A02 - AIS IV SOO Draft.pdf

ATTACMENT 1

STATEMENT OF OBJECTIVES

DRUG ENFORCEMENT ADMINISTRATION

AVIATION DIVISION

AIRBORNE IMAGING SYSTEMS IV

1.0 OVERVIEW

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

2.0 SCOPE

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

A. Cessna 206 Aircraft B. Cessna 208 Aircraft C. Bell 407 Helicopter D. Bell 412 Helicopter

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 and Mission Equipment in accordance with any applicable FAA regulations and maintain the aircraft’s Standard Airworthy Certificate. Airborne Imaging Systems and Mission Equipment and or components with approved Supplemental Type Certificates are preferred but not mandatory.

3.0 PERFORMANCE REQUIREMENTS

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

3.1 AIRBORNE IMAGING SYSTEMS

3.1.1 CESSNA 206

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

A. One (1) L3Harris Wescam MX-10 Gyro-stabilized EO/IR imager, which will be provided as Government Furnished Property (GFP). See Exhibit 1 for imagers specifications.

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, which shall be Contractor Acquired Property (CAP). The MX-10 shall be attached to the camera mount utilizing a quick release mount, which shall be provided as CAP.

C. One (1) Shotover Ion High Definition Digital Video Recorder (or most current model), which shall be provided as CAP.

D. Two (2) Macro-Blue MB15W 15.6-inch High Definition Video Monitors, shall be provided as CAP and shall have the following minimum features:

1. Four HD-SDI video inputs.

2. Touch screen capability.

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1920 x 1200.

5. 16:10 ratio wide screen monitor.

6. NVIS class B compatible.

E. One (1) Shotover ARS-750 (or most current model) Augmented Reality Mapping

System, which will be provided as GFP.

F. One (1) Stowable Keyboard with touch pad, which shall be provided as CAP.

G. One (1) Technisonic RC-9100 Remote Control Head, which will be provided as

GFP.

H. Installation of one (1) Rear cargo door Medeco lock. The lock will be provided as

GFP, the installation shall be the responsibility of the Contractor.

I. Two (2) True Blue TA202 USB Charging Ports, one located within reach of the copilot and one located on the Operator Console. The True Blue USB Charging Ports shall be provided as CAP.

J. One (1) Operator Console, which shall be provided as CAP and shall consist of the two Macro-Blue MB17W video monitors, Shotover Ion digital video recorder, Shotover ARS-750 Augmented Reality Mapping System, stowable keyboard, Janteq AVITR3 Transceiver remote control unit, Technisonic RC-9100 remote control head and PS Engineering CTL45A control head (or previously installed audio/intercom controller) in a compact package giving the operator unobstructed legroom. The Technisonic RC-9100 remote control head shall be integrated into the Technisonic TDFM-9100 multiband radio; all other necessary components shall be CAP. The Operator Console shall be located in the rear cabin area directly behind the pilot and copilot’s seats within convenient reach of the operator and shall be easily removable by the utilization of wiring cable quick disconnects 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 for ease of viewing by the operator. The Operator Console shall be configured as to allow unimpeded egress from the aircraft.

K. For pilot reference, the Contractor shall route a separate video in control signal including the ARS-750 map overlay to the cockpit Garmin Multi-Function Display.

L. The Contractor shall integrate all Airborne Imaging System components into a user-friendly interface utilizing the touch screen capability of the monitors and the stowable keyboard. 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 imaging sensors and the ARS-750 Augmented Reality Mapping System data. Video selected from the primary monitor shall be directed, upon command to the Ion DVR or the ARS-750 or both for recording. The pilot’s reference video display shall be integrated to display video from any sensor selected by the operator along with the ARS-750 overlay.

M. The Contractor shall install and integrate the Janteq AViTR3 Transceiver System, which will be provided as GFP to transmit C-Band frequencies and while receiving L-Band frequencies allowing live video through a secure connection to and from ACRx citywide systems.

N. Aircraft intercom audio and ARS-750 map overlay shall not be recorded on the Ion DVR or ARS-750. ARS-750 map overlay is for operator reference only.

3.1.2 CESSNA 208

The Airborne Imaging Systems for each Cessna 208 aircraft shall consist of the

A. One (1) L3Harris Wescam MX-15HDi Gyro-stabilized EO/IR imager, which will be provided as GFP. See Exhibit 1 for imagers specifications.

B. The MX-15HDi shall be mounted on the left side of the aircraft via a fuselage camera mount, which shall be provided as CAP. The MX-15HDi shall be attached to the imager mount utilizing a quick release mount, which shall be provided as CAP.

C. One (1) Shotover Ion High Definition Digital Video Recorder (or most current model), which shall be provided as CAP.

D. Two (2) Macro-Blue MB17W 17-inch High Definition Video Monitors, which shall be provided as CAP and shall have the following minimum features:

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1920 x 1200.

G. Three (3) True Blue TA202 USB Charging Ports, one located within reach of the pilot, one within reach of the copilot and one located on the Operator Console. The True Blue USB Charging Ports shall be provided as CAP.

H. One (1) Technisonic RC-9100 Remote Control Head, which will be provided as GFP.

I. One (1) Operator Console, which shall be provided as CAP and shall consist of the two Macro-Blue MB17W video monitors, Shotover Ion digital video recorder, Shotover ARS-750 Augmented Reality Mapping System, stowable keyboard, Janteq AViTR3 Transceiver remote control unit, Technisonic RC-9100 remote control head and PS Engineering CTL45A control head (or previously installed audio/intercom controller) in a compact package giving the operator unobstructed legroom. The Technisonic RC- 9100 remote control head shall be integrated into the Technisonic TDFM-9100 multiband radio; all other necessary components shall be provided as CAP. The Operator Console shall be located in the rear cabin area on the left-hand side at Fuselage Station 205.0 within convenient reach of the operator and shall be easily removable by the utilization of wiring cable quick disconnects to allow for aircraft maintenance. The video monitors shall be mounted vertically, in a one on top of the other configuration and attached to individual swing arms to allow adjustment for ease of viewing by the operator. The Operator Console shall be configured as to allow

J. For pilot reference, the Contractor shall route a separate video in control signal

K. The Contractor shall integrate all Airborne Imaging System components into a user-friendly interface utilizing the touch screen capability of the monitors and the stowable keyboard. 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 imaging sensors and the ARS-750 Augmented Reality Mapping System data. Video selected from the primary monitor shall be directed, upon command to the Ion DVR or the ARS-750 or both for recording. The pilot’s reference video display shall be integrated to display video from any sensor selected by the operator along with the ARS-750 overlay.

L. The Contractor shall install and integrate the Janteq AViTR3 Transceiver System, which shall be provided as GFP to transmit C-Band frequencies and while receiving L- Band frequencies allowing live video through a secure connection to and from ACRx citywide systems.

M. Aircraft intercom audio and ARS-750 map overlay shall not be recorded on the Ion

DVR or ARS-750. ARS-750 map overlay is for operator reference only.

3.1.3 BELL 407

The Airborne Imaging Systems for each Bell 407 shall consist of the following:

provided as GFP. See Exhibit 1 for imager specifications.

B. The imager for the Bell 407 shall be mounted on the aircraft’s nose utilizing an imager mount, which shall be provided as CAP. The imager shall be attached to the imager mount utilizing a quick release dovetail mount, which shall be provided as CAP. Additionally, the landing light shall be relocated to the landing gear cross tube.

D. Two (2) Macro-Blue MB15W 15.6-inch High Definition Video Monitors, which shall be provided as CAP and shall have the following minimum features:

3. Anti-Reflective glass and sunlight readable.

4. Minimum resolution of 1920 x 1200 pixels.

6. NVIS class B compatible.

G. One (1) Technisonic RC-9100 Remote Control Head, which will be provided as

GFP.

H. One (1) Operator Console, which shall be provided as CAP and shall consist of the two Macro-Blue MB15W video monitors, Shotover Ion digital video recorder, Shotover ARS-750 Augmented Reality Mapping System, stowable keyboard, Janteq AViTR3 Transceiver remote control unit and Technisonic RC-9100 remote control head in a compact package giving the operator unobstructed legroom. The Technisonic RC-9100 remote control head shall be integrated into the existing Technisonic TDFM-9100 multiband radio; all other necessary components shall be provided as 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 by the utilization of wiring cable quick disconnects 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 for ease of viewing by the operator. The Operator Console shall be configured as to allow

The existing rear audio panel will remain in its current location; it will not be relocated to the Operator Console.

I. For pilot reference, the Contractor shall route a separate video in control signal

For aircraft not equipped with Garmin Avionics Systems, the Contractor shall install and integrate a seven-inch flip-up stowable monitor, which shall be provided as CAP and shall be mounted on the aircraft’s instrument panel for pilot reference.

The pilot’s reference monitor shall have a swivel base to allow adjustment for ease of viewing.

J. The Contractor shall integrate all Airborne Imaging System components into a user-friendly interface utilizing the touch screen capability of the monitors and the stowable keyboard. 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 imaging sensors and the ARS-750 Augmented Reality Mapping System data. Video selected from the primary monitor shall be directed, upon command to the Ion DVR or the ARS-750 or both for recording. The pilot’s reference video display shall be integrated to display video from any sensor selected by the operator along with the ARS-750 overlay.

K. Aircraft intercom audio and ARS-750 map overlay shall not be recorded on the Ion DVR or ARS-750. ARS-750 map overlay is for operator and pilot reference only.

L. The Contractor shall install and integrate the Janteq AViTR3 Transceiver System, which shall be provided as GFP to transmit C-Band frequencies and while receiving L-Band frequencies allowing live video through a secure connection to and from ACRx citywide systems.

M. The Bell 407 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 manufacturer’s Supplemental Type Certificate. NVIS manufacturer are either Aerodynamix or Ahlers.

3.1.4 BELL 412

The Airborne Imaging Systems for each Bell 412 shall consist of the following:

provided as GFP. See Exhibit 1 for imager specifications.

B. The Imager for the Bell 412 shall be mounted on the aircraft’s belly forward of the pilot’s position, the mount shall be provided as CAP. The imager shall be attached to the imager mount utilizing a quick release mount, which shall be provided as

CAP.

D. One (1) Apple iPad Pro 12.9-inch tablet for video display, which shall be provided as GFP.

E. Imager operation shall be through the Wescam handheld controller with video displayed via wireless connection on an Apple iPad Pro tablet. Video shall be recorded on the Ion digital video recorder. Aircraft intercom audio shall not be recorded on the DVR.

F. Two (2) separate imager handheld controller connections, one located in the cockpit and one located in the cabin area of the helicopter. This will allow operation of the imager from the cockpit or from the cabin area of the helicopter.

G. For pilot reference, the imager video shall route via wireless connection to any onboard iPad tablet for crew and passenger reference, iPad tablets shall be provided as GFP.

H. The Contractor shall integrate all Airborne Imaging System components into a user-friendly interface utilizing the touch screen capability of the iPad Pro tablet. Video selected from the iPad tablet shall be directed, upon command to the Ion DVR for recording.

I. The Bell 412 helicopter referenced in this SOO is equipped with Night Vision Imaging System (NVIS) lighting. The Airborne Imaging System shall be NVIS compatible and certified under Rebtech’s NVIS Supplemental Type Certificate.

3.2 AIRCRAFT MISSION EQUIPMENT

3.2.1 CESSNA 206 MULTI-BAND RADIOS

The Technisonic TDFM-9100 Multi-Band Radio and Motorola APX 7000/8000 Radio provisions for each Cessna 206 aircraft shall consist of the following:

A. The installation and integration of one (1) Technisonic TDFM-9100 Multi-band Radio, which will be provided as GFP and shall be located on the right side of the aircraft instrument panel.

B. The installation and integration of one (1) Technisonic RC-9100 remote control head, which will be provided as GFP and shall be located on the Operator Console.

C. The installation and integration of provisions for an external handheld radio a Motorola APX 7000/8000 which shall interface with the TDFM-9100 Multi-band radio. One handheld radio charger base shall be located within reach of the pilot and one within reach of the Operator Console. The handheld radio charger bases will be provided as GFP. The external handheld radio shall interface with the TDFM-9100 Multi-band radio via a DIN connector and interface cable, which shall be provided as CAP. See Exhibit 3 for external handheld radio interface cable specifications.

D. The installation and integration of three (3) Comant Tri-Band antennas, P/N:

CI 295-300, which shall be provided as CAP. Two (2) antennas shall be dedicated to the Technisonic TDFM-9100 and one (1) antenna shall be dedicated to the external handheld radio. All three antennas shall be mounted on the bottom of the aircraft.

3.2.2 CESSNA 206 PS ENGINEERING DIGITAL AUDIO SYSTEM

A. The installation and integration of a PS Engineering PAC45A digital audio system with two (2) CTL45A Control Heads, which will be provided as CAP. One Control Head shall be located within reach of the pilot and one shall be located on the Operator Console. See Exhibit 5 for the Audio Panels Configuration Table.

B. The installation and integration of one (1) Skye Avionics Ltd. Headset Drop

Cord, P/N SAL-203-12 shall be located on the Operator Console. The Skye Avionics Ltd. Headset Drop Cord shall be provided as CAP.

C. The installation and integration of one (1) Lektro Foot Switch, P/N L-2-S shall be located on the Operator Console. The Lektro Foot Switch, which shall be provided as CAP.

3.2.3 CESSNA 206/CESSNA 208/BELL 407 TRANSCEIVER SYSTEM

The Downlink system for each aircraft type shall consist of the following:

A. One (1) Janteq AViTR3 Transceiver System, which will be provided as

GFP. See Exhibit 2 for downlink specifications.

B. One (1) Janteq AViTR3 Transceiver Remote Control Unit, which will be provided as GFP and shall be mounted on the Operator Console.

C. Antennas

1. Two (2) Peak Antennas Wideband Hemispherical Omni C-Band Antennas, part number WHO180, which will be provided as GFP.

2. Two (2) Peak Antennas Wideband Hemispherical Omni L-Band Antennas, part number WHO470, which will be provided as GFP.

3. 2 foot spacing must be maintained between each WHO180 and WHO470 antenna to avoid interference

4. Antennas shall be configured on the bottom of the aircraft to ensure adequate separation of each antenna type, and maximize diversity transmission and reception. Spacing and placement shall minimize interruption of connectivity with the stationary ground antenna during normal flight configurations for surveillance operations.

D. Janteq AViTR3 Transceiver Configuration and Integration

1. The contractor shall integrate the video output of the imager and ARS-

750 with a two-way toggle switch for “ARS” (video with mapping overlay) and “VIC” (video without overlay) for transmission to the ACRx citywide system.

2. The contractor shall integrate the data transmission capability of the AViTR3 Transceiver to a Local Area Network (LAN) to provide the

1. Data connection to the ARS-750 system for Tactical

Awareness Kit utilization.

2. Provide a separate LAN data connection/port for future Tactical Communication Device utilization.

3.2.4 CESSNA 206 CABIN EQUIPMENT

Aircraft Mission Equipment for each Cessna 206 shall consist of the following:

A. Installation of one (1) North Point Aviation (Soloy) Observation Seat, which

B. Installation of one (1) North Point Aviation (Soloy) Headliner, which shall be provided as CAP.

3.2.6 CESSNA 208 MULTI-BAND RADIOS

The Technisonic TDFM-9100 Multi-Band Radio and Motorola APX 7000/8000 Radio provisions for each Cessna 208 aircraft shall consist of the following:

band Transceiver, which will be provided as GFP and shall be located on the center section of the aircraft instrument panel.

control head, which will be provided as GFP and shall be located on the a Motorola APX 7000/8000 which shall interface with the TDFM-9100 Multi-band radio. One handheld radio charger base shall be located within reach of the pilot and one within reach of the Operator Console. The handheld radio charger bases will be provided as GFP. The external handheld radio shall interface with the TDFM-9100 Multi-band radio via a DIN connector and interface cable, which shall be provided as CAP. See

CI 295-300, which shall be provided as CAP. Two (2) antennas shall be dedicated to the Technisonic TDFM-9100 and one (1) antenna shall be dedicated to the external handheld radio. All three antennas shall be mounted on the bottom of the aircraft.

3.2.7 CESSNA 208 PS ENGINEERING DIGITAL AUDIO SYSTEM

system with two (2) CTL45A Control Heads, which will be provided as CAP. One Control Head shall be located within reach of the pilot and one

3.2.8 BELL 407 MULTI-BAND RADIOS

Technisonic TDFM-9100 Multi-Band Radio and Motorola APX 7000/8000 Radio provisions for each Bell 407 aircraft shall consist of the following:

band Transceiver, which will be provided as GFP and will be located on the center aircraft instrument console.

control head, which will be provided as GFP and will be located on the a Motorola APX 7000/8000 which will interface with the TDFM-9100 Multi-band radio. One handheld radio charger base shall be located within reach of the pilot and one within reach of the Operator Console. The handheld radio charger bases will be provided as GFP. The external handheld radio will interface with the TDFM-9100 Multi-band radio via a DIN connector and interface cable, which will be provided as CAP. See

CI 295-300, which shall be provided as CAP. Two (2) antennas will be dedicated to the Technisonic TDFM-9100 and one (1) antenna will be dedicated to the external handheld radio. All three antennas shall be mounted on the bottom of the aircraft. See Exhibit 4 for antenna mounting locations.

3.2.9 BELL 407 PS ENGINEERING DIGITAL AUDIO SYSTEM

system with two (2) CTL45A Control Heads, which will be provided as GFP. One Control Head shall be located within reach of the pilot and one shall be provided as CAP.

4.0 PERIOD OF PERFORMANCE AND PLACE OF PERFORMANCE

The objective of this procurement is to install an indefinite quantity of Airborne Imaging Systems and Mission Equipment on an indefinite quantity (IDIQ) of DEA aircraft. The Period of Performance shall 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 and Mission Equipment 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 and Mission Equipment 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 PROPERTY (GFP)

The Government Furnished Property shall consist of the following:

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

A. Cessna 206 aircraft, (nine each) B. Cessna 208/208B aircraft, (two each) C. Bell 407 helicopters, (five each) D. Bell 412 helicopter, (one each) E. L3Harris Wescam MX-10 Imagers, (Harnesses and cabling are not provided, they shall be CAP)

1. Hand Controller

2. GPS Antenna

3. Cable External, GPS Extension

4. Hand Controller Mounting Bracket

5. Imager Shipping Case

F. L3Harris Wescam MX-15HDi Imagers, (Harnesses and cabling are not included, they shall be CAP)

1. Hand Controller

2. Laser Arming Panel, (MX-15HDi only)

3. GPS Antenna

4. Cable External, GPS Extension

5. Hand Controller Mounting Bracket

6. Imager Shipping Case

G. Shotover Systems ARS-750, (or most current model) Augmented Reality

Mapping System H. Technisonic TDFM-9100 multiband radio I. Technisonic RC-9100 Remote Control Head J. Janteq AViTR3 Transceiver System K. Janteq Transceiver Remote Control Unit L. Two (2) Peak Antennas Wideband Hemispherical Omni C-Band Antennas, part number WHO180, for the Janteq AViTR3 Transceiver System M. Two (2) Peak Antennas Wideband Hemispherical Omni L-Band Antennas, part number WHO470, for the Janteq AViTR3 Transceiver System

5.2 CONTRACTOR ACQUIRED PROPERTY

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

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 and Mission Equipment in Government-owned and operated (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 maintenance and inspection.

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 and Mission Equipment.

H. The Contractor shall ensure the aircraft, in its final configuration with the complete Airborne Imaging System and Mission Equipment installed does not adversely affect the center of gravity of the aircraft. The aircraft shall be physically weighed upon completion of the Airborne Imaging System and Mission Equipment installation and a new aircraft Weight and Balance Report be provided.

I. The Contractor shall develop an Airborne Imaging System and Mission Equipment acceptance checklist to be utilized in the acceptance of the installed systems. 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 and Mission Equipment. The Contractor shall submit the acceptance checklist to the Government for approval prior the utilization of 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 and Mission Equipment shall be 100% operational prior to the Government’s acceptance and delivery 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 and delivery of the aircraft has occurred.

B. The Contractor shall be responsible for certification of the complete Airborne Imaging System and Mission Equipment 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, as necessary 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 provide a point-of contact for technical and operator support.

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 and Mission Equipment 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 and Mission Equipment 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 and Mission Equipment detailed illustrated parts catalog.

E. Airborne Imaging System and Mission Equipment detailed operator’s manual.

F. Airborne Imaging System and Mission Equipment detailed maintenance manual.

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

H. Airborne Imaging System and Mission Equipment 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.

The Contractor shall ensure that revisions to any technical publication are forwarded to the effected Airborne Imaging System and Mission Equipment within five business days of being published.

14.0 TRAINING

The Contractor shall conduct Airborne Imaging System operator training, this training shall commence within 30 days of the aircraft acceptance. The Contractor shall develop the syllabus, training manuals and provide any necessary materials. This training shall include classroom and a minimum of two flight hours per operator. The training shall include up to seven (7) 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 Contractor shall develop the syllabus, training manuals and provide any necessary materials. 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.

Travel for training will be authorized by the COR. Travel cost will be reimbursed as per Federal Travel Regulations.

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 System and Mission Equipment shall extend for a minimum period of one (1) year after final acceptance and delivery 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.