment for this solicitation)

(A) Two VHF-AM Radios (COM 1 & COM 2)

(B) One VHF-FM Radio (FM)

(C) One Auxiliary FM system (AUX FM)

(D) An Intercom System (ICS)

(E) Separate Audio Control systems for the PIC and SIC/observer

(F) Audio jacks with ICS and radio transmit capability in the rear seat connected to the SIC/observer Audio Control system. An Aft Audio Control system for this position is acceptable.

(G) One Global Positioning System (GPS)

(H) An Emergency Locator Transmitter (ELT)

(I) An Automated Flight Following system (AFF)

(J) One Transponder

(K) One Altimeter and Automatic Pressure Altitude Reporting system

(L) Equipment and lighting for night VFR operations in accordance with 14 CFR 135.159 and 14 CFR 135.161.

(M) Traffic Advisory System (TAS)

(N) Autopilot

(O) Multi-Function Display (MFD)

(P) VHF-FM Programming Port

(iii) Type 3 - Reserved (Not applicable to this solicitation)

(iv) Type 4 - Reserved (Not applicable to this solicitation)

Note 1: Air Tactical aircraft equipped with an approved TAS shall be identified “w/TAS” on the aircraft approval card.

Note 2: Reserved

Note 3: Supplemental Air Attack Kit installations shall not elevate the aircraft’s capability beyond the type for which it would otherwise be approved.

B.9 AVIONICS SPECIFICATIONS

All avionics used to meet this agreement shall comply with the following requirements and paragraph B.10 (AVIONICS INSTALLATION AND MAINTENANCE STANDARDS).

(a) Communications systems

(1) VHF-AM Radios

VHF-AM radios shall be TSO approved aeronautical transceivers, permanently installed, and operate in the frequency band of 118.000 to 136.975 MHz with a minimum of 760 channels in no greater than 25 KHz increments. Transmitters shall have a minimum of 5 Watts carrier output power and shall not open squelch on, or interfere with, other AM or FM transceivers on the aircraft monitoring different frequencies.

(2) VHF-FM Radios

All aircraft approved for fire operations shall use P25 Digital VHF-FM transceivers meeting the specifications of FS/OAS A-19. FM radios used in all aircraft shall be agency approved. FS/OAS A-19 and a list of currently approved FM radios can be found on the following website: http://www.nifc.gov/NIICD/documents.html . The following requirements shall be met.

(i) VHF-FM radios shall be aeronautical transceivers, permanently installed in a location that is convenient to the PIC and SIC/observer, and operate in the frequency band of 138 to 174 MHz. All usable frequencies shall be programmable in flight. Narrowband and digital operation shall be selectable by channel for both MAIN and GUARD operation. Carrier output power shall be 6- 10 Watts nominal.

(ii) Transceivers shall have a GUARD capability constantly monitoring 168.625 MHz and have a tone of 110.9 on all GUARD transmissions. Simultaneous monitoring of MAIN and GUARD is required. Scanning of GUARD is not acceptable. Aircraft not approved for Air Tactical operation only require one FM GUARD receiver.

(iii) Transceivers shall have the capability of encoding CTCSS sub audible tones on all channels. A minimum of 32 tones meeting the current TIA/EIA-603A standards shall be selectable.

(iv) Transceivers shall have the capability to display both receiver and transmitter frequencies. Activation indicators for transmit and receive shall be provided for both MAIN and GUARD operation.

(v) The radio shall use an external broadband antenna covering the frequency band of 138 to 174 MHz (Comant CI-177-1 or equivalent).

(3) Auxiliary FM systems (AUX FM)

An interface to properly operate a portable FM radio through the aircraft audio control systems shall be provided using an MS3112E12-10S type bulkhead mounted connector with contact assignments as specified by FS/AMD A-17 available at the following website: http://www.nifc.gov/NIICD/documents.html . Sidetone for the portable radio shall be provided (AEM AA34 or equivalent). The following applies to all AUX FM installations.

(i) An external broadband antenna covering the frequency band of 138 to 174 MHz (Comant CI-177-1 or equivalent) shall be installed with the associated coax terminated in a bulkhead mounted BNC connector adjacent to the above 10 pin connector.

(ii) A portable radio mount (Field Support Services AUX-EPH-RB or equivalent) shall be installed providing the crew unrestricted operation of the radio controls when connected with an 18 inch adapter cable.

(iii) A VHF-FM radio meeting the requirements of paragraph B.9(a)(2) may be installed, in addition to the radios already required, in lieu of the AUX FM system.

(4) Non-Standard Radios

Non-standard radios shall be aeronautical transceivers interfaced to the aircraft audio control systems and a compatible antenna via an approved installation. The radio shall be compatible with the requesting unit.

(b) Audio Systems

(1) Intercom systems (ICS)

ICS shall integrate with the aircraft audio control systems and mix with selected receiver audio. An ICS volume control and a “hot mic” capability shall be provided for the PIC and SIC/observer. Passenger volume adjustments shall not affect the PIC. Hot mic may be voice activated (VOX) or controlled via an activation switch. The PIC shall have an isolation capability.

(2) Audio Control systems

(i) General

Controls for transmitter selection and independent receiver selection of all required radios shall be provided for each required audio control system. Each system shall have the capability to simultaneously select and utilize a different transmitter (and PA if required). Sidetone shall be provided for the user as well as for cross monitoring by all installed systems. Receiver audio shall be automatically selected when the corresponding transmitter is selected. Receiver audio shall be provided to each position which requires ICS. Aft audio control systems are not required to provide NAV audio.

All required passenger positions shall utilize the SIC/observer’s audio control system unless an aft audio control system is installed. Drop cords may be used provided MS3112E10-6S type 6-pin connectors are installed adjacent to the required passenger headset jacks and wired for compatibility with an appropriate drop cord (Alpine Aerotech AAL280 series or equivalent).

Audio controls shall be labeled as COM-1, FM-1, AUX, PA etc… as appropriate or as COM-1, COM-2, COM-3, etc… with the corresponding transceiver labeled to match. Audio shall be free of distortion, noise, or crosstalk. The system shall be designed for use with 600 ohm earphones and carbon equivalent, noise cancelling, boom type microphones. All required positions shall have JJ-033 and JJ-034 type microphone and headphone jacks separated by no more than 4 inches. Cockpit speakers shall be sufficiently amplified for use in flight.

Crew positions shall have radio Push-To-Talk (PTT) switches on their respective flight controls. A PTT switch shall be provided to allow the SIC/observer to transmit without touching the flight controls.

(ii) Drop Cord Requirements

(A) Coil cord with sufficient length to provide unrestricted movement according to mission requirements (Minimum 3 feet retracted)

(B) 6-Pin MS3476L10-6P type connector on the coil cord

(C) JJ-033 and JJ-034 type headset jacks at the housing

(D) Large clip

(E) Volume control

(F) ICS switch with momentary and lock positions

(G) Radio PTT switch (only for positions which require radio transmit)

(iii) Aft Audio Control systems (when required)

The audio controller shall be installed in a location that provides the operator directly behind the SIC/observer unobstructed access to the controls while seated. Aft passengers shall utilize this audio control system. If multiple aft audio controllers are installed, passengers shall utilize the most logical system.

(iv) Required Audio Control systems

The following audio control systems are required based on mission type

(A) Type I and Type II Air Tactical airplanes

1. Two separate audio control systems (which may be combined in a single unit) for the PIC and SIC/observer

2. The instructor position (directly behind the SIC/observer) shall have radio transmit capability. This position shall follow the SIC/observer system or have an aft audio control system.

(c) Navigation systems

(1) Global Positioning Systems (GPS)

(i) Aeronautical GPS

Each required GPS shall be TSO approved, permanently installed where both the PIC and SIC/observer can clearly view the display, use an approved external aircraft antenna, and be powered by the aircraft electrical system. The GPS shall utilize the WGS-84 datum, reference coordinates in the DM (degrees/minutes/decimal minutes) format and have the ability to manually enter waypoints in flight. The GPS navigation database shall be updated annually covering the continental United States. Aircraft operating in Alaska shall include an Alaskan database in the annual coverage.

(ii) Portable Aviation GPS

Portable aviation GPS units (Garmin GPSMAP, aera, or equivalent) are acceptable when an Aeronautical GPS is not specified. They shall be securely mounted via an approved installation using the aircraft electrical system and a remote antenna. The GPS shall present information from an overhead perspective. The PIC shall have clear view of the display and unrestricted access to the controls. The SIC/observer shall also have a clear view of the display in Air Tactical aircraft. The GPS shall meet the above datum, coordinate, and database requirements for an aeronautical GPS. Portable GPS units are not acceptable for aircraft performing IFR or NVG operations.

(iii) GPS with Moving Map

The GPS providing data to the moving map shall meet all of the above GPS requirements. The moving map’s display shall be 3 inches wide, 1.5 inches high, and show the aircraft’s present position relative to user selected waypoints and geographical features. The map may be integrated with the GPS.

(d) Surveillance systems

(1) Emergency Locator Transmitters (ELT)

Emergency locator transmitters shall be automatic-fixed, installed in a conspicuous or marked location, and meet the requirements detailed in 14 CFR 91.207 (excluding section f). ELT antennas shall be mounted externally to the aircraft unless installed in a location approved by the aircraft manufacturer. TSO C91a or newer ELTs are required.

TSO C126 and newer ELTs require documentation of current registration from the national civil aviation authority for which the aircraft is registered.

(2) Automated Flight Following systems (AFF)

Automated flight following systems shall be compatible with the government’s tracking program (AFF.gov), utilize satellite communications, and use aircraft power via a dedicated circuit breaker.

AFF shall be functional in all phases of flight and in all geographic areas where the aircraft will operate. The following additional requirements shall be met.

(i) A subscription service shall be maintained through the equipment provider allowing position reporting via the Government AFF Program. The reporting interval shall be every two minutes while in flight.

(ii) AFF equipment shall be registered with AFF.gov providing all requested information. Changes to equipment and registration information shall be reported to AFF.gov ensuring the program is current prior to aircraft use. For assistance, the Fire Applications Help Desk (FAHD) may be reached at (866) 224-7677 or

(360) 326-6002.

(iii) An AFF operational test shall be performed prior to the annual compliance inspection. This test shall ensure that the system meets all requirements and is displayed in the AFF viewer with the correct information. A user name and password are required. Registration and additional information are available at https://www.aff.gov/ .

(iv) If AFF becomes unreliable the aircraft may, at the discretion of the Government, remain available for service utilizing radio/voice systems for flight following. The system shall be returned to full operational capability within 5 calendar days after the system is discovered to be unreliable.

(v) This clause incorporates the Specific Section Supplement available at https://www.aff.gov/contractspecs.asp as if it was presented as full text herein.

(vi) For questions about current compatibility requirements contact the AFF Program Manager listed under contacts at https://www.aff.gov

(3) Transponders

Transponder systems shall meet the requirements of 14 CFR 91.215(a). Part 135 aircraft shall meet the “Mode S” requirements of 14 CFR 135.143(c). Transponder systems shall be tested and inspected every 24 calendar months as specified by 14

CFR 91.413.

(4) Altimeter and Automatic Pressure Altitude Reporting systems

Altimeter, static pressure, and automatic pressure altitude reporting systems shall be installed and maintained in accordance with the IFR requirements of 14 CFR Part 91.

These systems shall be tested and inspected every 24 calendar months as specified by

14 CFR 91.411.

(5) Traffic Advisory Systems (TAS)

Traffic advisory systems shall be TSO approved, use active interrogation, graphically display traffic relative to the aircraft’s horizontal position, and provide alert audio to the PICs audio control system. The display shall be within view of the PIC and SIC/observer.

The system shall provide coverage in all directions above and below the aircraft with a maximum range of at least 10 nautical miles. The display shall allow range selection of 2 miles or less.

(e) General Systems

(1) Autopilots

Autopilots shall be capable of operating the aircraft controls to maintain flight and maneuver it about the three axes.

(2) RADAR Altimeters Reserved (Not applicable to this solicitation)

(3) Multi-Function Display (MFD)

MFD shall be installed within view of the PIC and display GPS navigation information on a color moving map. TAS and weather datalink information shall be displayed on the MFD when these systems are required.

(4) Cockpit Voice Recorder (CVR) Reserved (Not applicable to this solicitation)

(5) Reserved

(6) Supplemental Antennas Reserved (Not applicable to this solicitation)

(7) Supplemental Radio Kit Provisions Reserved (Not applicable to this solicitation)

(8) Supplemental Air Attack Kit Provisions Reserved (Not applicable to this solicitation)

(9) Supplemental Radio Kits Reserved (Not applicable to this solicitation)

(10) Supplemental Air Attack Kits Reserved (Not applicable to this solicitation)

(11) VHF-FM Programming Ports

DB-9 type D-subminiature connectors shall be installed in a location convenient to the SIC/observer. These shall be wired for RS232 serial communication between all required VHF-FM radios and a laptop computer. Individual connectors or an FM select switch may be used. Pin 2 shall be data transmitted from the FM. Pin 3 shall be data received by the FM. Pin 5 shall be signal ground. Compatible radio front panel connectors may be used to meet this requirement if serial adapter cables are provided with the aircraft. For example TDFM 136A radios s/n FDA1200 and higher.

(12) GPS Data Connectors(Reserved (Not applicable to this solicitation)

(13) External Portable Aviation GPS Antennas Reserved (Not applicable to this solicitation)

B.10 AVIONICS INSTALLATION AND MAINTENANCE STANDARDS

All avionics used to meet this agreement shall comply with the manufacturer’s specifications and installation instructions, federal regulations, and the following requirements.

(a) Strict adherence to the guidelines in FAA AC 43.13-1B Chapter 11 “Aircraft Electrical Systems” and Chapter 12 “Aircraft Avionics Systems” as well as FAA AC 43.13-2B Chapter 1 “Structural Data”, Chapter 2 “Communication, Navigation and Emergency Locator Transmitter System Installations” and Chapter 3 “Antenna Installation” is required.

(b) All antennas shall be FAA approved, have a Voltage Standing Wave Ratio (VSWR) less than 3.0 to 1 and be properly matched and polarized to their associated avionics system.

(c) Labeling and marking of all avionics controls and equipment shall be understandable, legible, and permanent. Electronic label marking is acceptable.

(d) Avionics installations shall not interfere with passenger safety, space or comfort. Avionics equipment shall not be mounted under seats designed for energy attenuation. In all instances, the designated areas for collapse shall be protected.

(e) All avionics equipment shall be included on the aircraft’s equipment list by model, nomenclature, and location.

(f) Avionics systems shall meet the performance specifications of FS/OAS A-24 Avionics Operational Test Standards. For a copy of all FS/OAS documents visit http://www.nifc.gov/NIICD/documents.html

B.11 AIRCRAFT AND EQUIPMENT SECURITY

(a) The Contractor is responsible for the security of their aircraft, vehicles, and associated equipment used in the support of this contract.

(b) Any aircraft used under this contract will be physically secured and disabled via a dual-lock method whenever the aircraft is unattended. Any combinations of anti-theft devices designed to lock the aircraft flight control surfaces when not in use, or designed to secure an aircraft to the ground, are acceptable, provided they are appropriate for the aircraft. Operational environments and personnel safety must be considered when selecting the locking devices and methods to be used.

(c) Removal and/or disabling of locking devices and methods must be incorporated into preflight checklists to prevent accidental damage to the aircraft and must be installed in a manner which precludes its inadvertent interference with in-flight operations.

(d) Examples of Acceptable Locking Devices and Methods are identified below. Utilization of other means of securing or disabling an aircraft are acceptable provided they achieve a level of security equal to or greater than the following examples methods.

(1) Keyed Magneto

(2) Keyed to Starter Switch

(3) Keyed to Master Power Switch

(4) Hidden Battery Cut-Off Switches

(5) Hidden Relay Switches

(6) Throttle/Power Lever Lock

(7) Mixture/Fuel Lever Lock

(8) Locking Fuel Cut-Off

(9) Locking Tie –Down Cable

(10) Locking Control Surface “Gust-Lock”

(11) Propeller Lock

(12) Propeller Chain Lock

(13) Propeller Cable Lock

(14) Locking Wheel Lock or Chock

(15) Locking “Club-type Devices or Control Yoke

(e) Examples of Unacceptable Locking Devices and Methods

(1) Locking aircraft doors

(2) Fenced or gated parking area

B.12 AIRCRAFT MAINTENANCE

(a) All aircraft shall be maintained to 14 CFR Part 135 standards. The Contractor shall provide or arrange for sufficient maintenance capability to keep the aircraft in airworthy condition. The Contractor shall provide maintenance when needed, either by an A&P mechanic at the designated base, or at an approved maintenance facility.

(b) The Contractor shall identify to the Government the maintenance facilities and/or maintenance personnel used to fulfill the requirements of this contract.

(c) Aircraft operated with components and accessories on approved TBO extension programs are acceptable provided the Contractor who provides the aircraft must be the holder of the approved extension authorization (not the owner if the aircraft is leased), and shall operate in accordance with the extension.

(d) Mechanics assigned to work on aircraft shall have appropriate FAA certification and ratings or shall at all times be working in the presence of one so certified and rated.

(e) Compliance with applicable mandatory manufacturer's bulletins, as required by operations specifications, FAA Airworthiness Directives (AD), and the correction of maintenance deficiencies shall be accomplished prior to delivery and continue during contract performance.

(f) All maintenance shall be accomplished in accordance with the standards established by 14 CFR Part 135; Advisory Circular (AC) 43.13, and the manufacturer's instructions and in accordance with those procedures established in the Contractor's maintenance program approved under 14 CFR Part 135 Operations Specifications.

(g) A copy of the current maintenance record required by 14 CFR 91.417 shall be kept at the Principal Base of Operation or maintenance facility.

(h) A test flight shall be performed at the Contractor's expense following overhaul, repair, and replacement of any engine (installations of reciprocating engines that are new, rebuilt, or overhauled shall accumulate 3-hours of operation, including 2 hours in flight, prior to Government use), power train, or control equipment, and following any adjustment of the flight control systems before the aircraft resumes service under this contract. The result of any test flight shall be logged in the aircraft flight records by the Pilot. Results of test flights shall be reported to the U.S. Forest Service Aircraft Maintenance Inspector (AMI) before the aircraft is returned to contract availability.

(i) When any non-scheduled maintenance or repairs are performed due to mechanical or equipment deficiencies, a Government Aircraft Maintenance Inspector and the Contracting Officer shall be notified for "return to contract available” status, before the aircraft performs under the contract.

(j) The Interagency Airplane Data Record Card shall be posted inside the aircraft.

(k) All weighing of aircraft shall be performed on scales that have been certified accurate within the previous 12 months. The certifying agency may be any accredited weights and measures laboratory.

B.13 PERSONNEL

Pilot Experience Requirements. The Pilot-in-Command shall hold a currently valid FAA commercial or higher pilot certificate with instrument rating. In addition, the pilot shall also have logged flight time as Pilot-in-Command in fixed-wing aircraft of at least the following minimum amounts:

(a) Flight Hours Experience

All airplanes Flying hours Total time 1500 Pilot in command total 1200 Pilot in command, as follows:

Category and class to be flown 200 Fixed wing – preceding 12-months 100

Cross Country 500 Operations in Mountainous terrain* 200

Night 100 Instrument – in flight 50 Instrument – actual/simulated 75 Make and model to be flown 25

Make & Model- preceding 60-days 10

*Low level mountainous terrain is flight at 2500 feet AGL and below in terrain identified as mountainous in 14 CFR 95.11 and depicted in the Aeronautical Information Manual (AIM) Figure 5-6-2.

(b) Each Pilot-in-Command shall, at the discretion of the Contracting Officer, pass a Government evaluation ride (not to exceed 2-hours) in make and model over mountainous or typical terrain.

Note: Mountainous vs. Typical depends upon location of designated base.

(c) The Pilot-in-Command shall be capable of performing basic programming functions and operations of Contractor installed aircraft avionics. This includes the ability to enter and utilize newly assigned frequencies and tones by selected channel positions.

The Pilot-in-Command shall be able to instruct the Agency observer in how to perform basic programming and operation of VHF-AM and VHF-FM radios, and GPS.

(d) All pilots must possess a Class I or Class II FAA medical certificate.

(e) All pilots shall possess and carry a current Interagency Airplane Pilot Qualification Card or Point-to-Point Only Pilot Qualification Card, in accordance with the Schedule of Items.

(f) Pilots must speak English fluently.

Pilot Approvals and Qualifications and Background Investigation

Homeland Security Presidential Directive (HSPD) 12 background investigations are no longer required by contract. Flight crew member record checks are required in accordance with 49 USC 44703 and 49 CRF 1544.230, regardless of the type of operation being conducted (parts 91,121,125,133,135,137 or public aircraft). The contractor will request, receive, and evaluate performance and safety related information (as specified by the law and regulation) before allowing any pilot to begin service as a flight crew member under this contract. Records of compliance will be made available for review when requested by the contracting officer or designated government representative.

B.14 FLIGHT HOUR AND DUTY LIMITATIONS

(a) Pilots.

(1) Flight limitations. Flight crewmembers shall be subject to the following flight hour limitations:

(i) All flight time, regardless of…