15DDHQ18R00000019-2.pdf

SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS 1. REQUISITION NUMBER PAGE 1 OF

OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24, & 30 D-18-0A-0096 52

2. CONTRACT NO. 3. AWARD/EFFECTIVE 4. ORDER NUMBER 5. SOLICITATION NUMBER 6. SOLICITATION ISSUE

DATE , DATE

See Block 31 c. 15DDHQ18R00000019 07/12/2018

a. NAME b. TELEPHONE NUMBER (No collect 8. OFFER DUE DATE/

7. FOR SOLICITATION

calls) LOCAL TIME

INFORMATION CALL: 08/06/2018

Nancy A Costello 202-353-1493 10:00am ET

9. ISSUED BY CODE 10. THIS ACQU ISITION IS lJ UNRESTRICTED OR ~ SET AS IDE: 100 % FOR:

USDOJ/DEA Headquarters (8] SMALL BUSINESS

WOMEN-OWNED SMALL BUSINESS ---

D (WOSB) ELIGIBLE UNDER THE WOMEN-OWNED

Office of Acquisition and Relocation Management D HUBZONE SMALL SMALL BUSINESS PROGRAM NAICS:

8701 Morrissette Drive BUSINESS

0EDWOSB 336411

Springfield , VA 221 52 D SERVICE-DISABLED

VETERAN-OWNED SIZE STANDARD:

SMALL BUSINESS D8 (A) 1,500 employees 11 . DELIVERY FOR FOB DESTINA- 12. DISCOUNT TERMS 13b. RATING

TION UNLESS BLOCK IS D 13a. THIS CONTRACT IS A

MARKED RATED ORDER UNDER

DPAS (15 CFR 700) 14. METHOD OF SOLICITATION

D SEE SCHEDULE 0 RFQ D1FB [8:J RFP

15. DELIVER TO CODE 16. ADMINISTERED BY CODE I

DEA - Aviation Division DEA Headquarters 2300 Horizon Dr. 8701 Morrissette Drive Ft. Worth , TX 76177-5300 Springfield , VA 22152 17a. CONTRACTOR/ CODE I I FACILITY 18a. PAYMENT WILL BE MADE BY CODE I OFFEROR CODE

Prospective Offeror DEA - Aviation Division invoice.aviation@usdoj .gov

I

Ft. Worth , TX 76177-5300

TELEPHONE NO.

D 17b. CHECK IF REMITTANCE IS DIFFERENT AND PUT SUCH ADDRESS IN 18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a UNLESS BLOCK

OFFER BELOW IS CHECKED D SEE ADDENDUM

19. 20. 21. 22. 23. 24 .

ITEM NO. SC HEDULE OF SUPPLI ES/SERVICES QUANTITY UNIT UNIT PRICE AMOUNT

This RFP is for a single Indefinite Delivery/Indefinite Quantity (IDIQ) contract with fi xed price delivery orders for Airborne Imaging System Installation and Integration.

Work shall be performed in accordance with the Statement of Objectives and terms and conditions attached.

Procurement is pursuant to FAR 12 and FAR 15.

See continuation pages attached.

(Use Reverse and/or Attach Additional Sheets as Necessary)

25. ACCOUNTING AND APPROPRIATION DATA 26. TOTAL AWARD AMOUNT (For Govt. Use Only)

[8] 27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1, 52.212-4. FAR 52.212-3 AND 52.212-5 ARE ATTACHED. ADDENDA

D 27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4 . FAR 52.212-5 IS ATTACHED. ADDENDA

[8] ARE DARE NOT ATTACHED

D ARE D ARE NOT ATTACHED

D 28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN --- D 29. AWARD OF CONTRACT: REF. OFFER

COPIES TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND

DATED . YOUR OFFER ON SOLICITATION

DELIVER ALL ITEMS SET FORTH OR OTHERWISE IDENTIFIED ABOVE AND ON ANY (BLOCK 5) , INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE

ADDITIONAL SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED SET FORTH HEREIN, IS ACCEPTED AS TO ITEMS:

30a. SIGNATURE OF OFFEROR/CONTRACTOR 31a. UNITED STATES OF AMER ICA (SIGNATURE OF CONTRACT/NG OFFICER)

30b. NAME AND TITLE OF SIGNER (Type or print)

I

AUTHOR IZED FOR LOCAL REPRODUCTION

PREVIOUS EDITION IS NOT USABLE

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

Ryan F. Burke, Contracting Officer

STANDARD FORM 1449 (REV. 212012)

Prescribed by GSA- FAR (48 CFR) 53 .212

19.

I

20. 21. 22. 23. 24 .

ITEM NO. SCHEDULE OF SUPPLIES/SERVICES QUANTITY UNIT UNIT PRICE AMOUNT

I

I 32a. QUANTITY IN COLUMN 21 HAS BEEN

D RECEIVED D INSPECTED D ACCEPTED, AND CONFORMS l'O THE CONTRACT, EXCEPT AS NOTED: --------------- 32b. SIGNATURE OF AUTHORIZED GOVERNMENT 32c. DATE 32d. PRINTED NAME AND TITLE OF AUTHORIZED GOVERNMENT

REPRESENTATIVE REPRESENTATIVE

32e. MAILING ADDRESS OF AUTHORIZED GOVERNMENT REPRESENTATIVE 32f. TELPHONE NUMBER OF AUTHORZED GOVERNMENT REPRESENTATIVE

I 32g. E-MAIL OF AUTHORIZED GOVERNMENT REPRESENTATIVE

33. SHIP NUMBER 34. VOUCHER NUMBER 35. AMOUNT VERIFIED 36. PAYMENT 37. CHECK NUMBER

CORRECT FOR

0PARTIAL 0FtNAL D COMPLETE 0PARTIAL DFINAL

38. S/R ACCOUNT NO. 39. S/R VOUCHER NUMBER 40. PAID BY

41 a. I CERTI FY THIS ACCOUNT IS CORRECT AND PROPER FOR PAYMENT 42a. RECEIVED BY (Print)

41 b. SIGNATURE AND TITLE OF CERTIFYING OFFICER 41c. DATE

42b. RECEIVED AT (Location)

42c. DATE REC'D (YY/MM/00) 142d. TOTAL CONTAINERS

STANDARD FORM 1449 (REV. 212012) BACK

Section 2

15DDHQ18R00000019

Schedule of Supplies/Services

Base Year:

Contract Line Item Number

(CLIN)

Supplies/Services Est.

Quantity

Unit

Unit Price $

Total Price $

0001 Airborne Imaging System Installation and Integration, Bell 407 helicopter

3 EA

0002 Airborne Imaging System Installation and Integration, Bell 206L3 helicopter

0 EA

0003 Airborne Imaging System Installation and Integration, Airbus AS350 helicopter

1 EA

0004 Airborne Imaging System Installation and Integration, Cessna 208 aircraft

3 EA

0005 Airborne Imaging System Installation and Integration, Cessna 206 aircraft

7 EA

0006 Airborne Imaging System Installation and Integration, Cessna 206 Soloy aircraft

1 EA

0007 Training for DEA maintenance personnel

16 EA

TOTAL

Option Year 1 1001 Airborne Imaging System

Installation and Integration, Bell 407 helicopter

3 EA

1002 Airborne Imaging System Installation and Integration, Bell 206L3 helicopter

0 EA

1003 Airborne Imaging System Installation and Integration, Airbus AS350 helicopter

1 EA

1004 Airborne Imaging System Installation and Integration, Cessna 208 aircraft

3 EA

1005 Airborne Imaging System Installation and Integration, Cessna 206 aircraft

7 EA

1006 Airborne Imaging System Installation and Integration, Cessna 206 Soloy aircraft

1 EA

1007 Training for DEA maintenance personnel

2 EA

TOTAL

Option Year 2:

Contract Line Item Number

(CLIN)

Supplies/Services

Est.

2001 Airborne Imaging System Installation and Integration, Bell 407 helicopter

3 EA

2002 Airborne Imaging System Installation and Integration, Bell 206L3 helicopter

0 EA

2003 Airborne Imaging System Installation and Integration, Airbus AS350 helicopter

2 EA

2004 Airborne Imaging System Installation and Integration, Cessna 208 aircraft

3 EA

2005 Airborne Imaging System Installation and Integration, Cessna 206 aircraft

7 EA

2006 Airborne Imaging System Installation and Integration, Cessna 206 Soloy aircraft

1 EA

2007 Training for DEA maintenance personnel

2 EA

TOTAL

Option Year 3:

3001 Airborne Imaging System

Installation and Integration, Bell 407 helicopter

3 EA

3002 Airborne Imaging System Installation and Integration, Bell 206L3 helicopter

1 EA

3003 Airborne Imaging System Installation and Integration, Airbus AS350 helicopter

2 EA

3004 Airborne Imaging System Installation and Integration, Cessna 208 aircraft

3 EA

3005 Airborne Imaging System Installation and Integration, Cessna 206 aircraft

7 EA

3006 Airborne Imaging System Installation and Integration, Cessna 206 Soloy aircraft

1 EA

3007 Training for DEA maintenance personnel

2 EA

TOTAL

Option Year 4:

Contract Line Item Number

(CLIN)

Supplies/Services

Est.

4001 Airborne Imaging System Installation and Integration, Bell 407 helicopter

3 EA

4002 Airborne Imaging System Installation and Integration, Bell 206L3 helicopter

0 EA

4003 Airborne Imaging System Installation and Integration, Airbus AS350 helicopter

1 EA

4004 Airborne Imaging System Installation and Integration, Cessna 208 aircraft

3 EA

4005 Airborne Imaging System Installation and Integration, Cessna 206 aircraft

7 EA

4006 Airborne Imaging System Installation and Integration, Cessna 206 Soloy aircraft

1 EA

4007 Training for DEA maintenance personnel

2 EA

TOTAL

Grand Total (base and options) $______________

2.1 Maximum Value and Minimum Guarantee

The maximum value for this IDIQ contract (inclusive of the aggregate price of all delivery orders issued) shall not exceed [amount to be added upon award]. The guaranteed minimum under this contract shall be equal to the value of the first delivery order issued.

2.2 Estimated Quantities

All quantities specified in Section 2 are estimated quantities only. The Government reserves the right to order more than or less than the quantities provided, but will not order less than the minimum guarantee or more than the maximum dollar value specified in clause 2.1.

Section 3

STATEMENT OF OBJECTIVES

DRUG ENFORCEMENT ADMINISTRATION

AVIATION DIVISION

AIRBORNE IMAGING SYSTEMS

1.0 OVERVIEW

The U.S. Department of Justice, Drug Enforcement Administration (DEA) Aviation Division has a requirement for Airborne Imaging Systems to be installed on Government-owned aircraft.

2.0 SCOPE

This Statement of Objectives (SOO) establishes the requirements to install Airborne Imaging Systems on the following types of Government-owned aircraft in support of DEA law enforcement missions.

A. Bell 206LIII B. Bell 407 Helicopter C. Airbus AS350B2 Helicopter D. Cessna 208 Aircraft E. Cessna 206 Aircraft F. Cessna 206 Soloy Aircraft

The aircraft for this requirement are operated and maintained in accordance with Federal Aviation Administration (FAA) Part 91 and the aircraft manufacturer’s recommendations. The Contractor shall be responsible for certification of the complete Airborne Imaging Systems in accordance with any applicable FAA regulations and maintain the aircraft’s Standard Airworthy Certificate. Airborne Imaging Systems with approved Supplemental Type Certificates are preferred but not mandatory.

3.0 PERFORMANCE REQUIREMENTS

The Contractor shall procure any necessary equipment, hardware and components and install and integrate the Airborne Imaging Systems for the referenced Government-owned aircraft. Some aircraft will require the removal of existing older imaging systems to include all components, wiring and hardware; no components, wiring or hardware from these existing older imaging systems shall be utilized for this requirement.

3.1 HELICOPTERS

3.1.1. BELL 206LIII

The Airborne Imaging Systems for each Bell 206LIII shall possess the following features:

A. One Wescam MX-10 or MX-15HDi Gyro-stabilized EO/IR imager will be provided as Government Furnished Equipment (GFE). See Exhibit 1 for imagers’ specifications.

B. The Imager for the Bell 206LIII shall be mounted on the aircraft’s nose, the mount shall be provided as Contractor Acquired Property (CAP). The imager shall be attached to a camera mount utilizing a quick release dovetail mount and shall be

(CAP).

C. One Churchill Navigation Ion High Definition Digital Video Recorder (DVR) (CAP).

D. Two 14 to 15 inch High Definition Video Monitors (CAP) shall have the following minimum features:

1. Two HD-SDI video inputs.

2. Touch screen capability.

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1280 x 800 WXGA.

5. 16:9 ratio wide screen monitor.

6. NVIS class B compatible.

E. One Churchill Navigation, ARS-700 mission management system (GFE).

F. One stowable keyboard with touch pad (CAP).

G. One five to seven inch flip-up stowable monitor for pilot reference (CAP).

H. One Operator Console (CAP) that shall consist of the two video monitors, digital video recorder, ARS-700 mission management system, stowable keyboard and if installed, one Technisonic multiband radio remote control head (RC-6000, RC-7000 or RC-9000) in a compact package giving the operator unobstructed legroom. The Technisonic multiband radio remote control head will be provided as GFE; all other components shall be CAP. The Operator Console shall be located in the rear cabin area in place of the left rear facing passenger seat within convenient reach of the operator and shall be easily removable to allow for aircraft maintenance. The video monitors shall be mounted in a side-by-side configuration attached to individual swing arms to allow adjustment and ease of viewing by the operator. The Operator Console shall be configured as to allow unimpeded egress from the aircraft.

The rear audio panel in these aircraft will remain in their present location; they will not be relocated to the Operator Console.

I. On aircraft equipped with Garmin Avionics Systems, the Contractor shall route a separate video in control signal to the G500H or G1000H Multi- Function Display.

This separate video signal is for pilot reference and shall be utilized in lieu of the flip-up stowable monitor.

For aircraft that are not equipped with Garmin Avionics Systems, the Contractor shall install and integrate the five to seven inch flip-up stowable monitor (CAP), mounted on the aircraft’s instrument panel glare shield for pilot reference. The pilot’s monitor shall have a swivel base to allow adjustment for ease of viewing for the pilot.

J. The Contractor shall integrate all Airborne Imaging System components, imaging sensors and ARS-700 mission management system into a user friendly interface utilizing the touch screen capability of the monitors. The video monitors shall be separated into a primary and secondary arrangement. Both monitors shall be configured for quad screen operation and shall be capable of displaying video from all sensors and ARS mission management system data. Video selected from the primary monitor shall be directed, upon command to the DVR or ARS-700 or both for recording. The pilot’s video display shall be integrated to display video from any sensor selected by the operator.

Aircraft intercom audio and ARS-700 map overlay shall not be recorded on the DVR or ARS-700. ARS map overlay is for operator reference only.

K. The helicopters referenced in this SOO are equipped with Night Vision Imaging

System (NVIS) lighting. The Airborne Imaging System shall be NVIS compatible and certified under the NVIS’s manufacturer Supplemental Type Certificate.

3.1.2. Bell 407

The Airborne Imaging Systems for each Bell 407 shall possess the following features:

A. One Wescam MX-10 or MX-15HDi Gyro-stabilized EO/IR imager will be provided as Government Furnished Equipment (GFE). See Exhibit 1 for imagers’ specifications.

B. The Imager for the Bell 407 shall be mounted on the aircraft’s nose, the mount shall be provided as Contractor Acquired Property (CAP). The imager shall be attached to a camera mount utilizing a quick release dovetail mount and shall be CAP.

C. One Churchill Navigation Ion High Definition Digital Video Recorder (DVR) (CAP).

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1280 x 800 WXGA.

E. One Churchill Navigation, ARS-700 mission management system (GFE).

installed, one Technisonic multiband radio remote control head (RC-6000, RC-7000 or RC-9000) in a compact package giving the operator unobstructed legroom. The Technisonic multiband radio remote control head will be provided as GFE; all other components shall be CAP. The Operator Console shall be located in the rear cabin area in place of the left rear facing passenger seat within convenient reach of the operator and shall be easily removable to allow for aircraft maintenance. The video monitors shall be mounted in a side-by-side configuration attached to individual swing arms to allow adjustment and ease of viewing by the operator. The Operator Console shall be configured as to allow unimpeded egress from the aircraft.

separate video in control signal to the G500H or G1000H Multi- Function Display.

This separate video signal is for pilot reference and shall be utilized in lieu of the flip-up stowable monitor.

For aircraft that are not equipped with Garmin Avionics Systems, the Contractor shall install and integrate the five to seven inch flip-up stowable monitor (CAP), mounted utilizing the touch screen capability of the monitors. The video monitors shall be separated into a primary and secondary arrangement. Both monitors shall be configured for quad screen operation and shall be capable of displaying video from all sensors and ARS mission management system data. Video selected from the primary monitor shall be directed, upon command to the DVR or ARS-700 or both for recording. The pilot’s video display shall be integrated to display video from any sensor selected by the operator.

K. The helicopters referenced in this SOO are equipped with Night Vision Imaging

System (NVIS) lighting. The Airborne Imaging System shall be NVIS compatible and certified under the NVIS’s manufacturer Supplemental Type Certificate.

3.1.2. AIRBUS AS350B2

The Airborne Imaging Systems for each Eurocopter AS350 shall possess the following features:

A. One Wescam MX-10 or MX-15HDi Gyro-stabilized EO/IR imager (GFE). See Exhibit 1 for imagers’ specifications.

B. The Imager for the Eurocopter AS350 shall be mounted to the aircraft’s belly just aft of the left hand chin bubble, the mount shall be (CAP). The imager shall be attached to a camera mount utilizing a quick release dovetail mount (CAP).

C. One Churchill Navigation Ion High Definition Digital Video Recorder (CAP).

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1280 x 800 WXGA.

E. One Churchill Navigation ARS-700 mission management system (GFE).

G. One Operator Console (CAP) that shall consist of the two video monitors, digital installed, one Technisonic multiband radio remote control head (RC-6000, RC-7000 or RC-9000) in a compact package giving the operator unobstructed legroom. The Technisonic multiband radio remote control head will be provided as GFE; all other components shall be CAP. The Operator Console shall be located in the rear cabin area within convenient reach of the operator and shall be easily removable in order to allow for aircraft maintenance. The video monitors shall be mounted in a side-by-side configuration attached to individual swing arms to allow adjustment and ease of viewing and operation by the operator. The Operator Console shall be configured as to allow unimpeded egress from the aircraft.

H. The Contractor shall route a separate video in control signal to the Garmin Avionics

System G500H Multi-Function Display. This separate video signal is for pilot reference.

I. The Contractor shall integrate all Airborne Imaging System components, imaging utilizing the touch screen capability of the monitors. The video monitors shall be separated into a primary and secondary arrangement. Both monitors shall be configured for quad screen operation and shall be capable of displaying video from all sensors and ARS mission management data. Video selected from the primary monitor shall be directed, upon command to the DVR or ARS-700 or both for recording. The pilot’s video display shall be integrated to display video from any sensor selected by the operator.

J. The helicopters referenced in this SOO are equipped with Night Vision Imaging

System lighting. The Airborne Imaging System shall be NVIS compatible and certified under the NVIS’s manufacturer Supplemental Type Certificate.

3.2 CESSNA 208/208B

The Airborne Imaging Systems for each Cessna 208 aircraft shall possess the following:

A. One Wescam MX-15HDi Gyro-stabilized EO/IR imager (GFE). See Exhibit 1 for imager specifications.

B. The MX-15HDi shall be mounted on the left side of the aircraft via a fuselage camera mount that allows the most unobstructed camera view, the mount shall be (CAP). The MX-15HDi shall be attached to the camera mount utilizing a quick release dovetail mount (CAP).

C. One Churchill Navigation Ion High Definition Digital Video Recorder (CAP).

D. Two 17 inch High Definition Video Monitors (CAP) shall have the following

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1280 x 800 WXGA.

video recorder, ARS-700 mission management system, stowable keyboard, rear audio panel and if installed, one Technisonic multiband radio remote control head (RC- 6000, RC-7000 or RC-9000) in a compact package giving the operator unobstructed legroom. The rear audio panel and Technisonic multiband radio remote control head will be provided as GFE; all other components shall be CAP. The Operator Console shall be located in the rear cabin area within convenient reach of the operator and shall be easily removable in order to allow for aircraft maintenance. The video monitors shall be mounted vertically, one on top of the other attached to individual swing arms to allow adjustment and ease of viewing and operation by the operator.

The Operator Console shall be configured as to allow unimpeded egress from the aircraft.

separate video in control signal to the G600 or G1000 Multi-Function Display. This separate video signal is for pilot reference and shall be utilized in lieu of the flip-up stowable monitor.

For aircraft that are not equipped with Garmin Avionics Systems, the Contractor shall install and integrate the five to seven inch flip-up stowable monitor mounted on the aircraft’s instrument panel glare shield for pilot reference. The pilot’s monitor shall have a swivel base to allow adjustment for ease of viewing for the pilot.

utilizing the touch screen capability of the monitors. The video monitors shall be separated into a primary and secondary arrangement. Both monitors shall be configured for quad screen operation and shall be capable of displaying video from all sensors and ARS mission management data. Video selected from the primary monitor shall be directed, upon command to the DVR or ARS-700 or both for recording. The pilot’s video display (for pilot reference) shall be integrated to display video from any sensor selected by the operator.

3.3 CESSNA U206G/TU206F/TU206G/206H/T206H

The Airborne Imaging Systems for each Cessna 206 aircraft shall possess the following:

A. One L3 Wescam MX-10 Gyro-stabilized EO/IR imager (GFE).

B. The MX-10 shall be mounted on the left side of the aircraft just behind the rear most window via a fuselage camera mount (CAP). The MX-10 shall be attached to the camera mount utilizing a quick release dovetail mount (CAP).

C. One Churchill Navigation Ion High Definition (HD) Digital Video Recorder (CAP).

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1280 x 800 WXGA.

video recorder, ARS-700 mission management system, stowable keyboard, rear audio panel and if installed, one Technisonic multiband radio remote control head (RC- 6000, RC-7000 or RC-9000) in a compact package giving the operator unobstructed legroom. The rear audio panel and Technisonic multiband radio remote control head will be provided as GFE; all other components shall be CAP. The Operator Console shall be located in the rear cabin area within convenient reach of the operator and shall be easily removable in order to allow for aircraft maintenance. The video monitors shall be mounted in a side-by-side configuration attached to individual swing arms to allow adjustment and ease of viewing and operation by the operator.

separate video in control signal to the G500 or G1000 Multi-Function Display. This separate video signal is for pilot reference and shall be utilized in lieu of the flip-up stowable monitor.

For aircraft that are not equipped with Garmin Avionics Systems, the Contractor shall install and integrate the five to seven inch flip-up stowable monitor (CAP) mounted utilizing the touch screen capability of the monitors. The video monitors shall be separated into a primary and secondary arrangement. Both monitors shall be configured for quad screen operation and shall be capable of displaying video from all sensors and ARS mission management data. Video selected from the primary monitor shall be directed, upon command to the DVR or ARS-700 or both for recording. The pilot’s video display shall be integrated to display video from any sensor selected by the operator.

3.4 CESSNA U206G SOLOY

The Airborne Imaging Systems for each Cessna U206G Soloy aircraft shall possess the following:

A. One L3 Wescam MX-10 Gyro-stabilized EO/IR imager (GFE).

B. The MX-10 shall be mounted on the bottom of the left wing, the mount shall be (CAP). The MX-10 shall be attached to the camera mount utilizing a quick release dovetail mount (CAP).

C. One Churchill Navigation Ion High Definition (HD) Digital Video Recorder (CAP).

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1280 x 800 WXGA.

H. One Operator Console (CAP) that shall consist of the two video monitors, digital video recorder, ARS-700 mission management system, stowable keyboard, rear audio panel and if installed, one Technisonic multiband radio remote control head (RC- 6000, RC-7000 or RC-9000) in a compact package giving the operator unobstructed legroom. The rear audio panel and Technisonic multiband radio remote control head will be provided as GFE; all other components shall be CAP. The Operator Console shall be located in the rear cabin area within convenient reach of the operator and shall be easily removable in order to allow for aircraft maintenance. The video monitors shall be mounted in a side-by-side configuration attached to individual swing arms to allow adjustment and ease of viewing and operation by the operator.

separate video in control signal to the G500 Multi-Function Display. This separate video signal is for pilot reference and shall be utilized in lieu of the flip-up stowable monitor.

For aircraft that are not equipped with Garmin Avionics Systems, the Contractor shall install and integrate the five to seven inch flip-up stowable monitor (CAP) mounted utilizing the touch screen capability of the monitors. The video monitors shall be separated into a primary and secondary arrangement. Both monitors shall be configured for quad screen operation and shall be capable of displaying video from all sensors and ARS mission management data. Video selected from the primary monitor shall be directed, upon command to the DVR or ARS-700 or both for recording. The pilot’s video display shall be integrated to display video from any sensor selected by the operator.

4.0 PERIOD OF PERFORMANCE AND PLACE OF PERFORMANCE

The objective of this procurement is to install an indefinite quantity of Airborne Imaging Systems on an indefinite quantity of DEA aircraft. The Period of Performance will be from contract award for one base year and four option years. The place of performance shall be the Contractor’s secure facility. The Contractor shall be required to complete an Airborne Imaging System installation within ten weeks after aircraft delivery to the Contractor’s facility.

Due to mission requirements, the Government anticipates no more than 2 aircraft at a time undergoing an Airborne Imaging System installation. If it is in the best interests of the Government to provide more than 2 aircraft for installation and the Contractor can accept the additional aircraft and deliver them within the stated timeframe, an agreement will be made in writing.

5.0 EQUIPMENT

5.1 GOVERNMENT FURNISHED EQUIPMENT (GFE)

The Government Furnished Equipment shall consist of the following:

(Aircraft quantities are estimates only and are not guaranteed.)

A. Bell 206LIII helicopter, (one each).

B. Bell 407 helicopters, (five each).

C. Airbus AS350B2 helicopters, (six each).

D. Cessna 208/208B aircraft, (two each).

E. Cessna U206G aircraft, (eight each).

F. Cessna TU206F aircraft, (two each).

G. Cessna TU206G aircraft, (one each).

H. Cessna 206H aircraft, (eleven each).

I. Cessna T206H aircraft, (nine each).

J. Cessna U206G Soloy aircraft, (five each).

K. L3 Wescam MX-10 Imagers, see Exhibit 1 for imager specifications.

L. L3 Wescam MX-15HDi Imagers, see Exhibit 1 for imager specifications.

1. Hand Controller.

2. Laser Arming Panel.

3. GPS Antenna.

4. Cable External, GPS Extension.

5. Hand Controller Mounting Bracket.

6. Shipping Case.

M. Churchill Navigation ARS-700 mission management system.

N. Existing aircraft rear audio panel.

O. Technisonic multiband radio remote control head (RC-6000, RC-7000 or RC-

9000).

5.2 CONTRACTOR-ACQUIRED PROPERTY

The Contractor shall procure all necessary equipment, hardware and components to meet the objectives and technical requirements of this SOO. Procured equipment shall be turned over and become property of the Government upon aircraft acceptance. All equipment procured for this SOO shall be the most current and up-to-date model/revision available at the time of acceptance.

6.0 APPLICABLE STANDARDS AND REGULATIONS

Any applicable U. S. Federal Aviation Administration Aviation Regulations and Mil-Spec standards.

7.0 REQUIREMENTS AND DELIVERABLES

A. The requirements are to procure and install Airborne Imaging Systems in Government-owned (DEA) aircraft as specified in this SOO. The period of performance is specified in paragraph 4.0.

B. Deliverable items required by the Contractor shall be a Preliminary Design Review within 30 days from award of contract and a Critical Design Review within 60 days of award. In addition, the Contractor shall provide to the Government a monthly status report demonstrating progress against the schedule established in this SOO.

C. The Contractor shall ensure that modifications performed under this SOO do not in any way adversely affect the performance characteristics of the aircraft electrical, communications, navigation system or Government installed equipment.

D. The Contractor shall ensure that all new wiring associated with this requirement be laser marked with an appropriate identification and provide service loops for each component. Additionally, any exposed wiring, cables or wire bundles for equipment installed in the aircraft cabin shall be secured from damage by the use of coverings, guards or protective shields. Consideration shall be given so that no items shall be installed in any areas that deny or make it difficult to access panels and enclosures that require opening for periodic inspection and maintenance.

E. All associated system wiring, hardware and electrical/video connectors shall comply with applicable Technical Standard Order, Design Order and/or Mil-Spec standards.

The Contractor shall not use consumer grade wiring, hardware or electrical/video connectors for this requirement.

F. Any modifications and equipment installations as well as changes to the external configuration as they affect drag, stability and control to the aircraft performed in accordance with this SOO shall be FAA approved and shall maintain the current aircraft’s Standard Airworthiness Certificate.

G. The Contractor shall perform an electrical load analysis on each aircraft being modified under this SOO before and after system installation in accordance with applicable aircraft manufacture’s specifications and FAA regulations to insure the aircraft’s electrical system can support the Airborne Imaging System.

H. The Contractor shall ensure the aircraft, in its final configuration with the complete Airborne Imaging System installed does not adversely affect the center of gravity of the airplane. The airplane shall be physically weighed upon completion of the Airborne Imaging System installation in all possible configurations (i.e. camera installed, camera removed, console installed, console removed, etc.) and a new aircraft Weight and Balance Report provided for each configuration.

I. The Contractor shall develop an Airborne Imaging System acceptance checklist to be utilized in the acceptance of the installed system. The acceptance checklist shall be tailored to each type of aircraft and contain sufficient detail to verify the functionality of the installed Airborne Imaging System. The Contractor shall submit the acceptance checklist to the Government for approval prior the utilizing the checklist.

J. The Contractor shall return the aircraft with no noticeable deviations from the original interior and exterior paint and finish.

8.0 INSPECTION AND ACCEPTANCE

A. A fully configured Airborne Imaging System shall be 100% operational prior to the Government’s acceptance of each aircraft. No partial deliveries will be accepted. The

Government will indicate acceptance in writing. No payments will be made until the Government’s written acceptance has occurred.

B. The Contractor shall be responsible for certification of the complete Airborne Imaging System in accordance with any applicable FAA regulations and maintain each aircraft’s Standard Airworthy Certificate.

C. The Contractor shall be responsible for obtaining any required commercial or FAA certifications and/or approvals for new or modified parts, subsystems, components, equipment, modifications and installations in accordance with any applicable FAA regulations.

D. The Government will supply a flight crew to operate the aircraft for the purpose of test flights and any flights such as moving the aircraft to and from a location. The Contractor may perform ground runs of fixed wing aircraft as necessary by appropriately trained individuals. The Contractor is not authorized to perform ground runs of rotor wing aircraft. No flight of any Government aircraft by the Contractor is authorized.

E. Any changes to the aircrafts’ FAA approved Pilots Operating Handbook or Flight

Manual resulting from any modifications and installations performed under this SOO shall be developed, FAA Approved (as required) and furnished by the Contractor and incorporated as required by applicable FAA regulations.

9.0 PROGRAM RESPONSIBILITY

The Contractor shall have total program responsibility for ensuring that the requirements defined in this SOO are accomplished. The Contractor shall provide program, technical, manufacturing, engineering and liaison management. The Contractor shall identify a single focal point of contact to interface with the Contracting Officer and Contracting Officer’s Representative (COR). The Contractor shall track program cost, schedule and overall performance to bring this requirement to a successful completion. The Contractor shall immediately notify the COR of any technical issues or program schedule delays.

10.0 QUALITY CONTROL PLAN

A. The Contractor shall develop a Quality Control Plan (QC Plan) for the term of this contract that establishes and maintains well documented quality control procedures that ensure the acceptable performance in accordance with this Statement of Objectives. The Plan shall assure adequate quality control throughout all areas of contract performance and shall be implemented to assure reliability and effective performance. The Government reserves the right to review the quality controls established and to evaluate its effective use in the performance of the requirements under this contract. The Contractor shall be solely responsible for controlling and assuring quality work and providing objective evidence that such control does, in fact exist. The Contractor shall also be liable for Contractor employee negligence and any fraud, waste or abuse. It shall be the responsibility of the Contractor to enforce all QC Plan requirements for any and all subcontractors.

B. The QC Plan shall be submitted as part of the offeror’s proposal and evaluated by the

Government. Upon acceptance by the Government at contract award, the QC Plan shall be incorporated into this contract. The QC Plan shall be updated annually or as requested by the Government.

C. The operation of the QC Plan shall be maintained current and made available to the

COR. Any revisions to the QC Plan shall be approved in writing by the Contracting Officer prior to implementation.

11.0 TECHNICAL SUPPORT AND DESIGN COORDINATION

The Contractor shall serve as the overall technical lead for this requirement and shall provide technical oversight of any subcontractors to ensure compliance with this SOO. The Contractor shall coordinate the engineering design of all systems, modifications, installations, test plans, FAA approvals and certifications for the Government based upon this SOO.

The Contractor shall ensure the Government has the opportunity to participate in the design and procurement decisions as required by this SOO.

12.0 EXISTING ENGINEERING, COMMERCIAL OFF THE SHELF

The Contractor shall use existing engineering and technical data to the maximum extent possible.

The Airborne Imaging Systems should incorporate “Commercial-Off-The Shelf” equipment to the greatest extent possible.

13.0 TECHNICAL PUBLICATIONS

The Contractor shall provide copies of all data required to maintain and operate the Airborne Imaging System including, but not limited to:

A. FAA approved pilot operating handbook or flight manual supplements.

B. Current aircraft weight and balance reports.

C. Airborne Imaging System check lists, to include pilot and airborne imaging system operator.

D. Airborne Imaging System detailed illustrated parts catalog.

E. Airborne Imaging System detailed operators manual.

F. Airborne Imaging System detailed maintenance manual.

G. Airborne Imaging System detailed structural drawings, wiring and electrical schematics.

H. Airborne Imaging System detailed instructions for continued airworthiness.

I. Airborne Imaging System detailed operator training manuals.

The Contactor shall provide one copy of each manual in paper form and one (1) copy in electronic form per Airborne Imaging System installed.

14.0 TRAINING

The Contractor shall conduct Airborne Imaging System operator training. This training shall commence within 30 days of the aircraft acceptance. This training shall include classroom and a minimum of two flight hours per operator. The training shall include up to five students per aircraft system installed. The training typically shall be performed at the aircraft’s home station.

However, if mutually agreed to by both the Government and the Contractor in writing, the training location may be conducted at a location other than the aircraft’s home station.

The Contractor shall conduct training for DEA maintenance personnel. The training shall include, but not limited to system operation, system layout, component identification and location, system integration and system troubleshooting. The training typically shall be performed at the aircraft’s home station. However, if mutually agreed to by both the Government and the Contractor in writing, the training location may be conducted at a location other than the aircraft’s home station.

15.0 WARRANTY AND SUPPORT

In addition to any Original Equipment Manufacturers’ warranties, the Contractor shall warrant that all work furnished pursuant to this SOO strictly conforms to applicable specifications, drawings, descriptions and other requirements of this SOO, and is free from defects in design, material and workmanship. All component warrantees shall be transferable to the Government.

The warranty for the Airborne Imaging Integration System shall extend for a minimum period of one (1) year after final acceptance of each aircraft by the Government unless a different period is mutually agreed to by both the Government and the Contractor in writing. The warranty shall include parts, labor and if necessary, travel cost for a technician to provide warranty support at the aircraft’s location.

The Contractor shall provide a point-of contact for technical and operator support during the contract period.

Section 3 – Exhibit 1

WESCAM MX-10 & MX-15HDi

SPECIFICATIONS

DRUG ENFORCEMENT ADMINISTRATION

AVIATION DIVISION

AIRBORNE IMAGING SYSTEMS

Wescam MX-10 Specifications

• MX-10 Base Camera, Gen 3 or Gen 4.

• EON-MX10: Spotter Scope.

• LLC-MX10: Low Light Imager.

• LIRF-MX10-ND: Laser Illuminator and Range Finder.

• AVT-MX-10: Auto Video Tracking.

• MX-GEO-GPS-10: Geo Locating.

• MX-RCS-IF-10: Remote Control Subsystem Interface Option.

• MX-METADATA-10: Metadata RS-422 Port Option.

• MX-METADATA-KLV-10: Metadata Key Length Variable Option.

• LAP-MX: Laser Arming Panel.

• MX-HCU: Hand Controller.

Additional Items

• ANT-35C1GA-TW-SS-N: GPS Antenna.

• 42325-01: Hand Controller Mounting Bracket.

• 43981-105: Cable External, GPS Extension.

• TM01264: MX-10 Multi Sensor System Operations and Maintenance Manual.

• 45145-02: Shipping Case.

Wescam MX-15HDi Specifications

• MX-15HDi: Base Camera, Gen 5.

• HDIR-MX15: High Definition Infrared Thermal Imager.

• EON-THD-DCNS-STEP: Day/Night Spotter.

• LRF-MX15: Laser Range Finder.

• LI-MX15: Laser Illuminator, Narrow Beam Divergence.

• AT-MX-02-INT: Auto Video Tracking.

• MX-GEO-GPS-INT: Geo Locating.

• MX-RCS-IF: Remote Control Subsystem Interface Option.

• MX-METADATA-STRM: Metadata RS-422 Port Option.

Section 3 – Exhibit 1

• MX-METADATA-KLV: Metadata Key Length Variable Option.

• LAP-MX: Laser Arming Panel.

• MX-HCU: Hand Controller.

Additional Items

• ANT-35C1GA-TW-SS-N: GPS Antenna.

• 42328-05: Hand Controller Mounting Bracket.

• 43981-105: Cable External, GPS Extension.

• TM00743: MX-15HDi Multi Sensor System Operations and Maintenance Manual.

• 41179-02: Shipping Case.

Section 4 - DEA PROVISION & CLAUSE MATRIX – COMMERCIAL ITEMS Updated through FAC 2005-97 (1/24/2018)

Solicitation #: 15DDHQ18R00000019

52.252-1 SOLICITATION PROVISIONS INCORPORATED BY REFERENCE (FEB 1998)

This solicitation incorporates one or more solicitation provisions by reference, with the same force and effect as if they were given in full text. Upon request, the Contracting Officer will make their full text available. The offeror is cautioned that the listed provisions may include blocks that must be completed by the offeror and submitted with its quotation or offer. In lieu of submitting the full text of those provisions, the offeror may identify the provision by paragraph identifier and provide the appropriate information with its quotation or offer. Also, the full text of a solicitation provision may be accessed electronically at this address:

https://www.acquisition.gov/sites/default/files/current/far/html/FARTOCP52.html#wp372482.

(End of provision)

CONTRACTING OFFICER: Check the corresponding box for the provisions and clauses applicable to this procurement.

52.204-6 UNIQUE ENTITY IDENTIFIER (OCT 2016)

52.204-7 SYSTEM FOR AWARD MANAGEMENT (OCT 2016)

52.204-7 ALT I SYSTEM FOR AWARD MANAGEMENT (OCT 2016) WITH ALTERNATE I (JUL 2013)

52.204-16 COMMERCIAL AND GOVERNMENT ENTITY CODE REPORTING (JUL 2016)

52.209-7 INFORMATION REGARDING RESPONSIBILITY MATTERS (JUL 2013)

52.209-12 CERTIFICATION REGARDING TAX MATTERS (FEB 2016)

52.211-6 BRAND NAME OR EQUAL (AUG 1999)

52.212-1 INSTRUCTIONS TO OFFERORS—COMMERCIAL ITEMS (JAN 2017)

52.212-2 EVALUATION—COMMERCIAL ITEMS (OCT 2014)

(a) The Government will award a contract resulting from this solicitation to the responsible offeror whose offer conforming to the solicitation will be most advantageous to the Government, price and other factors considered. The following factors shall be used to evaluate offers:

Technical Capabilities Past Performance Corporate Capabilities

[Contracting Officer shall insert the significant evaluation factors, such as (i) technical capability of the item offered to meet the Government requirement; (ii) price; (iii) past performance (see FAR 12.301(c)]

Technical factors and past performance, when combined, are significantly more important than cost/price.

(b) Options. The Government will evaluate offers for award purposes by adding the total price for all options to the total price for the basic requirement. The Government may determine that an offer is unacceptable if the option prices are significantly unbalanced. Evaluation of options shall not obligate the Government to exercise the option(s).

(c) A written notice of award or acceptance of an offer, mailed or otherwise furnished to the successful offeror within the time for acceptance specified in the offer, shall result in a binding contract without further action by either party. Before the offer’s specified expiration time, the Government may accept an offer (or part of an offer), whether or not there are negotiations after its receipt, unless a written notice of withdrawal is received before award.

52.212-3 OFFEROR REPRESENTATIONS AND CERTIFICATIONS—COMMERCIAL ITEMS (NOV 2017)

Note: Effective 2/26/2016, this provision was revised to incorporate a new paragraph (q) entitled “Representation by Corporation Regarding Delinquent Tax Liability or a Felony Conviction under any Federal Law.” Any offeror whose annual representations and certifications posted in the System for Award Management does not include the FEB 2016 or later version of provision 52.212-3 must either

(a) Update its annual representations and certifications with the FEB 2016 or later version of provision 52.212-3, or

(b) Complete paragraph (b)(2) and provide this representation with its offer.

Attention is drawn to paragraph (b) of provision 52.212-3, which requests offeror-provided fill-in information in (b)(2), when applicable:

(b)(1) Annual Representations and Certifications. Any changes provided by the offeror in paragraph (b)(2) of this provision do not automatically change the representations and certifications posted on the SAM website.

https://www.acquisition.gov/sites/default/files/current/far/html/FARTOCP52.html#wp372482 https://www.acquisition.gov/sites/default/files/current/far/html/52_200_206.html#wp1137830 https://www.acquisition.gov/far/current/html/52_200_206.html#wp1137850 https://www.acquisition.gov/far/current/html/52_200_206.html#wp1137850 https://acquisition.gov/far/current/html/52_200_206.html#wp1152012 http://acquisition.gov/far/current/html/52_207_211.html#wp1144964 https://www.acquisition.gov/sites/default/files/current/far/html/52_207_211.html#wp1148667 https://www.acquisition.gov/far/current/html/52_207_211.html#wp1143854 https://www.acquisition.gov/far/current/html/52_212_213.html#wp1179124 https://www.acquisition.gov/far/current/html/52_212_213.html#wp1179178 https://www.acquisition.gov/sites/default/files/current/far/html/Subpart%2012_3.html#wp1084408 https://www.acquisition.gov/sites/default/files/current/far/html/52_212_213.html#wp1179194

Solicitation #: 15DDHQ18R00000019

(2) The offeror has completed the annual representations and certifications electronically via the SAM website accessed through http://www.acquisition.gov. After reviewing the SAM database information, the offeror verifies by submission of this offer that the representations and certifications currently posted electronically at FAR 52.212-3, Offeror Representations and Certifications—Commercial Items, have been entered or updated in the last 12 months, are current, accurate, complete, and applicable to this solicitation (including the business size standard applicable to the NAICS code referenced for this solicitation), as of the date of this offer and are incorporated in this offer by reference (see FAR 4.1201), except for paragraphs ______________.

[Offeror to identify the applicable paragraphs at (c) through (u) of this provision that the offeror has completed for the purposes of this solicitation only, if any.

These amended representation(s) and/or certification(s) are also incorporated in this offer and are current, accurate, and complete as of the date of this offer.

Any changes provided by the offeror are applicable to this solicitation only, and do not result in an update to the representations and certifications posted electronically on SAM.]

***Paragraph (i) contracting officer fill-in information***

Note: Paragraph (i)(1): The end products being acquired under this solicitation that are included in the List of Products Requiring Contractor Certification as to Forced or Indentured Child Labor are listed by Schedule of Supplies/Services Item Number as follows:

[when applicable, enter item numbers with country of origin in parentheses and separated by commas]

***Paragraph (k) contracting officer fill-in information***

Contracting officer — select applicable item when an exemption to the Service Contract Labor Standards statute applies.

Paragraph k(1) is applicable. Paragraph k(2) is applicable.

52.222-56 CERTIFICATION REGARDING TRAFFICKING IN PERSONS COMPLIANCE PLAN (MAR 2015)

52.222-62 PAID SICK LEAVE UNDER EXECUTIVE ORDER 13706 (JAN 2017)

52.225-7 WAIVER OF BUY AMERICAN STATUTE FOR CIVIL AIRCRAFT AND RELATED ARTICLES (FEB 2016)

52.233-2 SERVICE OF PROTEST (SEPT 2006)

***fill-in information***

[Designate the official or location where a protest may be served on the Contracting Officer.]

DEA-2852.209-75 NATIONAL SECURITY RISK ASSESSMENT (JUN 2014)

(a) Any offeror responding to this solicitation acknowledges that before acquiring information technology equipment or software, the U.S. Department of Justice and its component entities will assess the supply chain risk of cyber-espionage or sabotage associated with the acquisition of such equipment or software, including any risk associated with such equipment or software being produced, manufactured, or assembled by one or more entities identified as posing a cyber-threat, including but not limited to, those that may be owned, directed, or subsidized by the People’s Republic of China.

(b) By submitting an offer to this solicitation, the Offeror understands and agrees that the Government retains the right to reject any offer or response to this solicitation made by the Offeror, without any further recourse by, or explanation to, the Offeror, if the Government determines the Offeror or the equipment or software offered by the Offeror, in whole or in part, presents an unacceptable risk to national security.

(c) To assist the Government in assessing whether the acquisition poses a national security risk, offerors are required to complete and submit with its offer or quotation the National Security Acquisition Risk Assessment Questions, which are attached to this solicitation. Offerors must answer all questions completely and accurately to the best of their knowledge and belief. All answers are to be reflective of the parent and subsidiary levels of an organization.

(d) Offerors are also required to request, collect, and forward with its offer or quotation completed National Security Acquisition Risk Assessment Questions from all subcontractors that will provide any equipment or software in performance of the contract or order. Offerors are responsible for the thoroughness and completeness of each subcontractor's submission.

(e) Failure to provide any such requested information may render a proposal unacceptable.

http://www.acquisition.gov/ https://www.acquisition.gov/sites/default/files/current/far/html/Subpart%204_12.html#wp1073667 https://www.acquisition.gov/sites/default/files/current/far/html/52_222.html#wp1163537 https://www.acquisition.gov/sites/default/files/current/far/html/52_222.html#wp1170084 https://www.acquisition.gov/far/current/html/52_223_226.html#wp1169222 http://acquisition.gov/far/current/html/52_233_240.html#wp1113323

SOLICITATION #: 15DDHQ18R00000019

52.252-2 CLAUSES INCORPORATED BY REFERENCE (FEB 1998)

This contract…