Amendment_01.pdf

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT

1. CONTRACT ID CODE PAGE OF PAGES

1 7

2. AMENDMENT/MODIFICATION NO. 3. EFFECTIVE DATE 4. REQUISITION/PURCHASE REQ. NO. 5. PROJECT NO. (If applicable)

Amendment 01 February 10, 2017

6. ISSUED BY CODE 7. ADMINISTERED BY (If other than Item 6) CODE

U.S. FOREST SERVICE - CONTRACTING

NATIONAL INTERAGENCY FIRE CENTER

OWYHEE BLDG – MS 1100

3833 S DEVELOPMENT AVE

BOISE ID 83705-5354

Same as Item 6

8. NAME AND ADDRESS OF CONTRACTOR (No., street, county, State and ZIP Code) 9A. AMENDMENT OF SOLICITATION NO.

AG-024B-S-17-0001

9B. DATED (SEE ITEM 11)

January 17, 2017

10A. MODIFICATION OF CONTRACT/ORDER NO.

10B. DATED (SEE ITEM 13)

CODE FACILITY CODE

11. THIS ITEM APPLIES ONLY TO AMENDMENTS OF SOLICITATIONS

The above numbered solicitation is amended as set forth in Item 14. The hour and date specified for receipt of Offers is extended, is not extended.

Offers must acknowledge receipt of this amendment prior to the hour and date specified in the solicitation or as amended, by one of the following methods:

(a) By completing Items 8 and 15, and returning 1 copies of the amendment; (b) By acknowledging receipt of this amendment on each copy of the offer submitted;

or (c) By separate letter or telegram which includes a reference to the solicitation and amendment numbers. FAILURE OF YOUR ACKNOWLEDGEMENT TO BE RECEIVED AT THE PLACE DESIGNATED FOR THE RECEIPT OF OFFERS PRIOR TO THE HOUR AND DATE SPECIFIED MAY RESULT IN REJECTION OF YOUR OFFER. If by virtue of this amendment you desire to change an offer already submitted, such change may be made by telegram or letter, provided each telegram or letter makes reference to the solicitation and this amendment, and is received prior to the opening hour and date specified.

12. ACCOUNTING AND APPROPRIATION DATA (if required)

13. THIS ITEM APPLIES ONLY TO MODIFICATIONS OF CONTRACTS/ORDERS.

IT MODIFIES THE CONTRACT/ORDER NUMBER AS DESCRIBED IN ITEM 14.

CHECK

ONE

A. THIS CHANGE ORDER IS PURSUANT TO: (specify authority) THE CHANGES SET FORTH IN ITEM 14 ARE MADE IN THE CONTRACT ORDER

NO. IN ITEM 10A.

B. THE ABOVE NUMBERED CONTRACT/ORDER IS MODIFIED TO REFLECT THE ADMINISTRATIVE CHANGES (such as changes in paying office, appropriation date, etc.) SET FORTH IN ITEM 14, PURSUANT TO THE AUTHORITY OF FAR 43.103(b).

C. THIS SUPPLEMENTAL AGREEMENT IS ENTERED INTO PURSUANT TO AUTHORITY OF:

D. OTHER (specify type of modification and authority)

E. IMPORTANT: Contractor is not, is required to sign this document and return copies to the issuing office.

14. DESCRIPTION OF AMENDMENT/MODIFICATION (Organized by UCF section headings, including solicitation/contract subject matter where feasible.)

A. Section B.6 and B.7: Authorize the installation of the Wing and Tail Strobe Lights, DME, Radar Altimeter, Additional Equipment, and General Equipment to be installed with an STC, TCDS, or an FAA Field Approval. Field Approval with 8110 acceptable means - Field Approved for installation with supporting FAA Form 8110-3 and all DER supporting engineering substantiation documentation attached.

B. Replacement pages attached with changes noted with bold and italicized text.

Except as provided herein, all terms and conditions of the document referenced in Item 9A or 10A, as heretofore changed, remains unchanged and in full force and effect.

15A. NAME AND TITLE OF SIGNER (Type or print) 16A. NAME AND TITLE OF CONTRACTING OFFICER (Type or print) MICHAEL MCFARLANE, Contracting Officer

15B. CONTRACTOR/OFFEROR 15C. DATE SIGNED 16B. UNITED STATES OF AMERICA 16C. DATE SIGNED

208-387-5695

(Signature of person authorized to sign) (Signature of Contracting Officer)

NSN 7540-01-152-8070

Previous edition unusable

STANDARD FORM 30 (REV. 10-83)

Prescribed By GSA FAR (48 CFR) 53.243

Solicitation No. AG-024B-S-17-0001 U.S. Forest Service Single Engine Turbine Aircraft National Office

SECTION B

SUPPLIES OR SERVICES AND PRICE

(8) Minimal visual obstructions from any aircraft structure to view up to 3 miles straight out, when terrain contour allows, from the pilot, copilot or any observer seat position side window. While seated the field of view shall allow 70 degrees down and 120 degrees forward to aft.

(9) Minimal to no window/windshield tinting is desirable or the ability to customize level of tint at the time of acquisition is required. In addition, exhaust distortion must be minimized for optimal mission performance.

(b) Mandatory Equipment Requirements:

(1) New manufactured airplane in current production.

(2) Equipped with single turbine engine.

(3) Meeting 14 CFR Part 36 Stage IV noise standards.

(4) Minimum Crew - One (1) pilot.

(5) Equipped with all weights, measures, markings, and instruments in Imperial units and in the English language.

(6) Equipped with an Environmental Control System (ECS) for all areas that could be occupied by aircrew and passengers. This includes heating and air conditioning for crew and passenger comfort.

(7) Seating for the pilot and copilot with dual flight controls.

(8) A double strap shoulder harness restraint system for pilot and copilot.

(9) Provisions for cargo restraints and seat track tie downs that will allow for the safe hauling of cargo.

(10) Provisions for a cargo door allowing an item with the dimension of 48 inches by 48 inches to be loaded and unloaded into the cabin area.

(11) Oxygen System capable of providing oxygen to all certificated seats.

(12) Dual Controls (Pilot and Co-Pilot Positions)

(13) Wing and Tail Strobe Lights with independent activation switch as well as a pulse type conspicuity lighting system (FAA Approval via 8110 authorized).

(c) Minimum Avionics Requirements:

(1) Primary Flight Displays (PFDs) with Synthetic Vision for the pilot and copilot interfaced to all navigation systems including HSI functionality

(2) Dual Attitude Heading and Reference Systems. Capable of operating, without restrictions, in Alaska.

(3) Dual Air Data Systems

(4) One Multi-Function Display (MFD) in the pilot and copilot field of view. This must have the capability to display traffic with a range selection of 2 NM or less.

(5) Two VHF-AM communications radios having a minimum of 760 channels operating from 118.000 to 136.975 MHz

(6) Two VOR/Localizer/Glideslope systems

(7) One Marker Beacon system

(8) One DME system (FAA Approval via 8110 authorized)

(9) One Radar Altimeter (FAA Approval via 8110 authorized)

(10) Two WAAS GPS systems approved for LPV approaches

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

(12) An Active Traffic Advisory System (TAS) approved to TSO C-147 with a minimum range of 10 NM using directional antennas on top and bottom of the aircraft

(13) One Mode-S Transponder with 1090ES ADS-B OUT

(14) One Diversity ADS-B IN system receiving both 1090ES and UAT signals.

Traffic must be coordinated with the TAS system and displayed on the MFD and PFD Synthetic Vision. FIS-B weather must be displayed on the MFD.

(15) Advisory Terrain displayed on the MFD and PFD Synthetic Vision

(16) One TSO-C126 or newer ELT. An ELT transmitting GPS position information is preferred.

(17) One Hour Meter, to record actual flight time, controlled by a weight on wheels or airspeed switch

(18) Audio and Intercom Systems (ICS) for the pilot and copilot. ICS for all passengers is preferred.

(19) A Three Axis Autopilot with Flight Director coupled to the PFD and navigation systems and approved for ILS and LPV approaches. The autopilot must have an altitude alert, capture and hold system.

(20) The aircraft must have sufficient space to install the optional mission equipment listed below

(d) Additional Mission Equipment:

(1) Tactical Audio System with identical controllers for the pilot, copilot and front right passenger (instructor) (FAA Approval via 8110 authorized):

(i) This may be installed as the sole audio system in the aircraft or as supplemental to an OEM audio system. Installation as a sole system is preferred. This may replace a standard OEM system.

(ii) All cockpit and cabin positions must use the tactical audio system

(iii) Audio controllers must have laser etched, or equivalent quality, custom labels. Radio positions must be labeled as Com 1, Com 2, FM 1, FM 2 etc. as appropriate.

(iv) Audio panel annunciations must default to full bright when the dimmers are off

(v) The audio system must be compatible with 600 Ohm earphones and general aviation microphones

(vi) The audio system must be free of distortion, hum, noise and crosstalk

(vii) Warning audio must be provided to the pilot and copilot

(viii) Radio receive audio and ICS must be provided for all positions with Hot Mic and VOX capability

(ix) The pilot must have an ICS isolation capability

(x) Passenger positions must follow the instructor audio selections

(xi) Controls for transmitter selection and independent receiver selection of all required radios shall be provided for each audio controller

(xii) Receive audio must be automatically enabled for the selected transmitter

(xiii) Controls shall be provided for the pilot, copilot and instructor to each independently select and adjust headset volume for each installed communications transceiver

(xiv) Each audio controller must have independent controls for radio and ICS volume adjustment

(xv) The pilot, copilot and instructor must have the capability to simultaneously transmit on any combination of separate radios

(xvi) Each audio controller must have a transmit indication

(xvii) A Push-To-Talk (PTT) switch shall be installed to allow the copilot to transmit without touching the flight controls

(xviii) The instructor position must have unobstructed access to the audio controls and a PTT switch while seated

(xix) Radio key lines must be wired to the pilot, copilot and instructor mic jacks

(xx) JJ033 and JJ034 style headset jacks shall be installed at each position and separated by no more than four inches

(xxi) Powered jacks compatible with the BOSE A20 Aviation Headset shall be installed at the pilot, copilot and instructor positions in addition to the standard jacks

(xxii) Cockpit speakers shall be sufficiently amplified for use in flight

(2) Tactical Communications Systems meeting the requirements below (FAA Approval via 8110 authorized):

(i) Transmitters shall not open squelch on, or interfere with, other AM or FM transceivers on the aircraft which are monitoring different frequencies.

Transmit interlock functions shall not be used with communication transceivers.

(ii) VHF-FM System 1(Offeror’s may comply with System 1 or 2):

(A) Two Technisonic TDFM-136B VHF-FM Radios permanently installed in a location convenient to the pilot and copilot. These must correspond to FM1 and FM 2 positions on the audio controllers

(B) One Auxiliary FM system corresponding to an AUX FM position on the audio controllers and meeting the following requirements:

(1) 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 by an AEM AA34 or equivalent.

(2) 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.

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

(iii) VHF-FM System 2(Offeror’s may comply with System 1 or 2):

(A) One Technisonic TDFM-9000 Radio, project number P90508, permanently installed in a location convenient to the pilot and copilot. The four modules must correspond to FM 1, FM 2, FM 3 and FM 4 positions on the audio controllers. A separate CI-177-1, or equivalent, antenna shall be installed for each module.

(3) General Equipment:

(i) One Latitude S100 Automated Flight Following (AFF) system (FAA Approval via 8110 authorized).

(ii) Auxiliary power installation. The aircraft shall be equipped with both AC and USB power receptacles for use in powering various mission-required equipment, as detailed below (FAA Approval via 8110 authorized):

(A) Mid Continent TA 102, or equivalent, Dual USB Charging Ports. One each shall be installed at the pilot, copilot and all passenger positions. These must be accessible while seated. The location of the connector is to be approved by USFS personnel prior to delivery of the aircraft.

(B) A Mid Continent TI500, or equivalent, AC inverter supplying pure sinewave 115VAC 60Hz power to the copilot, forward left passenger and forward right passenger. The AC output must be circuit breaker protected. The outlets will be compatible with the standard U.S. three prong AC plug and accessible while seated.

The location of the connector is to be approved by USFS personnel prior to delivery of the aircraft.

(e) Aircraft Paint - Contractor shall apply “Forest Service,” the Forest Service Shield and the assigned FAA registration number (N number) per the approved paint scheme. The N number shall be designated and furnished by the Forest Service. The approved paint to form a neat straight line without ridges or tape lines.

B.7 CONTINUED AIRWORTHINESS AND MAINTENANCE

(a) Type Design:

(1) The airplane will be delivered meeting all requirements of the FAA approved Type Design.

(b) Equipment Installation:

(1) The installation of additional equipment and/or modification of the aircraft to meet the specifications of this contract shall be completed in accordance with 14 CFR requirements and manufacturer's recommendations or engineering data and be FAA approved by the TCDS or STC unless otherwise specified above.

Field Approval with 8110 acceptable means – Field Approval for installation with supporting FAA Form 8110-3 and all DER supporting engineering substantiation documentation attached. The government will be given full rights to any alteration/modification data.

(c) Maintenance and Service Instructions:

(1) Each airplane will be delivered with a complete set of required operations, maintenance and service instructions, along with a complete set of service bulletins.

(d) Airworthiness Directives and Service Bulletins:

(1) The delivered aircraft shall comply with all current Airworthiness Directives.

(2) At the start of Government acceptance inspections and at delivery of each aircraft procured under this effort, the Government shall be provided a list or lists identifying the airplane’s compliance with applicable Airworthiness Directives and the airplane’s compliance with all Service Bulletins (SB).

(3) Draft SBs shall be provided to the Government for approval 60 days prior to scheduled acceptance to address those SBs that are applicable to the aircraft but will not be accomplished at the time of delivery.

(e) Master Minimum Equipment List (MMEL):

(1) The aircraft shall have a FAA approved Master Minimum Equipment List (MMEL).

(f) Weight and Balance:

(1) The aircraft shall be weighed in accordance with OEM standard practices.

(2) Records that reflect the modified configuration shall be delivered with the aircraft.