AG-024B-S-15-9011_ASM_Bridge_Solicitation.pdf

SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS

OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24, & 30

1. REQUISITION NUMBER

2. CONTRACT NO.

3. AWARD/EFFECTIVE

DATE

4. ORDER NUMBER

5. SOLICITATION NUMBER

AG-024B-S-15-9011

6. SOLICITATION ISSUE

DATE

03/18/2015

7. FOR SOLICITATION

INFORMATION CALL:

a. NAME

KELLEN LOGAN

b. TELEPHONE NUMBER (No collect calls)

(208) 387-5361

8. OFFER DUE DATE/

LOCAL TIME

04/03/2015

4:30 PM MT

9. ISSUED BY CODE 024b 10. THIS ACQUISITION IS UNRESTRICTED OR SET ASIDE: 100% FOR:

NATIONAL INTERAGENCY FIRE CENTER

U.S. FOREST SERVICE – CONTRACTING

OWYHEE BUILDING - MS 1100

3833 S. DEVELOPMENT AVE

BOISE, ID 83705-5354

SMALL BUSINESS

WOMEN-OWNED SMALL BUSINESS

(WOSB) ELIGIBLE UNDER THE WOMEN-OWNED

SMALL BUSINESS PROGRAM

HUBZONE SMALL

BUSINESS (EDWOSB) NAICS: 532411

SERVICE-DISABLED

VETERAN-OWNED

SMALL BUSINESS

8 (A)

SIZE STANDARD:

$32.5 M

11. DELIVERY FOR FOB DESTINA-

TON UNLESS BLOCK IS

MARKED

SEE SCHEDULE

12. DISCOUNT TERMS

13a. THIS CONTRACT IS A

RATED ORDER UNDER

DPAS (15 CFR 700)

13b. RATING

14. METHOD OF SOLICITATION

RFQ IFB RFP

15. DELIVER TO CODE 16. ADMINISTERED BY CODE

U.S. FOREST SERVICE - CONTRACTING

NATIONAL INTERAGENCY FIRE CENTER

3833 S. DEVELOPMENT AVENUE

BOISE, ID 83705-5354

17a. CONTRACTOR/ CODE FACILITY 18a. PAYMENT WILL BE MADE BY CODE

OFFEROR CODE

ALBUQUERQUE SERVICE CENTER

INCIDENT BUSINESS – CONTRACTS

101B SUN AVENUE, NE

ALBUQUERQUE, NM 87109

TELEPHONE NO. NINE-DIGIT DUNS NO. .

17b CHECK IF REMITTANCE IS DIFFERENT AND PUT SUCH ADDRESS IN

OFFER

18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a UNLESS BLOCK BELOW

IS CHECKED

SEE ADDENDUM

19.

ITEM NO.

20.

SCHEDULE OF SUPPLIES/SERVICES

21.

QUANTITY

22.

UNIT

23.

UNIT PRICE

24.

AMOUNT

See Schedule B (attached) Minimum Quantity ten (10) aircraft Maximum Quantity fifteen (15) aircraft.

25. ACCOUNTING AND APPROPRIATION DATA

26. TOTAL AWARD AMOUNT (For Govt. Use Only)

27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1, 52.212-4. FAR 52.212-3 AND 52.212-5 ARE ATTACHED. ADDENDA ARE ARE NOT ATTACHED

27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4. FAR 52.212-5 IS ATTACHED. ADDENDA ARE ARE NOT ATTACHED

28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN 3 .

COPIES TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND

DELIVER ALL ITEMS SET FORTH OR OTHERWISE IDENTIFIED ABOVE AND ON ANY

ADDITIONAL SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED

HEREIN.

29. AWARD OF CONTRACT: REF. _________________ __ OFFER

DATED _______________ . YOUR OFFER ON SOLICITATION (BLOCK

5), INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE SET

FORTH HEREIN, IS ACCEPTED AS TO ITEMS:

30a. SIGNATURE OF OFFEROR/CONTRACTOR 31a. UNITED STATES OF AMERICA (SIGNATURE OF CONTRACTING OFFICER)

30b. NAME AND TITLE OF SIGNED (Type or print) 30c. DATE SIGNED 31b. NAME OF CONTRACTING OFFICER (Type or print) 31c. DATE SIGNED

AUTHORIZED FOR LOCAL REPRODUCTION

PREVIOUS EDITION NOT USABLE STANDARD FORM 1449 (REV. 2/2012)

Prescribed by GSA - FAR (48 CFR) 53.212

Solicitation No. AG-024B-S-15-9011 US Forest Service Aerial Supervision Module (ASM) Platforms National Office

TABLE OF CONTENTS

i

SECTION A – SOLICITATION/CONTRACT FORM

SECTION B – SUPPLIES OR SERVICES AND PRICES/COSTS

B.1 LEASED AIRCRAFT

B.2 SCHEDULE OF ITEMS

SECTION C - DESCRIPTION/ SPECIFICATIONS/EXHIBITS

C.1 BACKGROUND

C.2 SCOPE OF CONTRACT

C.3 TECHNICAL REQUIREMENTS AND GENERAL AIRCRAFT SPECIFICATIONS

C.4 AVIONICS

C.5 ADDITIONAL SPECIAL MISSION EQUIPMENT

C.6 AIRCRAFT MAINTENANCE

C.7 ADDITIONAL GENERAL REQUIREMENTS and AIRCRAFT

APPEARANCE AND CONDITION

C.8 ACCIDENTS AND INCIDENTS

C.9 EQUIPMENT INSTALLATION

C.10 FUEL (PETROLEUM, OIL AND LUBRICANT- POL) AND OTHER

CONSUMABLES

C.11 GOVERNMENT PILOT EXPERIENCE

C.12 DESIGNATED BASE (DB)

C.13 CONTRACTOR’S REPRESENTATIVE

C.14 PUBLIC OFFICIALS NOT PERSONALLY LIABLE

C.15 ENVIRONMENTAL CONCERNS

C.16 AIRCRAFT SECURITY

C.17 SUBSTITUTION OR REPLACEMENT OF AIRCRAFT

C.18 AIRCRAFT MARKINGS

C.19 RETURN TO CONTRACT AVAILABILITY INSPECTIONS

C.20 PRE-USE INSPECTIONS

C.21 RE-INSPECTION EXPENSES

C.22 INSPECTION OF SUBSTITUTE EQUIPMENT

C.23 INSPECTIONS DURING USE

C.24 AIRCRAFT DOCUMENTATION

C.25 AIRCRAFT DEFICIENCY DOCUMENTATION

C.26 USE OF GOVERNMENT PROVIDED FACILITY HANGER

C.27 CONTRACT PERIOD

C.28 TIME OF DELIVERY

C.29 MANDATORY AVAILABILITY PERIOD (MAP)

C.30 UNAVAILABILITY

C.31 POINT OF DELIVERY

C.32 DELIVERY OF AIRCRAFT

C.33 DAILY AVAILABILTY REQUIREMENTS & PAYMENTS

C.34 METHOD OF PAYMENT – ELECTRONIC FUNDS TRANSFER

C.35 PAYMENT PROCEDURES

C.36 ACRONYMS & DEFINITIONS

TABLE OF CONTENTS

ii

SECTION D - CONTRACT CLAUSES

D-1 CONTRACT CLAUSES INCORPORATED BY REFERENCE

D.2 ADDENDUM TO 52.212-4 CONTRACT TERMS AND CONDITIONS -

COMMERCIAL ITEMS

D.3 CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT

STATUTES OR EXECUTIVE ORDERS -- COMMERCIAL ITEMS

D.4 PERIOD OF PERFORMANCE

D.5 OPTION TO EXTEND SERVICES

D.6 OPTION TO EXTEND THE TERM OF THE CONTRACT

D.7 COMMERCIAL FILMING AND VIDEOTAPING

D.8 PROPERTY AND PERSONAL DAMAGE

D.9 ASSURANCE REGARDING FELONY CONVICTION OR TAX

DELINQUENT STATUS FOR CORPORATE APPLICANTS

D.10 CONTRACTOR PERFORMANCE ASSESSMENT REPORTING SYSTEM

(CPARS)

D.11 INSPECTION AND ACCEPTANCE

D.12 CONTRACTOR AUTHORIZED SIGNATURES

D.13 PRE-AWARD INSPECTION OF FACILITIES AND EQUIPMENT

D.14 DETAILED AIRCRAFT INFORMATION

SECTION E - SOLICITATION PROVISIONS

E.1 INSTRUCTIONS TO OFFERORS - COMMERCIAL ITEMS

E.2 EVALUATION – COMMERCIAL ITEMS

E.3 CONTRACT AWARD

E.4 CERTIFICATION REGARDING RESPONSIBILITY MATTERS

E.5 INFORMATION REGARDING RESPONSIBILITY MATTERS

E.6 OFFEROR REPRESENTATIONS AND CERTIFICATIONS –

COMMERCIAL ITEMS

E.7 SERVICE OF PROTEST

E.8 REPRESENTATION BY CORPORATIONS REGARDING AN UNPAID

DELINQUENT TAX LIABILITY OR A FELONY CONVICTION

E.9 SIZE STANDARD AND NAICS CODE INFORMATION

E.10 INQUIRIES

E.11 EVALUATION OF OPTIONS

E.12 PRE-BID/ PRE-PROPOSAL CONFERENCE

E.13 POST-AWARD CONFERENCE

E.14 LIST OF ATTACHMENTS

ATTACHMENT A - LEASED AIRCRAFT CONTRACT PERFORMANCE

EVALUATION

ATTACHMENT B - SUMMARY OF ACCIDENTS

ATTACHMENT C – AIRCRAFT MAINTENANCE LOG

ATTACHMENT D - PAST PERFORMANCE QUESTIONNAIRE

SECTION B

SUPPLIES OR SERVICES AND PRICES/COSTS

The Government plans to award Firm Fixed Price type contract(s), with fixed-price rates for the dry lease of aircraft and flight hours used. The number of flight hours is dependent upon the amount of wild land fire and other related activities each year, which makes estimating the total overall contract quantity of flight hours difficult to predict. Many variables determine the severity and the length of fire seasons, including weather and local or regional long-term climate trends such as droughts or unusually wet periods. Two to four hundred (200-400) flight hours are estimated annually. However, this estimate IS NOT A REPRESENTATION OR A GUARANTEE to an offeror or Contractor that the estimated flight hour quantities will be incurred, or those conditions affecting requirements will be stable or normal. The Government requires that all aircraft are of the same make/model/series as defined for each CLIN’s performance requirements, for this acquisition.

B.1 LEASED AIRCRAFT

This acquisition is for a minimum of 10 and up to a maximum of 15 aircraft (over the life of the contract) to be rented on a dry lease basis, with contractor provided maintenance and insurance, available for the exclusive use by Government pilots for wild land fire missions and other administrative activities. The daily rate is to accommodate payment flexibility for inconsistent days in a month or in a year.

All aircraft under the resultant contract shall be ready for delivery on JULY 01, 2015 to the US Forest Service. Delivery will occur at the Contractor’s base of operations or other mutually agreed upon location.

This solicitation is for the dry lease (aircraft only, without fuel, crews, or pilots) of a minimum of TEN (10) aircraft. One award of all three Contract Line Item Numbers (CLIN’s) or multiple awards of the individual CLIN’s (one for each CLIN or combination of CLIN’s) may be made.

B.2 SCHEDULE OF ITEMS

Base Performance Period: July 1, 2015 - June 30, 2016.

Dry Lease of Aircraft - Flight Hours: Estimated to be 200 - 400 hours per year.

Option Period: One (1) six month option – July 01, 2016 thru December 31, 2016. FAR 52.217-8

CLIN 0001 - Year 2015 - 2016

SUBCLIN

N-

Number Make/Model Year Series

Hourly Fuel Consumption Gal.

Hourly Flight Rate

300 Hours (Estimated for evaluation)

Daily Availability

Rate

Total Availability (Daily x 365

Days) 01A 01B 01C 01D 01E

CLIN 0002 - Year 2015 - 2016

SUBCLIN

N-

Number Make/Model Year Series

Hourly Fuel Consumption Gal.

evaluation)

Daily Availability

Rate

Total Availability (Daily x 365

Days) 02A .

02B 02C 02D 02E

CLIN 0003 - Year 2015 - 2016

N-

Number Make/Model Year Series

Hourly Fuel Consumption

Gal.

evaluation)

Daily Availability

Rate

Total Availability

(Daily x 365 days)

03A 03B 03C 03D 03E

CLIN 0001 – Option Period July 1, 2016 – December 31, 2016

N-

Number Make/Model Year Series

Hourly Fuel Consumption

Gal.

150 Hours evaluation)

Daily Availability

Rate

Total Availability

(Daily x 365 days)

03A 03B 03C

CLIN 0002 - Option Period July 1, 2016 – December 31, 2016

N-

Number Make/Model Year Series

Hourly Fuel Consumption

Gal.

evaluation)

Daily Availability

Rate

Total Availability

(Daily x 365 days)

03A 03B 03C

CLIN 0003 - Option Period July 1, 2016 – December 31, 2016

N-

Number Make/Model Year Series

Hourly Fuel Consumption

Gal.

evaluation)

Daily Availability

Rate

Total Availability

(Daily x 365 days)

03A 03B 03C

CLIN 04 - Year 2015 - 2016

Provide for other direct costs (ODC) for design work, technical drawings, aircraft modifications, and miscellaneous technical services for the contracted aircraft over and above normal maintenance. This may be used on a case by case basis as may be requested by the Government (IAW FAR 52.212-4(c) and only by Contracting Officer direction with the issuance of a contract modification. The ABS billing will be for miscellaneous items and noted as such in the ABS invoicing system.

FOR PROPOSAL/BIDDING PURPOSES ONLY THE FOLLOWING DOLLAR FIGURE WILL BE USED FOR ALL SUBMITTED PROPOSALS. THIS CLIN, IF UTILIZED DURING THE CONTRACT PERFORMANCE PERIOD WILL BE FUNDED ON A CASE BY

CASE BASIS.

$ 50,000.00

SECTION C

DESCRIPTIONS/SPECIFICATIONS/EXHIBITS

C.1 BACKGROUND

The United States Forest Service (USFS) is responsible for protecting National Forest lands from wild land fires and, by agreement with other agencies, assists in protecting other jurisdictions. The FS has accomplished this mission by sharing resources with other State and Government cooperators. Since the 1950s, the FS has placed increasing reliance on fixed and rotor wing aircraft to support fire suppression operations. Aircraft are used to drop fire retardant, deliver smokejumpers to remote areas, deliver helitack firefighters for passenger and cargo transportation, and to provide logistical and administrative support.

To ensure the efficiency and safety of aviation operations, the FS deploys airborne Aerial Supervision Module (ASM) platforms for in-flight supervision on fires and to conduct other administrative support activities. When the aircraft is performing the low level support role (Lead plane), the mission will consist of directing and guiding air tankers into fire areas and as necessary “leading” them during the actual retardant drop, at times operating below 500 feet above ground level (AGL) in steep mountainous terrain and turbulent conditions. The air attack mission (ATGS) consists of operating above 500’ (AGL) and coordinating tactical use of all aircraft working at the incident. The ASM role combines both the Lead plane and ATGS role into one. The administrative support mission includes carrying passengers and/or cargo.

C.2 SCOPE OF CONTRACT

This solicitation is for the dry lease (aircraft only, without fuel, crews, or pilots) of a minimum of TEN (10) and a maximum of up to FIFTEEN (15) aircraft and includes complete contractor provided maintenance support. The aircraft shall be made available from 01 July 2015. The base period of performance will be from Contract Award through June 30, 2016 with one (1) six

(6) month option period with a period of performance from July 01, 2016 through December 31, 2016. The aircraft will be utilized by USFS National and Regional aviation groups for support of fire and aviation management activities.

This solicitation and resultant commercial, Firm Fixed Price (FFP) type contracts will be awarded for the dry lease of manufacturer built, dual-engine, turbine powered aircraft. The Contractor shall make the aircraft available for year-round, exclusive use by Federal Government pilots for missions associated with supporting wild land fire suppression. Other types of work to a lesser degree will be resource management, passenger and cargo transportation, law enforcement, pilot training, pilot proficiency, and administrative activities.

The ASM mission consists of directing and guiding large air tankers into a fire area, and as necessary, “leading” them during actual retardant drop. This means operating below 500 feet AGL in steep mountainous terrain in turbulent conditions. The aircraft may have other Government employees on board as an Air Tactical Group Supervisor (ATGS), an instructor, and/or trainee. Mission/Agency qualified Government pilots will operate all of these aircraft.

The Contractor shall provide the aircraft and complete maintenance of the aircraft. The Government shall provide all of the fuel. The contractors shall provide all oxygen, petroleum, oils, and lubricants (POL) for the aircraft. The Government will operate in accordance with the United States Department of Agriculture Forest Service Manual FSM 5700 – Aviation Management and all applicable portions of 14 CFR Part 91.

The resultant contract shall require the contractor to provide aircraft that, at the initial delivery of the aircraft, and after the completion of all maintenance (both scheduled and unscheduled), are

(1) neat and clean in appearance, (2) fully operable and maintained to 14 CFR 135 inspection standards or equivalent and manufacturers recommendations with an FAA approved Minimum Equipment List (MEL) and appropriate Letter of Authorization (LOA), listing the aircraft, (3) equipped with calibrated and marked instruments and radios, (4) in good condition both visually and operationally, and (5) timely and properly maintained in compliance with 14 CFR Parts 43 and 91, mandatory manufacturer’s service bulletins and FAA AD’s. The aircraft may be used for other FS cooperator wild land fire needs (i.e. Federal, State, and local Agencies) within North America.

C.3 TECHNICAL REQUIREMENTS AND GENERAL AIRCRAFT SPECIFICATIONS

The offeror’s shall provide specific written authorization from the aircraft manufacturer by make, model, series, and serial number for operation in the firefighting environment. The aircraft must have a manufacturer approved maintenance and inspection program that accounts for usage in the firefighting environment. The aircraft shall be FAA certificated as a Normal, Standard, or Utility category dual-engine airplane, be certificated for single pilot operation with a minimum flight deck capacity of two with dual controls plus a minimum passenger capacity of two.

The airplane must be in current production, dual-engine, turboprop, manufacturer built (no amateur or manufacturer built kit aircraft), new or used. The airplane shall be air-conditioned and pressurized with a target 230 knots true airspeed (KTAS) cruise speed. The airplane shall have a minimum maneuvering speed (Va) of 150 Knots Indicated Airspeed (KIAS) or greater and a flight endurance of four (4) hours or longer with a payload of at least 800 pounds. The aircraft, must have a minimum controllable airspeed (Vmca) of 100 KIAS or lower, a single engine service ceiling of 12,500 feet or higher (pressure altitude and standard temperature) and the ability to maintain a single engine rate of climb at 120 KIAS or slower. The airplane shall have a maximum gross take-off weight of no more than 19,000 pounds. The minimum scheduled maintenance interval must be no less than 200 hours. The airplane must have auto feather or similar system capable of automatically feathering the propeller of a failed engine. If equipped with retractable landing gear, a gear warning horn silence button must be mounted on the pilot’s yoke or power levers to facilitate silencing the horn with the flaps up or in an approach position regardless of power lever position.

C.4 AVIONICS

(a) MINIMUM REQUIREMENTS

All avionics used to meet this agreement shall comply with the requirements of paragraph b.

(AVIONICS SPECIFICATIONS) and paragraph c. (AVIONICS INSTALLATION AND

MAINTENANCE STANDARDS).

The following are the minimum avionics which shall be installed. Additional avionics may be required. Please read this document thoroughly.

(1) Aerial Supervision Module (ASM) Aircraft

ASM aircraft shall be approved for day and night Visual Flight Rules (VFR), Instrument Flight Rules (IFR), and flight into known icing conditions. Aircraft with identical avionics, autopilots and flight directors are preferred.

(i) Two VHF-AM Radios (COM 1, COM 2)

(ii) Three VHF-FM Radios (FM 1, FM 2 & FM 3)

(iii) FM channeling switches on the PICs yoke for FM 1 and FM 2

(iv) An Intercom System (ICS) for the PIC, SIC/observer and Instructor (directly behind the SIC/observer)

(v) Separate Audio Control systems for the PIC, SIC/observer and Instructor

(vi) Bose series X jacks for the PIC and SIC/observer

(vii) Controls for the PIC, SIC/observer and Instructor to each independently adjust headphone volume for each communications receiver. These controls shall be a built in, integral part of each audio controller.

(viii) Individual cockpit speakers for the PIC and SIC/observer

(ix) Controls for the PIC and SIC/observer to each independently select and adjust speaker volume, independent of headset audio, for each communications receiver

(x) One IFR certified WAAS Global Positioning Systems (GPS) with moving map

(xi) An Emergency Locator Transmitter (ELT) certified to TSO-C126

(xii) An Automated Flight Following system (AFF)

(xiii) One Mode S Transponder

(xiv) One Altimeter and Automatic Pressure Altitude Reporting system

(xv) One Traffic Collision Avoidance System (TCAS) with 1 mile display selection

(xvi) A Three Axis Autopilot (Roll, Pitch, and Yaw)

(xvii) One RADAR Altimeter

(xviii) One Multi-Function Display (MFD)

(xix) Equipment and lighting for night VFR operations in accordance with 14 CFR

135.159 and 14 CFR 135.161

(xx) Two VOR/Localizer systems

(xxi) One Glideslope system interfaced to the #1 Localizer

(xxii) One Three Light Marker Beacon system

(xxiii) One Weather RADAR system usable during all flight conditions

(xxiv) One Satellite Weather system with XM Aviator subscription or equivalent

(xxv) One Class B Terrain Awareness and Warning System (TAWS)

(xxvi) An Auxiliary Power Source at the Instructor Position

(b) AVIONICS SPECIFICATIONS

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

(1) Communications systems

(i) 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.

(ii) 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.

(A) 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.

(B) 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.

(C) 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.

(D) 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.

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

(2) Audio Systems

(i) 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.

(ii) Audio Control systems

(A) 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, COM-2, COM-3, FM-1, FM-2, FM-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.

(B) Drop Cord Requirements

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

2. 6-Pin MS3476L10-6P type connector on the coil cord

3. JJ-033 and JJ-034 type headset jacks at the housing

4. Large clip

5. Volume control

6. ICS switch with momentary and lock positions

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

(C) Aft Audio Control systems

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.

(D) Required Audio Control systems

The following audio control systems are required for ASM aircraft.

1. Two separate audio control systems for the PIC and SIC/observer. These shall be identical individual units.

2. An aft audio control system for the instructor

3. Drop cords for the SIC/observer and instructor

(3) Navigation systems

(i) Global Positioning Systems (GPS)

(A) 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. A current IFR GPS navigation database shall be maintained covering the continental United States. Aircraft operating in Alaska shall include an Alaskan database in the coverage.

(B) (Reserved)

(C) 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.

(4) Surveillance systems

(i) 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 C126 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.

(ii) 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.

(A) 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.

(B) 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.

(C) 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/ .

(D) 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.

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

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

(iii) Transponders

Transponder systems shall meet the requirements of 14 CFR 91.215(a). ASM aircraft shall have a “Mode S” transponder installed. Transponder systems shall be tested and inspected every 24 calendar months as specified by 14 CFR 91.413.

(iv) 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.

(v) Traffic Collision Avoidance Systems (TCAS)

Traffic Collision Avoidance 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 1 miles or less.

(5) General Systems

(i)Autopilots

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

Autopilots in ASM aircraft shall be certified for IFR approach procedures, couple to the navigation systems for vertical and horizontal operation, interface to the PICs flight director and HSI, and provide altitude preselect, automatic trim, and PIC electric trim controls.

(ii) RADAR Altimeters

RADAR altimeters shall be approved, operate from zero to a minimum of 2000 feet AGL and provide the operator an adjustable cursor which enables an altitude low (decision height) annunciation. The altitude low annunciation shall be clearly identified, and in the PIC’s primary field of view.

(iii) Multi-Function Displays (MFD)

MFDs 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.

(iv) Cockpit Voice Recorder (CVR)

Cockpit voice recorders shall meet all applicable regulations for standard and transport category aircraft.

(v) Auxiliary Power Source (3 Pin)

An MS3112E12-3S type connector shall be installed and mounted in a location convenient to the SIC/observer and protected by a 10 Amp circuit breaker. Pin A shall be +28 VDC in 28 Volt aircraft. Pin B shall be airframe ground. Pin C shall be +14 VDC in 14 Volt aircraft. Pins A and C shall never be simultaneously wired to the connector. Refer to FS/OAS A-16.

(vi) 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.

(c) 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.

(1) 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.

(2) 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.

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

(4) 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.

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

(6) 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 .

C.5 ADDITIONAL SPECIAL MISSION EQUIPMENT

(a) All aircraft shall have:

(1) Safety Belts. The aircraft furnished under this contract shall have one set of lap safety belts for all occupants and double strap shoulder harness with automatic or manual locking inertia reel harnesses type safety belts for front seat occupants meeting the requirements of 14 CFR. The shoulder straps and lap belts shall fasten with one single point metal to metal quick release mechanism. Single shoulder harness safety belts shall be provided for all passenger seats. Military style harnesses are acceptable.

Lap belt and shoulder harness condition – the following ARE NOT acceptable:

(i) Webbing: Webbing that is frayed five percent (5%) or more, torn webbing, crushed webbing, swelled webbing that results in twice the thickness of the original web, or if difficult to operate through hardware, creased webbing (no structural damage allowed), and sun deterioration if it results in severe fading, brittleness, discoloration, and stiffness.

(ii) Hardware: Buckle or other hardware is inoperable, nylon bushing at shoulder harness-to-lap belt connection missing or damaged, fabricated bushings or tie wraps used as bushings, rust/corrosion if not minor in nature, wear beyond normal use.

(iii) Stitches: Broken or missing stitches, severe fading or discoloring, inconsistent stitch pattern.

(iv) Technical Standard Order (TSO) Tags (see 14 CFR 21.607): Missing or illegible tags are unacceptable unless inspection can confirm the suitability of installed equipment.

(v) Age: Belts/fabric over ten (10) years from the date of manufacture require close inspection because of the elements they are exposed to, but do not have to be replaced if it can be determined they are in serviceable condition and not life limited.

(2) Fire extinguisher(s), as required by 14 CFR 135.155, shall be a handheld bottle, minimum 1.5 pounds capacity, containing Class B and C extinguishing agent, mounted and accessible to the flight crew.

(3) The aircraft shall be equipped with a wing and tail strobe light system with an independent activating switch.

(4) The aircraft shall be equipped with a pulse type light system to enhance recognition of the aircraft. The system may utilize existing landing lights if they are visible with the landing gear retracted. A pulselite model 1220/2410-2 or equal will meet this requirement.

(5) Cabin air conditioning vents, bleed air heater and window defogger shall be controllable by the pilot.

(6) Aircraft will have an oxygen system capable of supplying the pilot, copilot and all available passenger stations with aviator breathing oxygen for a minimum of .8 hours for all positions minimum. The oxygen system will be a continuous flow system in accordance with

14 CFR 135.157.

(7) First Aid Kit (Aeronautical)

Each kit shall be in a dust-proof and moisture-proof container. The kit shall be on board the aircraft and accessible to the occupants. Kits may be commercially available types, which are FAA approved for the appropriate number of crew and passengers carried. The contents shall include the following minimum items:

Item Description Passenger Seats (0-9)

Passenger Seats

(10-15) Adhesive bandage strips (3 inches long) 8 16 Antiseptic or alcohol wipes (packets) 10 20 Bandage compresses, (4-inch) 2 4 Triangular bandage compresses, 40 inch (sling) 2 4 Roller bandage, 4 inch x 5 yards (gauze) 2 4 Adhesive tape, 1 inch x 5 yards (standard roll) 1 2 Bandage scissors 1 1 Body Fluids Barrier Kit: 1 1 2-pair of latex gloves 1-face shield 1-mouth-to-mouth barrier 1-protective gown 2-antiseptic towelettes 1-biohazard disposal bag

Note: Splints are recommended if space permits.

(8) Survival Kit (Aeronautical) (LOWER 48)

The contents shall include the following minimum items:

Item Item

Knife Signal Mirror Non-Marine Aerial Flares(6-each) Matches (2-small boxes in waterproof containers) Food (2-days @ a minimum 1,000 calories per day, emergency rations per occupant)

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

Space Blanket (1-per occupant) Candles Collapsible Water Bag Whistle Magnesium Fire Starter Nylon Rope or Parachute Cord (50-feet) Water Purification Tablets

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 Headnet (1-per occupant) Gill Net/Assorted Fishing Tackle Personal ELT Sunscreen

Note: A hand-held 760 channel VHF transceiver radio is recommended.

It should be attached, or immediately accessible, to a crewmember rather than placed in the aircraft survival kit.

(9) SMOKE GENERATOR

Aircraft shall be equipped with an FAA approved smoke generating system, actuated from the controls of the left seat pilot position.

(10) Hobbs meter (flight hour meter) that measures actual flight time from takeoff to landing in hours and tenths.

C.6 AIRCRAFT MAINTENANCE

(a) The Contractor is required to provide the complete maintenance of the aircraft. The aircraft shall be timely and properly maintained in compliance with the requirements of 14 CFR Parts 43, 91, and additional requirements in this section.

The contractor must perform the mandatory manufacturer’s service bulletins and FAA AD’s, but will coordinate with the respective Project Inspector (PI) and COR to minimize contract performance disruption. The Contractor shall correct all maintenance discrepancies prior to the start of the base performance period and each option period thereafter. The contractor shall correct all maintenance discrepancies as they become known. Refer to Section C.19 for Return to Contract Availability. The Contractor will assure that all maintenance performed on contract aircraft is recorded in the aircraft’s maintenance record and appropriate Aircraft Maintenance Log (FS 5700-E) that is with the aircraft.

(b) All aircraft maintenance inspections shall be performed in accordance with the manufacturer and FAA approved continuous airworthiness inspection program applicable to the aircraft prior to the start of the contract. All phase inspections will be conducted by FAA approved repair stations with a rating for the specific aircraft offered and have technicians who perform scheduled inspections with factory training for the offered aircraft. All unscheduled maintenance shall be performed by a FAA approve repair station with a rating specific to the aircraft offered.

Such unscheduled maintenance shall be communicated and a return to contract availability approved thru an agency aviation maintenance inspector prior to commencing operations.

Contractor will provide in each aircraft a current aircraft maintenance due list detailing aircraft components or system due maintenance or inspection through the next phase inspection or six months, whichever is greater. This list shall include the next time and/or date due for the following:

Next Inspection/Phase Transponder certification Static system/Altimeter certification Aircraft weighing ELT battery due date

(c) A complete and updated Maintenance Status Report shall be available on-line to the appropriate USFS PI and AMI for each aircraft.

(d) Aircraft offered will be weighed every 36 months. At the time of weighing, scales shall have been calibrated within the last 12 months. Scale calibration date shall be noted on the weigh record.

(e) Aircraft offered must comply with the aircraft manufacturer's recommended maintenance programs, or a program approved by the FAA, for each aircraft, aircraft engine, propeller. A manufacturer's maintenance program is one which is contained in the maintenance manual or maintenance instructions set forth by the manufacturer for the aircraft, aircraft engine, or propeller.

C.7 ADDITIONAL GENERAL REQUIREMENTS and AIRCRAFT APPEARANCE AND

CONDITION

The aircraft shall present a neat and clean appearance at all times. All required accessories and appliances will be in operable condition. Instruments and radios shall be properly calibrated and marked. Upholstery, paint, and Plexiglas shall be in good condition.

All windows and windshields must be clean and free of scratches, cracks, crazing, distortion, or repairs which hinder visibility. The aircraft interior shall be clean and neat. There shall not be excessive tears, rips, cracks, or other damage to the upholstery, headliner, or interior of the aircraft. The exterior finish, including the paint, shall be clean, neat, and in good condition.

Upon completion of the contract, aircraft shall be returned to the Contractor in the same condition as received, excluding normal wear and tear.

C.8 ACCIDENTS AND INCIDENTS

The Contractor shall report to the Government the accident history for all the aircraft offered in this solicitation.

(a) “Accident(s)” shall mean destruction or substantial damage to the aircraft, aircraft components and any injury to personnel, as defined by the National Transportation Safety Board (NTSB)(49 CF Part 830).

(b) Following an “Aircraft Accident” or when requested by the NTSB following the notification of a reportable “Incident”, the Contractor shall provide the Agency with the information that is necessary to complete a NTSB Form 6120.1.

(c) “Incident(s) with Potential” shall mean an incident that narrowly misses being an accident in which the circumstances indicate significant potential for substantial damage or serious injury, or a deviation from standard procedures. Classification of an incident as an “Incident with Potential” is determined by the Agency and is reported into the Agency’s reporting system called the SAFCOM system.

(d) The Contractor shall not permit removal or alteration of the aircraft, aircraft equipment, or aircraft records following an Aircraft Accident or Incident with Potential. Exceptions are when threat to life or property exists; the aircraft is blocking an airport runway, etc. The CO shall be notified immediately when such actions take place. All wreckage equipment and records that are involved in an accident related to this contract shall be under the control of the CO or other persons or agencies designated by the CO until released. The NTSB’s release of the wreckage does not constitute a release by the CO.

(e) The Contractor agrees to fully cooperate in any investigation and to provide any required records, statements, or parts in the investigation of any accident(s) or serious incident(s).

If the Government deems it necessary to disassemble any of the aircraft or its components to determine probable cause of the accident or incident, the Government will be responsible for any costs for disassembling. The Contractor will be responsible for any costs involved in reassembly and approval for return-to-service and transportation of any item(s) disassembled by the Government.

C.9 EQUIPMENT INSTALLATION

Any additional Government equipment, authorized or requested by the CO, shall be installed and removed at the end of the contract period at the Government’s expense.

C.10 FUEL (PETROLEUM, OIL AND LUBRICANT- POL) AND OTHER CONSUMABLES

(a) The Government shall supply all aircraft fuel consumables during the contract period for which the aircraft is in available status.

(b) The contractor shall furnish fuel and an alternate method of payment for non-reimbursable flights (i.e. mobilization, demobilization, functional check flights, maintenance test flights, and maintenance ferry flights) and for occasions when the Government fuel card is not accepted.

Contractor shall provide all oils and other consumables required for aircraft lubrication.

Contractor shall provide aviators breathing oxygen.

C.11 GOVERNMENT PILOT EXPERIENCE

The Government pilots will meet the requirements of Forest Service Handbook (FSH) 5709.16, GS-12 minimums, 14 CFR Part 91.

C.12 DESIGNATED BASE (DB)

For the purpose of this solicitation and resultant lease, Boise, Idaho will be the Designated Base (DB). However, the aircraft themselves will be positioned throughout the country and physically located at various Forest Service locations to best meet the needs of the Government.

C.13 CONTRACTOR’S REPRESENTATIVE

Before work begins on this contract, preferably at the pre-work conference, the Contractor shall designate, in writing to the COR or CO, the person or persons who will represent and act for the Contractor in the Contractor’s absence from the job. In the designation letter, the Contractor shall describe the specific areas of responsibility that is assigned to the representative(s).

C.14 PUBLIC OFFICIALS NOT PERSONALLY LIABLE

There shall be no personal liability upon the Contracting Officer or officer in charge, their agents or employees, for any act performed in the discharge of any duty imposed or the exercise of any power or authority conferred upon them by, or within the scope of the contract, it being understood that in all such matters, they act solely as agents and representatives of the U.S.

Government and the U.S. Forest Service.

C.15 ENVIRONMENTAL CONCERNS

(a) The Contractor shall be responsible to ensure the maintenance activities do not cause environmental damage to property or facilities.

The Contractor will be responsible to clean and rehabilitate areas adversely affected by their activities and shall, whenever practical and possible, utilize solvents and cleaning agents that are either biodegradable or consistent with acceptable safety, health and environmental concern practices.

(b) The Government may, at its option, assign an area to be utilized by the vendor for storage of equipment used in support of contract performance. Oil, solvents, engines, etc., will be stored and utilized in a manner consistent with acceptable safety, health and environmental concerns and also acceptable to the Contracting Officer. The Contractor will provide the COR a Material Safety Data Sheet (MSDS) for any chemical used or brought onto the facility.

(c) The Contractor is responsible for the prevention of oil contamination of airport ramps, parking areas, etc. by their aircraft or personnel. When such contamination is caused by the Contractor’s aircraft or personnel, the Contractor is responsible for all clean-up.

C.16 AIRCRAFT SECURITY

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

(b) Aircraft Physical Security. Any aircraft used under this contract will be physically securable via a dual-lock method. Any combination of anti-theft devices designed to lock aircraft flight control surfaces when not in use, or designed to secure an aircraft to the ground, are acceptable, provided they are appropriate and the same for all aircraft.

Operational environments and personnel safety must be considered when selecting the locking devices and methods to be used. A spare key will be located on the aircraft for Government use and one retained by the contractor for its use.

(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 & Methods are identified below. Utilization of other means of securing or disabling an aircraft is acceptable provided they achieve a level of security equal to or greater than the following examples.

Keyed Master Power Switch Hidden Battery Cut-Off Switches Hidden Start Relay Switches Throttle/Power Lever Lock Mixture/Fuel Lever Lock Locking Fuel Cut-Off Locking Tie-Down Cable Locking Control Surface “Gust-Lock” Propeller Lock Propeller Chain Lock Propeller Cable Lock Locking Wheel Lock or Chock Locking “Club”-type Devices for Control Yoke

Examples of Unacceptable Locking Devices & Methods

Locking aircraft doors Fenced or gated parking area

C.17 SUBSTITUTION OR REPLACEMENT OF AIRCRAFT

(a) The Contractor may substitute or replace aircraft with the same make, model, and series as originally offered that meet all of the requirements of the resultant contract(s). The Contracting

Officer (CO) must approve any/all substitutions or replacements of aircraft prior to implementation.

(b) All requests for substitutions/replacements of aircraft shall be made at least ten (10) days prior, in writing to the Contracting Officer (CO), to the proposed exchange, except for during unforeseen conditions/situations.

(c) Any required flight time to facilitate the substitution or the replacement will be at the Contractor’s expense.

C.18 AIRCRAFT MARKINGS

Aircraft shall be marked with either paint or vinyl stick-on material with high visibility orange which contrasts with the primary paint color scheme. The markings/paint shall be applied to areas as outlined below:

(1) The outboard tips on the upper and lower surface of the wings

(2) The outboard tips on the upper and lower horizontal stabilizer surfaces

C.19 RETURN TO CONTRACT AVAILABILITY INSPECTIONS

Inspection by the Government after a contract deficiency or maintenance discrepancy will be made as promptly as possible after the Contractor has given written notice to the COR/COR that the item has been corrected. When an inspection reveals that the failure has been corrected, the Contractor will be deemed in “available” status from the time the Contractor gave notice to the Government of the correction of the failure and the aircraft was located at the designated location.