Amendment_0001.pdf

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT

1. CONTRACT ID CODE PAGE OF PAGES

1 5

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

Amendment 01 January 25, 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-17-0005

9B. DATED (SEE ITEM 11)

January 03, 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. Cover Page; Item 3: Add a requirement to provide your response to paragraph E.3 as well as E.7 and E.10.

B. Page 2; B.1(b) CLIN 2.Ab: Change to read Lease of one sensor from “Date of Delivery” through December 31, 2017 (payments for the first month will be prorated based on available days and total days in the month).

C. Page 11; B.3(a)(1)(a) and (c): Add “and sensor mount” to the end of the sentence to clarify the requirement.

D. Page 11; B.3(a)(1)(Note): Add the following sentence to the paragraph as the second sentence:

“The currently installed camera door does not have to remain but if it does the modification from this solicitation has to be compatible with the existing door, has to replace it or take it back to OEM structure.”

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

Continuation Page Amendment 0001 to Solicitation AG-024B-S-17-0005

E. Page 11; B.3(a)(4): Reword section to clarify the FAA approval requirements for the aircraft integration and to annotate that STC’ed solutions will receive a more favorable evaluation as follows:

(4) Aircraft Integration of the sensor, weather sensor, data link with WiFi and other ancillary equipment may be approved by one of the following methods. STC’ed installations will result in a more favorable evaluation.

(a) An aircraft OEM installation

(b) FAA STC

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

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

F. Page 18; B.9: Change the Section to read as follows to be consistent with Section B.3:

B.9 SENSOR/AIRCRAFT INSTALLATION AND INTEGRATION

(a) One sensor system meeting the requirements of this contract installed by one of the following methods:

(1) Avcon STC SA1648CE camera door (currently installed on the aircraft) or other STC’ed camera door and sensor mount.

(2) STC’ed nose mounted retractable sensor mount.

(3) STC’ed belly pod and sensor mount.

Note: The US Forest Service is unsure as to which method(s) would be possible due to not knowing the multiple sensors that could be offered or compatibility with the currently installed camera door. The currently installed camera door does not have to remain but if it does the modification from this solicitation has to be compatible with the existing door, has to replace it or take it back to OEM structure. Offerors are encouraged to propose alternate integration methods.

(b) One weather sensor meeting the requirements of Section B.7 of this contract.

(c) Datalink with WiFi equipment meeting the requirements of Sections B.8 of this contract.

(d) Aircraft Integration of the sensor, weather sensor, data link with WiFi and other ancillary equipment may be approved by one of the following methods. STC’ed installations will result in a more favorable evaluation.

(1) An aircraft OEM installation

(2) FAA 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.

(e) The Imager shall be mounted to the provided airframe in a manner which maximizes imagery capabilities while minimizing performance impacts to the aircraft. The aircraft shall be capable of maneuvering in both right and left-hand orbits without degrading data acquisition quality/or availability.

Persistent Orbit

Off-set Presistent

Orbit Strip Mapping

Area of Interest Path (Perimeter)

Area Orbit Off-set Area

Orbit

Figure 1

(f) The sensor integration method shall not restrict the aircraft from performing in the multi mission role. The installation can be configured for removal and reinstallation by certificated maintenance personnel to allow the aircraft to perform other agency missions. The FAA installation approval must include a provision to allow reconfiguration via a logbook entry as an approved configuration change.

(g) Sensor configuration must comply with one of the following:

(1) A primary imager in a multi-axis stabilized 360-degree gimbal. Imager shall have an unobstructed continuous pan view from 10 degrees below the lowest horizontal plane of the aircraft (in-flight), and throughout downward pointing angle(s) to the earth's surface directly (perpendicular/nadir) below the aircraft at level (0) pitch, roll, and yaw. [Imager shall have free, 360-degree rotation throughout the horizontal plane parallel to the ground in straight and level flight. In the plane perpendicular to this, imager shall have free rotation from the vertical down position upward to within ten degrees of parallel to the horizontal axis, in either planar direction from vertical. This equates to a total of 160 degrees of freedom in this axis.]

(2) A primary imager in a multi-axis stabilized 360-degree gimbal. Imager shall have an unobstructed continuous pan view from 10 degrees below the lowest horizontal plane of the aircraft (in-flight), and throughout downward pointing angle(s) to the earth's surface directly (perpendicular/nadir) below the aircraft at level (0) pitch, roll, and yaw. Additionally, the integration method shall accommodate an additional Forest Service imager. Example systems include USFS Phoenix, USFS Firemapper, LiDAR, TMAP, AMS, and WAI.

(3) A primary imager in a Look-Down-Gimbal (LDG). LDG Imager shall have an unobstructed view throughout the LDG’s range of motion.

X X

X

(4) A primary imager in a Look-Down-Gimbal (LDG) with a secondary FMV imager in retractable or non-retractable multi-axis stabilized 360-degree gimbal. LDG Imager shall have an unobstructed view throughout the LDG’s range of motion. FMV Imager shall have an unobstructed continuous pan view from 10 degrees below the lowest horizontal plane of the aircraft (in-flight), and throughout downward pointing angle(s) to the earth's surface directly (perpendicular/nadir) below the aircraft at level (0) pitch, roll, and yaw.

G. Page 24; B.13(b) and (c): Delete paragraph 13(b) in its entirety and replace with the following and change existing paragraph (c) to paragraph (d):

(b) Detailed documentation for system operation, applicable field maintenance, and troubleshooting shall be provided upon delivery and updated upon any modification performed.

(c) On-the-job sensor system operation training for Agency SO staff (total 5 people) as well as required field maintenance and troubleshooting, shall be provided.

(1) On-the-job training shall be conducted by a provider SME over no more than the first 60 day period after acceptance of the completed system.

a. Training shall consist of approximately 80 hours of ground instruction and 10 in-flight instruction hours per Agency SO. This training is a part of the sensor system price and will not be paid separately under the contract.

b. The trainer shall only function within the scope of a proficient SO providing instruction to Agency employees in order to achieve the same level of SO proficiency.

c. The trainer shall update all system operation documentations, applicable field maintenance manuals, and troubleshooting guides in order to reflect the AFUE mission ConOps and fully reflect the mission training required for all current and future agency SOs.

d. Each trainer shall complete resident Agency Aircrew Resource Management Training and Interagency Aviation Training (IAT, https://www.iat.gov) web-based “Aircrew Member with Hazmat requirement” training prior to providing inflight instruction to Agency SO staff. Certificate of Completion shall be provided to the CO or designated representative.

i. Aircrew Member with Hazmat requirement:

A-100 Basic Aviation Safety (5hr)

A-110 Aviation Transportation of Hazardous Material (2hr)

A-116 General Awareness Security (0.5hr)

A-200 Mishap Review (2hr)

H. Page43; C.11(c): Correct reference to reference paragraph B.14.

I. Page 57; Exhibits: Add Exhibit 8: Electrical Loads Analysis N182Z and Exhibit 9: Aircraft Flight

Manual.

J. Page 65; Exhibit 7(l): Correct figures number in the second sentence to “Figures 7-10…”

K. Page 69; Exhibit 7 top of the page: Delete B.10 reference and leave as “Derived Product Requirements”

L. Page 72; Section E.3(a)(1): Authorize submission of offers and supporting information electronically stored on thumb drives only (CD or DVDs not acceptable.

M. Page 73; E.3(b)(3)(ii): Correct the reference to paragraph B.2.

N. Page 74; E.3(b)(4): Correct to state that Section E.10 must be completed and submitted.

O. Page 76; E.4(b)(2)(i): Correct reference to read Section B.4 Sensor Requirements.

P. Page 76; E.4(b)(2)(ii): Correct reference to read Section B.5 Work Station Requirements.

Q. Page 76; E.4(b)(2)(iii): Correct reference to read Exhibit 7 Software, User Interface, and Product

Requirements.

R. Page 77; E.4(b)(3): Change reference for the training in second sentence to B13(b).

S. Page 78; E.4(b)(4): Add (i) under the evaluation to document that we will be evaluating the installation methods for the sensor system. Change existing paragraph (i) to (ii) and existing (ii) to (iii):

(i) Installation approval methods and compatibility with the aircraft in its multi mission role. Installations that allow the aircraft to maintain more efficient use by a more proven installation method (STC), less time to convert to the passenger configuration and has a lower equipped weight when the mission equipment is removed will result in a more favorable evaluation.

(ii) Total Weight of the Sensor System. The Government will evaluate the total weight of the sensor system based on the maximum installation weight of the total sensor system offered. The lower total estimated weight, the more favorable evaluation your offer will receive.

(iii) Delivery Date of the fully installed Sensor System. The Government will evaluate the maximum delivery time offered for the installation of the complete sensor system into the aircraft. Delivery dates that provide for less time from delivery of the aircraft to the Contractor’s facility to the time the aircraft is redelivered back to the Government with an FAA approved Sensor System will receive a more favorable evaluation.

T. Remove blank pages from the solicitation.

U. Replace existing solicitation with Solicitation AG-024B-S-17-0005 Amendment 0001.Changes noted by bold and italicized text.