Statement of Requirements (SOR) Rev 2.pdf

COMBINED SYNOPSIS/SOLICITATION 70Z03823QE0000015

STATEMENT OF REQUIREMENTS (SOR) REV 2

BACKGROUND

The United States Coast Guard (USCG), Aviation Logistics Center (ALC), Engineering Services

Division (ESD) has a requirement for the manufacture of first articles and if approved, the subsequent manufacture of additional quantities of the cameras listed below:

NOMENCLATURE PART NUMBER (PN)

Hoist Camera HC60651-1

Cabin Camera CC60652-1

These Cameras are mounted on USCG rotary wing aircraft which are used to perform various missions such as search and rescue and law enforcement. The Hoist Camera is installed on the hoist platform facing down to display the hoisting evolution. The Cabin Camera is only used on the MH-60T helicopter and is installed in the cabin facing the door to record the hoisting evolution from within the cabin.

Running on the aircraft’s power system and with no user input, the cameras are automatically operational and recording whenever the aircraft is electrified.

SCOPE

A. General Requirements

The following requirements apply to both Cameras and all work under this order. This acquisition is subject to FAR 52.209-4, First Article Approval – Government Testing (Sep 1989). In addition to the information provided in this SOR, the Contractor should carefully review the text of FAR clause 52.209-

4 as well as the Instructions to Offerors and Evaluation Criteria provided in this acquisition’s Terms and

Conditions. For clarity’s sake, when the term Camera is utilized throughout this document, it shall refer to information and/or characteristics common to both the Hoist and Cabin Cameras.

All work shall be performed at the Contractor’s facility or other USCG-approved facility. The

Contractor shall provide all necessary materials, labor, tooling, equipment, and infrastructure to manufacture the Cameras. All services shall be accomplished as directed by the Government and any substantive requests for clarification shall be directed to the Contracting Officer or their designee. The

Contractor shall not exceed the firm fixed prices in the Schedule without prior authorization from the

Contracting Officer in the form of a signed, executed order modification.

The USCG is unable to provide drawings for the manufacture of these Cameras. In addition to the detailed specifications provided in this SOR, a sample mount will be provided to ensure the Cameras fit and are functional to with the existing aircraft mounts and connectors.

The USCG shall provide one Hoist Camera and one Mounting Bracket (PN: SVS-025-SS) as

Government Furnished Property (GFP) for the purposes of reverse engineering. The GFP shall be provided in a “ready for issue” condition. The Contractor shall accomplish a thorough inspection of the

GFP and report any deficiencies to the Government technical point of contact (POC). The technical POC will be determined upon award and contact information provided to the Contractor. Both items furnished as GFP shall be returned to the Government no later than thirty (30) days after written approval of the first articles under Line Items 2 and 4 in the Schedule.

For the purposes of quoting, pictures of the Mounting Bracket (PN: SVS-025-SS) along with detailed measurements are provided in Exhibit A – Sample Mounting Bracket Dimensions and Pictures.

The USCG is not able to provide any tooling as GFP for the manufacture of the Cameras. The

Contractor shall manufacture all special, non-standard tooling such as injection molds required specifically for the manufacture of the Cameras and retain it on-site as Government property. The

Contractor shall store all special, non-standard tooling in a protected, climate-controlled location for a period of three (3) years and be responsible for any damage which may occur during said storage period.

After a period of three (3) years and if no additional orders were placed for the Cameras during that time, the Contractor shall request disposition instructions for the tooling in writing from the Contracting

Officer or their designee. However, if a new order is awarded to the Contractor for the manufacture of either Camera, the three-year storage period shall reset and restart to the effective date of the last order.

The cost of specialized tooling, research and development, testing, and any other costs associated with reverse engineering the Cameras shall be included as Non-Recurring Engineering (NRE) costs as shown in the Schedule. The Contractor shall endeavor to minimize NRE costs where possible and shall divide such costs proportional to each Camera given their many shared performance specifications. Any specialized tooling developed for the manufacture of the Cameras shall be considered part of the NRE costs and as such, shall be considered paid for and owned by the Government.

The Offeror’s standard commercial warranty shall apply to this order and the terms of that standard warranty shall be provided with the offer. The warranty shall clearly state: (1) the exact nature of the item and its components as well as the characteristics that the offeror’s warranty covers; (2) the extent of the warranty including all the Contractor’s obligations to the Government for breach of warranty; (3) specific remedies available to the Government; and (4) the scope and duration of the warranty. Offered warranties that exceed the standard commercial warranty will be considered.

ALC considers items Ready-for-Issue (RFI) upon acceptance. The Contractor shall furnish a Certificate of Conformance (COC) IAW FAR 52.246-15 for all Cameras. Items determined to be non-RFI upon installation or operation may be returned to the Contractor for correction at Contractor’s expense.

Deficiencies will be described in a Product Quality Deficiency Report (PQDR) and sent to the

Contractor prior to the return of any item.

B. Applicable Documents

Abbreviations

MIL-STD = Military Standard

MIL-DTL = Military Detail Specification

RTCA = Radio Technical Commission for Aeronautics

MIL-STD-130N, Department of Defense (DoD) Standard Practice: Identification Marking of U.S.

Military Property (17 Dec 2007).

MIL-STD-461E, DoD Interface Standard: Requirements for the Control of Electromagnetic Interference

Characteristics of Subsystems and Equipment (20 Aug 1999). [Supersedes MIL-STD-461D/MIL-STD-

462D]

MIL-STD-704F, DoD Interface Standard: Aircraft Electric Power Characteristics (12 Mar 2004).

MIL-STD-810H, DoD Test Method Standard: Environmental Engineering Considerations and

Laboratory Tests (31 Jan 2019).

MIL-DTL-38999L, DoD Detail Specification: Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded, and Breech Coupling), Environment Resistant, Removable

Crimp and Hermetic Solder Contacts, General Specification For (30 May 2008).

MIL-DTL-26482H, DoD Detail Specification: Connectors, Electrical, (Circular, Miniature, Quick

Disconnect, Environment Resisting), Receptacles and Plugs, General Specification For (7 Dec 2009).

RTCA/DO-160, Versions D, E, F, and G – Environmental Conditions and Test Procedures for Airborne

Equipment (dated 27 Jul 1997, 20 Dec 2005, 6 Dec 2007, and 8 Dec 2010 respectively).

C. Performance Specifications

The following are common characteristics of both Cameras. All Cameras manufactured under this order shall comply with all requirements listed. The Camera shall:

1. not exceed two (2) pounds.

2. be 100% waterproof to protect electronics and optics.

3. be manufactured of a material that withstands saltwater corrosion.

4. withstand shock and vibration of up to 20G’s.

5. operate at a temperature range from minus forty degrees Celsius (-40° C) to fifty-five degrees

Celsius (55° C).

6. adhere to all applicable MIL-STDs or commercial aviation standard equivalents (RTCA/DO-

160)

7. include a visible orientation mark, at the 12 o’clock position, on the face of the camera near the lens and connector.

8. be marked with a visible part number and serial number.

9. operate on 28 VDC (volts direct current), two wires positive and neutral.

10. accomplish aircraft grounding with the outer shell of the connector.

11. utilize existing aircraft connector part number KPT02E12-3PA 206 (manufactured by ITT

CANNON) with black zinc cobalt oxide finish (reference MIL-DTL-26482 series). It is a 3-pin connector, with pin A (composite video), pin B (28 VDC), and pin C (neutral).

a. Part number KPT02E12-3P (manufactured by ITT CANNON) with conductive olive drab chromate over cadmium finish is an acceptable substitute for part number KPT02E12-

3PA 206.

12. have a high resolution, 1/3-inch Color Charge-Coupled Device (CCD) camera with 550 TV lines or better.

a. This specification outlines minimum requirements and is based on a thirteen-year-old design so improvements in technology are to be expected. A CMOS imager is acceptable.

We need cameras that, at minimum, provide the functionality stated in these requirements; exceeding these requirements is acceptable.

13. have a minimum illumination/low light mode of 0.1 Lux at F2.0 color and 0.05 Lux at F2.0 monochrome or better.

14. include a Programmable Digital Signal Processor (DSP) with day and night configuration.

15. output composite video RS-170A (NTSC Color Video) 1V p-p (peak to peak).

16. have camera glass with a surface quality of 60-40 or better.

17. have a fog-proof lens capable of handling altitude changes from 0 to 10,000 feet AGL (above ground level).

18. include a mounting bracket with each Camera. A sample mounting bracket will be provided. The mount shall be manufactured from T304 stainless steel and corrosion resistant. It should also allow the Camera to be adjusted left to right and up and down.

19. Hardware for the mounting bracket shall be made of Type 316 stainless steel and consists of four

(4) each:

a. ¼-20X3/8 Phillips pan-head screws

b. ¼” flat washers

c. ¼” lock washers

Hoist Camera Specific Optics and Information

The Hoist Camera shall have a fixed 3.6mm lens with a camera field of view (fov) of 54° vertical X 70° horizontally. The Hoist Camera shall capture video between 40 and 100 feet below the helicopter.

Cabin Camera Specific Optics

The Cabin Camera shall have a fixed 2.5mm lens with a camera field of view (fov) of 74°V X 90° H.

D. First Article Submission

The Contractor shall provide the Hoist Camera and Cabin Camera first articles to the USCG within ninety (90) calendar days after award. Shipment of the first articles shall be to the USCG using traceable means (e.g. Federal Express, United Parcel Services). The USCG shall test the first articles and provide feedback to the Contractor in writing within thirty (30) calendar days after receipt. If discrepancies are found, the first article(s) will be returned to the Contractor for correction. The

Contractor shall correct all discrepancies and resubmit the first article(s) to the USCG within thirty (30) calendar days for a second inspection. The final inspection and approval for the first article will be issued in writing from the Contracting Officer. Additional information about this requirement can be found in the Terms and Conditions under FAR clause 52.209-4.

The USCG requires delivery of the production quantities to begin no later than sixty (60) calendar days after the written approval of the first article at a rate of five (5) each Hoist Cameras and five (5) each

Cabin Cameras per month.

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