Amendment 0004 - FULL Package (Use PDF bookmarks to navigate).Use PDF bookmarks to navigate

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT

1. CONTRACT ID CODE

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

PAGE OF PAGES

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

8. NAME AND ADDRESS OF CONTRACTOR (No., street, county, State and ZIP Code)

CODE

9A. AMENDMENT OF SOLICITATION NO.

9B. DATED (SEE ITEM 11)

10A. MODIFICATION OF CONTRACT/ORDER NO.

10B. DATED (SEE ITEM 13)

CODE FACILITY CODE

11. THIS ITEM ONLY APPLIES TO AMENDMENTS OF SOLICITATIONS

The above numbered solicitation is amended as set forth in Item 14. The hour and date specified for receipt of Offers

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

Items 8 and 15, and returning is extended, is not extended.

12. ACCOUNTING AND APPROPRIATION DATA (If required.)

13. THIS ITEM APPLIES ONLY TO MODIFICATIONS OF CONTRACTS/ORDERS. IT MODIFIES THE CONTRACT/ORDER NO. AS DESCRIBED IN ITEM 14.

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

B. THE ABOVE NUMBERED CONTRACT/ORDER IS MODIFIED TO REFLECT THE ADMINISTRATIVE CHANGES (such as changes in paying office, C. THIS SUPPLEMENTAL AGREEMENT IS ENTERED INTO PURSUANT TO THE AUTHORITY OF:

D. OTHER (Specify type of modification and authority) appropriation date, etc.) SET FORTH IN ITEM 14.

E. IMPORTANT: Contractor is not, is required to sign this document and return

ORDER NO. IN ITEM 10A.

1 2

3. EFFECTIVE DATE

09/28/2018

AAQ-240 SERVICES BRANCH

Orville Wright Bldg. (FOB10A), Room 406W FAA National Headquarters 800 Independence Ave., SW

AAQ240-AFN

Washington DC 20591 x

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

separate letter or telegram which includes a reference to the solicitation and amendment number. FAILURE OF YOUR ACKNOWLEDGEMENT TO BE RECEIVED AT

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

copies of the amendment; (b) By acknowledging receipt of this amendment on each copy of the offer submitted ; or (c) By ___________ 1 x x

693KA7-18-R-00010

1 copies to the issuing office.

08/13/2018

(x)

See continuation page

16A. NAME AND TITLE OF CONTRACTING OFFICER (Type or print)15A. NAME AND TITLE OF SIGNER (Type or print)

15C. DATE SIGNED 16B. CONTRACT AUTHORITY 15B. CONTRACTOR/OFFEROR 16C. DATE SIGNED

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

Haynes W. Thompson

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

x

693KA7-18-R-00010-0004

Continuation Page

The purpose of this Amendment is to:

a. Provide responses to vendor submitted questions and comments

b. Provide amended SIR Sections and attachments

As a result of the foregoing, SIR 693KA7-18-R-00010 is amended as follows:

1. Responses to vendor submitted questions and comments are provided. See attachment.

2. In view of the foregoing, the following SIR Sections and attachments have been amended.

Offerors must remove the Sections & Attachments provided in the SIR and replace with the

Sections & Attachments identified in the below table, attached hereto and a part hereof:

attached hereto and a part hereof:

Section # of pages

C 11

E 3

F 1

J (index) 1

J-1 11

J-2 210

J-6 (add) 38

L 13

3. All other terms and conditions remain unchanged.

Attachment: CMM Submitted Questions & Responses, 4 pages

CMM Submitted Questions and Responses Clutter Map Memory

SIR 693KA7-18-R-0010

Amendment 0004

Q No. Reference Vendor Comment Amendment Response

Attachment J-1 Clutter Map

Memory CCA Control Signals, Section 2.3.2.5.2.1.2.1.2.4.5 Error

Register: (Page 2-219 PDF page

48)

This critical section is truncated, although figure 11-24 is provided, Page 2-220 should be include to complete the Error Register definition

Page 2-220 is provided. See page 9 of the revised

Attachment J-1.

Attachment J-2: Engineering

Drawings and Part List: (PDF Page

51)

The Engineering drawings do not include any mechanical dimensions.

Are the original board gerbers, or other engineering resources available to accurately place the connector and extraction components for the board?

Original Gerber files are not available. However, see revised attachment J-2 which incorporates Drawing

ID21062 & parts list (pages 203-210).

Attachment J-22: Engineering

Drawings and Part List:

(PDF Pages 53-54):

Components 645A670H02, 138C909H03, and 581R848H02 have been identified as critical for Form/Fit/Function equivalent. These parts seem to not be available on the open market or have extensive lead times. Are there known sources available for these critical connectors/extractors, and guide pins?

It is the Offerors responsibility to source the required parts or identify Form-Fit-Function equivalents. P/N

6454670H02 may be available through Amphenol Corp.

The Government does not have information for known suppliers of P/Ns 138C909H03 and 581R848H02. The preceeding information does not represent an endorsement of the suppliers noted or availablity of parts.

Attachment J-1, J-3, J-4 Missing

Timing requirements

There are several timing diagrams, but none have the timing requirements associated with them, like setup/hold requirements of the various signals. Do these exists, or will these have to be reverse engineered from the existing board?

The Government does not have the timing diagrams. The

Government requires the Offeror to reverse engineer the timing diagrams from the existing boards.

Part I Section C Page 5 (PDF Page

7) 5-C Environmental

Specifies 0-50 C operation conditions. The original components appear to be primarily mil spec (-55 C to 125C) components. Are industrial temp components (-40 C to 85C) acceptable for the redesign?

Yes, see revised Section C, Page 5, Development Test Plan and Procedures, Paragraph 5c)

6 General Electronic Design

The original design used 55 memory components arranged in 5 banks to create the 320 Kbits of Clutter Memory. Current technology allows a signal chip to be used for the on board memory. The original design also had all components socked to be field replaceable. Is it acceptable to minimize the design components with modern surface mount memories and have them directly soldered to the PCB?

Yes.

7 Error Detect and Correct Logic:

The original design has 1 bit correct 2 bit detect. Using more check bits, 2 bit correct, 3 bit detect is possible. Should this logic be improved where possible?

Yes.

8 General Technical Question Are there any ROHS (or Lead Solder) requirements for this design? No.

9 Test Stand Will the FAA provide a test stand that will operate the FFF redesigned

Clutter Memory CCA board?

No. The Offeror is required per the Statement of Work to provide the test stand in accordance with Section C 9.0, Test Equipment (CLIN 0006) (FFP)

9a If no:

Will FAA provide the detailed timing diagrams for all system signals?

• Clock frequency tolerance/jitter

• Setup/Hold time for signals

• Rise/Fall time tolerance

• Noise tolerance

Reference Government response to Vendor Comment #4

U9 (5962-8760201XX or

585R644H02) – Error Detection &

Correction

Will FAA provide datasheet for this part? Datasheet 585R644 is provided. See pages 10 through 50 of the revised Attachment J-2.

10a

U9 (5962-8760201XX or

585R644H02) – Error Detection &

Correction

Does FAA have any detailed engineering timing or data on this circuit?

Reference Government response to Vendor Comment #4

11 General Technical Question

Will FAA provide detailed drawings of the PCB?

• Board outline dimensions with tolerances

• Board cutout dimensions and tolerances

• Board thickness dimension and tolerances

• Board material requirements

Reference Government response to Vendor Comment #2

Amendment 0004

Q No. Reference Vendor Comment Amendment Response

12 General Technical Question

Will FAA provide datasheets for the following Identifying Part

Numbers?

a. 138C909H03

b. MS51923-157

c. 153C638H01

d. 645A670H02

e. 581R848H02

f. 635A866H04

g. M38510/30001BCX

h. M38510/30003BCX

i. 645A544H01

j. 635A861H01

k. M38510/32403BRX

l. M38510/30702BEX

m. M38510/07005BCX

n. M38510/32503BRX

o. M39510/30109BEX

p. M38510/31004BCX

q. M38510/07001BCX

r. M38510/07106BEX

s. M38510/07003BCX

The Government is only able to provide the below data sheets, incorporated into the revised Attachment J-2:

a. 138C909 page 51-52

C. 153C638 page 53-55

d. 645A670 page 56-76

e. 581R848 page 77-112

f. 635A866 pages 113-157

i. 645A544 pages 158-181

j. 635A861 pages 182-202

13 General Technical Question It appears the bid for this board is to replicate a design from 1985 -

1993. Do I understand the goal here correctly?

The Government requires the offeror to develop a Form-

Fit-Function equivalent. The offeror may replicate the existing design at their discretion, but satisfying the terms of the Statement of Work.

14 General Technical Question

I’d like to request the Gerber files and any drawings for the bare boards, as well as the bill of materials and any drawings for the assembly please for this RFP

Gerber files are not available. Please see revised

Attachment J-2 for available drawings and datasheets.

15 General Technical Question For schematic and PCB layouts, can we provide source files in OrCAD and Cadence Allegro instead of Altium?

No. Files must be submitted using Altium format. See revised Section C, page 4, as amended.

Section C (Statement of Work),

4.0 Prototype Units (CLIN 0002)

(FFP), page 5 of 11; 5.0, Pre-

Production Units (CLIN 0003)

(FFP), page 7 of 11; 6.0 First

Article Units (CLIN 0004) FFP, page

9 of 11; and 7.0 Production Units

(CLIN 0005) FFP, page 10 of 11.

Will you accept the schematics and PCB design files in other than the

Altium Designer format, for example, OrCAD Capture and OrCAD PCB

Editor?

Reference Government response to Vendor Comment #15

17 Section 5.1

"For each CMM CCA, electrical continuity & isolation PCB must be performed." Does this requirement refer to the blank unassembled

PCB, or the final soldered CCA (which, based on our experience, does not make sense)?

The Government requires electrical continuity and isolation for the blank unassembled PCBs. See revised

Section C, Section 5.1, as amended.

18 Section 9.0 What level of test is required for the test equipment (logic function only, power consumption, I/O levels, timing measurements?, etc.)

The level of testing required is predicated on the Offerors proposed solution.

19 Section 9.0

Some of the testing (if required) will necessitate the integration of off-the-shelf 3rd party test equipment. In that case, do we bid the test equipment as fully integrated, or allow FAA to purchase the equipment separately from the proprietary portion of the test equipment?

Offerors are to propose the test equipment as fully integrated.

20 Section 12.0 Is the Government furnished CCA in functional order? Yes.

21 General Technical Question

Missing documents that would be helpful. Are these available?

a. Dwg. No. 647A001 "Test spec" (important but not critical)

b. Dwg. No. 138C909H03 "Extractor" F/N 011 (important but not critical)

c. Dwg. No. 153C638H01 "Stiffener" F/N 013 (important but not critical)

d. Dwg. No. 645A670H02 "Connector P1" F/N 014 (critical)

The Government has included the following drawings as part of Attachment J, as specified herein:

a. Dwg. No. 647A001 "Test spec" - see revised J-1 pages 10 through 13

For the following drawings, reference Government response to Vendor Comment #12:

b. Dwg. No. 138C909H03 "Extractor" F/N 011,

c. Dwg. No. 153C638H01 "Stiffener" F/N 013,

d. Dwg. No. 645A670H02 "Connector P1" F/N 014.

22 General Technical Question

There is an edge connector on the opposite end of the CCA from P1.

We assume that this is where Test Points (in schematic) are terminated, for testing or debugging using an older test set-up. Are we required to be compatible with these connection points for testing or debugging using legacy testers or procedures also?

Yes, the connection points must be compatiable with legacy testers and procedures for testing and debugging.

Amendment 0004

Q No. Reference Vendor Comment Amendment Response

23 General Technical Question

For the memory in the CCA, we intend to use Static RAM (SRAM), not

DRAM as used in the legacy design. Are the error checking / correction functions required for the new SRAM design, if we can demonstrate with analysis and calculations that the error rate of the

SRAM approach without error detection or correction will have a lower error rate than the error-corrected DRAM? Alternatively, we can implement the error detection and correction functions with the

SRAM, and keep that functionality identical to the legacy design, but it would be moot and wasteful of manpower and logic gates.

Use of SRAM is acceptable.

24 SIR Evaluation Question What are the criteria for selecting the contractor for awarding this contract?

The FAA will perform evaluations based on the Offeror’s response to the SIR and in accordance with the evaluation factors for award as described in Part 4 - Section M. The

Offeror must clearly address each factor identified in SIR

Section M

It appears as though there are other cards in this system and we wanted to find out if you are seeking replacements for any of those as well.

No. The Government is only soliciting a solution for the

CMM CCA.

Part 4, Section L, L.18, page 11 of

Should the text be “Volume III Price Proposal”?

Yes. Additionally, Section L.17 should be changed from

"Volume III Past Peformance" to "Volume II Past

Performance". See revised Section L.

Part 1, Section C, SOW 6.0 CLIN

0004 First Article Units

CLIN 0004 First Article Units, FFP has a delivery date of “within 90 days” while Section F.2 has CLIN 0004 as “120 days”. Which delivery date is correct?

The delivery schedule for CLIN 0004, First Article units, is

90 days after Government approval of pre-production units. See revised Section F.2.

Part 1, Section F.2, CLIN 0007, Optional Production Units

It appears the word “Exercised” is missing from the statement, “No later than ten (10) days from the date of delivery of final production unit. Section C, SOW 10.0, appears correct and has the following text

“…and may exercise this option within ten (10) days from the date of delivery of the final production unit”.

CLIN 0007 is subject to AMS Clause 3.2.4-33 Option to

Increase Quantity - Separately Priced Line Item (Apr 1996).

See revised Section F.2 CLIN 0007 which states, "Delivery of optional units shall continue at the same rate that like items are called for under the contract, if the option is exercised."

Part 1, Section C, SOW Section

2.0, page 3 of 11. List of Applicable

Documents, Item 5: 3.3.1.4.7

Conformal Coating of Printed

Circuit Boards

The referenced section in Attachment J-5, FAA-G-2100H, makes it unclear if the vendor is required to conformal coat the new CMM

CAA or not. Please clarify.

Conformal coating is not required. If the offeror chooses to utilize components that are moisture-sensitive, then the offeror must apply applicable portions of FAA-G-2100H

Part 1, Section C, SOW Section

2.0, page 3 of 11. List of Applicable

Documents, Item 5: 3.3.1.4.8

Electromagnetic Shielding.

The referenced section in Attachment J-5, FAA-G-2100H, references another FAA document, FAA-STD-020. We do not have this document and the guidance to this section is not clear. Please clarify.

FAA-STD-020b is provided at Attachment J-6

31 Part 1, Section C, SOW listed within each CLIN deliverables is a reference to the schematic package Altium. Sometime the reference is “e.g., Altium” and sometimes it is referenced without the “e.g.”. Is the vendor permitted to use ORCAD for schematic capture development in this project, and not Altium?

Reference Government response to Vendor Comment #15

Attachment J, document TI

6310.26, page 2-214, Section

2.3.2.5.2.1.2.1.2.3 Memory Map

Controls.

How is the memory partitioned in banks? How big are the partitions?

Would it be possible for the FAA to provide a complete memory map of the CMM CCA?

The Government does not have this specific data available.

The Government cannot provide a complete CMM CCA memory map.

33 Attachment J, CCM CCA Are there additional Input/Output timing diagrams available? No.

Attachment J, document TI

6310.26, Figure 11-24, Target and two-level weather detector signal flow diagram (Sheet 2)

Are there any additional I/O signals for the CMM, other than power and Test Points, not shown in the diagram? Additionally, is there relevant information in (Sheet 1) which is not currently in the SIR package?

No additional data is available.

Attachment J, document TI

6310.38, Figure 11-48 Clutter map schematic diagram (Sheet 22 –

END)

What are the current limitations on the input +5V power, per connector pin? Note: this may not be an issue for today’s electronic components, but wanted to verify this point with the FAA.

Additionally, does the FAA have any data on the ripple level associated with the +5V power?

The Government requirement is 3 amps per pin.

36 General Technical Question

The legacy CCM CCA has a large bank of Test Points. Does the vendor have to replicate these Test Points as part of Fit, Form and Function?

Or is the vendor permitted to develop a new test point scheme. Note, any new design will have a different circuit implementation and different Test Points.

Reference Government response to Vendor Comment #22

Attachment J, J3, page 2-446, Section 2.43.7

Can the vendor implement any Memory ECC logic the meets the criteria of section 2.43.7? If the FAA requires the current EEC method to be used, can the associated data be provided?

The Offeror may implement any Memory EEC that meets the criteria of Section 2.43.7. The Government does not require the Offeror to use the current EEC method. The

Offeror may choose the current EEC method at its discretion.

Amendment 0004

Q No. Reference Vendor Comment Amendment Response

38 General Question Deliverable dates described in days, are those work days or does that include weekends/holidays?

Days mean calendar days, which includes weekends and holidays.

39 General Technical Question Are there any known sources for the connector? Reference Government response to Vendor Comment #3

40 General Technical Question Are there air flow requirements for cooling?

The Government does not have an air flow requirement for the CMM CCA

41 General Technical Question Will the Government provide sample of the CCA for the awarded contractor for analysis and comparison during the design?

Yes. See Section C, Statement of Work (SOW) Paragraph

12.0 Government Furnished Equipment

42 General Technical Question

The SIR includes a parts list for the Card components. IT lists JAN/MIL

MFR part no for the Connector (P1) on page 8-280 as P/N

645A670H2. This is the design company internal part number. The

SIR includes a datasheet for the next part on the list (635A866H04) which is a memory IC. Could you provide additional datasheet for the connector or provide source control drawing info that might point to possible vendor data for the P1 connector?

Reference Government response to Vendor Comment #12

43 General Technical Question We take the existing boards and re-work them and provide a 1-2 year warranty. Would this be something your division would consider?

No. The Government requirement does not encompass reworking the existing boards.

44 General Question Can you please let [us know] the last time this CCA was manufactured for the FAA?

Approximately 1993

45 General Question Has the FAA, prior to this solicitation hitting the street, received any prototypes or redesign writeups for this Clutter Map Memory CCA?

No.

46 General Question [AMS Clause] 3.10.4-13 says that formal third party ISO 9001 registration is not required. However, Section L.16 seems to say that it is required. Can you clarify?

The Offeror must provide a current Proof of Quality

Assurance Certificate applicable to ISO 9001.2008 held by the firm that will perform the manufacturing effort. See revised Section L.16 and revised Section E Clause 3.10.4-

13.

47 General Question

Under L.16, is the certificate only required for the parties that will engage in the manufacturing? Since we farm that work out to companies that are ISO 9001 certified, would be be eligible for the contract award?

Reference Government response to Vendor Comment #46

48 General Question

Is the Government requiring certification for only the manufacturing component (during CLIN 0003 and 0004) of the team or is the design/test engineers component of the team required to be certified as well?

Reference Government response to Vendor Comment #46

49 General Question [Would the FAA consider] engaging in a PCB Reverse Engineering process to obtain an exact replica of the existing CCA that will interface with the remaining components of the system?

Reference Government response to Vendor Comment #13

PART I - SECTION C 693KA7-18-R-00010-0004

Statement of Work CMM

FEDERAL AVIATION ADMINISTRATION (FAA)

CLUTTER MAP MEMORY (CMM)

CIRCUIT CARD ASSEMBLY (CCA)

September 20, 2018

1.0 Introduction

1.1 Background

The legacy Clutter Map Memory (CMM) Circuit Card Assembly (CCA) is a custom designed circuit card assembly built to FAA specifications. The CMM CCA is an integral component of the Airport Surveillance Radar – Model 9 (ASR-9) system. The program management office

(PMO) has determined that, to maintain and sustain the operational capability of the system, the

FAA will need to procure additional CMM units. Current spare levels in stock are insufficient to sustain operational readiness. The required quantity for this procurement will help to sustain operational readiness beyond 2021. However, at that time, available spare sources will be depleted as a result of a CMM CCA that was built several decades ago, using parts, designs and technology that are obsolete, are no longer available in the marketplace, or have reached their end-of-life cycle. The design and replacement of failing parts is required to support the continuing operation of the system.

The CMM board is 1 of 10 boards used in the target and two-level weather detector function in the Radar Receiver/Processor Channel A/B (Unit 2/5), reference designation A4A110. The

CMM Board A4A110 and the Clutter Map Control Board A4A112 are used to provide a scan average of the Zero Velocity Filters (ZVF) output (clutter) for the entire scan area, and a scan average of the Non Zero Velocity Filters (NZVF) outputs (residue) for the first 13 range cells.

The CMM board is a storage device for the clutter data of each range/azimuth cell, and transmits data to and from clutter map control A4A112 via the output register and stimulus bus. The input data is stored in 55 128K-bit dynamic RAMs. The memory is divided into five identical banks each with 11 dynamic 64K x 2 RAMs. The output is used to recover valid zero velocity targets and provides scan–to scan storage of ZVF data.

1.2 Purpose

This Statement of Work (SOW) delineates the Contractor's work required to bring the CMM

CCA, a component of the ASR-9 which forms a part of the FAA's National Airspace System, to a producible configuration.

1.3 Scope

This SOW defines the requirement to develop a CMM CCA design to a producible configuration. The anticipated acquisition is for the CMM board (CCA) designation number

A4A110 only.

The Contractor must design a Form-Fit-Function (FFF) equivalent CMM CCA based on information included herein and in Section J. These items must be manufactured, assembled, and tested to meet the requirements specified in the documentation and attachments provided as part of the contract.

The Contractor must provide all required labor, facilities, tools, equipment, fixtures, parts, supplies, materials, appropriate technical data/expertise, transportation, preservation, packaging, packing and marking required to furnish the items specified in Part I – Section B in accordance with (IAW) the terms, conditions, and provisions set forth herein.

Each FFF term defines a specific aspect of the requirement for a CMM CCA that conforms to Government requirements, as follows:

1. Form refers to such characteristics as external dimensions – weight, size, and visual appearance of a part or assembly. This is the element of “form” that is most affected by design choices, including enclosure, chassis, and control panel, that become the outward

"face" of the product.

2. Fit refers to the ability of the part or feature to connect or join to another feature or part within an assembly. The “fit” allows the part to meet the required assembly tolerances.

3. Function is a criterion that is met when the part meets performance and operational requirements as defined by this SIR. In an electronics product, for example, function can depend on the solid-state components used, software or firmware, and quite often on the features of the electronics enclosure selected.

International Traffic in Arms Regulation (ITAR) compliance is not required for CMM.

2.0 Applicable Documents

The following specifications, handbooks, orders, standards, and drawings form a part of this

SOW and are applicable to the extent specified herein. The latest version of these documents as of the contract date must apply. In the event of conflict between this SOW and any of the applicable documents cited below, the provisions of this SOW must apply. They are listed in the table below, cross-referenced to the applicable FFF requirement:

List of Applicable Documents Form Fit Function

1. Clutter Memory CCA (1D21061G01_2A4A110) Control

Signals. pdf

X

2. Clutter Memory CCA (1D21061G01_2A4A110)

Engineering Drawings.pdf

X X

List of Applicable Documents Form Fit Function

3. Clutter Memory CCA (1D21061G01_2A4A110) Depot

Pages and Schematic. pdf

X X X

4. TI 6310.38 – FIGURE 11-163 64Kx2-Bit DRAM Data

Sheet

X

5. FAA-G-2100H – Electronic Equipment, General

Requirements, Applicable sections:

3.2.2.1 (to include subsections) Printed Circuit Boards

3.3.1.4.7 Conformal Coating of Printed Circuit Boards

3.3.1.4.8 Electromagnetic Shielding

X X X

Offerors are hereby advised that the attachments identified in the table above are intended for informational purposes only as an aid in the development and delivery of requirement documents as specified below. They are not to be construed as CMM CCA design or manufacturing specifications.

3.0 Limited Production and Deployment Requirements

3.1 Critical Design Review (CLIN 0001) FFP

Prior to commencement of prototype development and production, the Contractor will conduct a

Critical Design Review (CDR) to allow the FAA’s review of the Contractor’s design of the

CMM CCA. The review must be conducted no later than 90 days after contract award.

The Contractor must support a CDR to take place at AJW-146 / ASR-9 RADAR Building 270, William J. Hughes Technical Center (WJHTC), Atlantic City, New Jersey 08405. The

Contractor will ensure that personnel critical to supporting the CDR are in attendance or are available by teleconference.

At the CDR, the Contractor must:

1. Describe the products, processes, methodologies, milestones, and measurements to be used in conducting development activities;

2. Present data flow and control flow diagrams describing design solutions;

3. Present design decisions defined and recorded for the CMM CCA; and

4. Document minutes, action items, and provide presentation materials.

As part of the CDR, the Contractor must present the following documents to the Government:

1. Detailed design approach, including interfaces;

2. Functional flow and schematic diagrams;

3. Physical description including lists of materials, parts, manufacturing flow processes, and board layout;

4. Producibility analysis;

5. Identification of design-driving/cost driving developmental elements;

6. Component level reliability and maintainability predictions;

7. Design concerns such as environmental control, electromagnetic compatibility/interoperability and derived design requirements; and

All CDR deliverables under CLIN 0001 may be submitted using a contractor’s format. CDR deliverables must be provided to the Government at least ten (10) days prior to the CDR. The

Government requires schematic and PCB layouts to be furnished in Altium.

3.2 CDR Acceptance Criteria

To successfully complete CDR, the Contractor must present evidence of meeting the following requirements:

1. Present a detailed design that shows a FFF equivalent CMM CCA in accordance with the seven documents listed in Section 3.1 that are presented at CDR (e.g., detailed functional analysis, functional flow and schematic diagrams, etc.);;

2. Present sufficient data, analysis and detail to show that requirements of the SOW will be met; and

3. Provide resolution, or an acceptable plan for resolution, of all action items.

The Contractor is required to successfully complete CDR Acceptance Criteria no later than 30 days after completion of CDR.

Non-Recurring Engineering (NRE) as well as all costs associated with the activities identified above must be accounted for as part of this CLIN.

4.0 Prototype Units (CLIN 0002) (FFP)

The Contractor must design, build, test and deliver two (2) Prototype CMM CCA units. The purpose of the prototype units is to successfully demonstrate the Contractor’s proof of concept design. Prototype production must not commence prior to FAA approval of the design. (CLIN

0001).

Deliverables under this CLIN must include:

1. Prototype units (hardware and software);

2. Development Test Plan and Procedures;

3. Development Test Reports;

4. Bill of Materials (BOM);

5. List of test tools (hardware and software) used to support CMM CCA development and testing;

6. Manufacturing specifications;

7. Schematics, Printed Circuit Board (PCB) layout design in Altium, JDEC (if applicable) and output files (e.g., Gerber; and

8. Programmable logic source code (if applicable).

Contractor format is acceptable.

For all data deliverables listed above the Contractor must provide the following:

1. BOM in MS excel format.

2. Schematics and PCB design file in Altium Designer format.

3. All mechanical drawings in Adobe pdf and AutoCAD drawing format.

4. All other documents in Adobe pdf and MS word format.

The Contractor must provide a Development Test Plan and Procedures to the FAA within 30 days of FAA approval of the design. (CLIN 0001). The objective of Development Test Plan and

Procedures is for the Contractor to prove that the CMM CCA meets all specifications and FFF requirements. The Government will review the Development Test Plan and Procedures within 30 days after receipt.

All other deliverables under CLIN 0002 are due to the FAA within 120 days of FAA approval of the design. (CLIN 0001)

The Development Test Plan and Procedures must:

1. Include a separate test plan and procedures for each test to be conducted by the

Contractor;

2. Cover all tests required for the conduct of all tests identified in the Development Test

Plan;

3. Be separately identified;

4. Meet those performance parameters and operating characteristics of the design criteria;

5. Include detailed planning information for test conduct. Information must be to a level necessary to show adequacy of the test methods and test limits. Specific methods for performance measurement must be included:

a) Form/Fit: mechanical compliance of all card dimensions, extractors, and Input/

Output (I/O) connector placement;

b) Function: memory read/write for all addresses;

c) Environmental: functional test in environmental chamber based on the following environmental conditions:

o Temperature: -40C to 85C o Relative Humidity: 5% to 90% o Elevation: 0 to 10,000 feet above sea level ; and

d) Timing Analysis: Memory read/write setup and hold verification.

Note that the format of the Development Test Plan and Procedures must be specified by the

Contractor. All test equipment (hardware and software) must be certified and validated prior to test. The Government reserves the right to witness any and all Development Testing activity conducted by the contractor at the contractor’s facility or FAA facility. While the contractor can perform the majority of development testing at contractor’s facility, the contractor may also elect to conduct any relevant testing at the FAA WJHTC, Building 270, Atlantic City, New Jersey utilizing Government’s ASR-9 system.

The Development Test Report must:

1. Document Development Test results. The reports are used to identify and evaluate discrepancies between expected and actual test results.

2. Address each test identified in the Development Test Plan and Procedures.

3. Address each test and associated test result separately and be identifiable.

4. Be in a contractor-specified format.

The Government will review the Development Test Report within 30 days after receipt.

4.1 Prototype Integration Testing

The FAA will perform functional testing on the delivered CMM CCAs to confirm functionality of the units. Any issues with the functional testing will be submitted in writing to the Contractor, who must provide resolution, subject to Government approval, of all identified issues no later than 30 days from receipt of Government comments. Prototype Integration Testing will be performed by the FAA at the WJHTC, Building 270, Atlantic City, New Jersey. The FAA will work jointly with the Contractor to integrate the CMM CCAs into the ASR-9 Radar System. The Contractor may be onsite at the WJHTC and assist in any special instructions or handling of the prototypes as well as witness the test in process, take notes, and if necessary, assist in troubleshooting, take measurements, or change firmware/software if any concerns identified.

4.2 Prototype Unit Acceptance Criteria

To successfully complete Prototype Unit Acceptance Criteria, the Contractor must present evidence of meeting the following requirements:

1. Government approval of Prototype Unit deliverables; and

2. Resolution, or an acceptable plan for resolution, of all action items and comments

5.0 Pre-Production Units (CLIN 0003) (FFP)

Upon the successful completion of functional testing of prototype units (CLIN 0002), and at the

FAA’s direction, the Contractor must design, build and deliver two (2) pre-production CMM

CCAs and supply them to FAA (AJW-146) for system testing. The purpose of the pre-production units is to confirm validation of the design as a manufacturing standard.

1. Updated Development Test Plan and Procedures;

2. Pre-Production units (hardware and software);

3. Development Test Reports;

4. Updated BOM;

5. List of test tools (hardware and software) used to support CMM CCA development and testing;

6. Updated manufacturing specifications;

7. Updated schematics, Printed Circuit Board (PCB) layout design using Altium, JDEC (if applicable) and output files (e.g., Gerber);

8. Updated programmable logic source code (if applicable); and

9. Factory Acceptance Test (FAT) Plan and Procedures.

3. All mechanical drawings in Adobe pdf and AutoCAD drawing format.

4. All other documents in Adobe pdf and MS word format.

The Contractor must provide an updated Development Test Plan and Procedures to the FAA within 30 days of FAA approval of the prototype. (CLIN 0002). The objective of Development

Test Plan and Procedures is for the Contractor to prove that the CMM CCA meets all specifications, and all FFF requirements. The Government will review the Development Test

Plan and Procedures within 30 days after receipt.

All other deliverables under CLIN 0003 are due to the FAA within 120 days of FAA approval of the prototype units. (CLIN 0002)

5.1 Factory Acceptance Test Plan and Procedures

The Contractor must develop a Factory Acceptance Test (FAT) Plan and Procedures.

The FAT Plan and Procedures must be reviewed and approved by the FAA prior to its implementation on the first article units (CLIN 0004). The FAT Plan and Procedures must also address the requirements of factory testing and inspection as stated in the quality section.

For each CMM CCA, electrical continuity & isolation PCB must be performed for the blank, unassembled PCBs.

For the final CMM CCA assembly, IPC-A-610B Class 3 compliance inspections and the FAT procedures must be performed. Installation, integrity, and labeling of the components must be physically verified as part of the FAT.

5.2 Pre-Production Integration Testing

The FAA will perform system testing on the delivered CMM CCAs to confirm functionality of the units. Any issues with the system testing must be submitted in writing to the Contractor, who will provide resolution, subject to Government approval, of all identified issues no later than 30 days from receipt of Government comments. Pre-Production Integration Testing will be performed by the FAA at the WJHTC, Building 270, Atlantic City, New Jersey. The FAA will work jointly with the Contractor to integrate the CMM CCAs into the ASR-9 Radar System. The Contractor may be onsite at the WJHTC and assist in any special instructions or handling of the prototypes as well as witness the test in process, take notes, and if necessary, assist in troubleshooting, take measurements, or change firmware/software if any problems are found.

5.3 Pre-Production Unit Acceptance Criteria

To successfully complete Pre-Production Unit Acceptance Criteria, the Contractor must present evidence of meeting the following requirements:

1. Government approval of Pre-Production Unit deliverables; and

2. Resolution, or an acceptable plan for resolution, of all action items and comments.

6.0 First Article Units (CLIN 0004) FFP

Upon the successful completion of pre-production unit testing (CLIN 0003), which must confirm to the FFF of the pre-production units, the Contractor must build and deliver six (6) CMM CCAs

First Article Units and supply them to FAA (AJW-146) for system testing and Government approval.

1. Final Development Test Plan and Procedures;

2. First Article units (hardware and software);

3. Final Development Test Reports;

4. BOM;

5. List of test tools (hardware and software) used to support CMM CCA development and testing;

6. manufacturing specifications;

7. schematics, PCB layout design using Altium, JDEC (if applicable) and output files (e.g., Gerber);

8. l programmable logic source code (if applicable); and

9. Final FAT Plan and Procedures.

3. All mechanical drawings in Adobe pdf and AutoCAD drawing format.

4. All other documents in Adobe pdf and MS word format.

The Contractor must provide an updated Development Test Plan and Procedures to the FAA within 30 days of FAA approval of the pre-production unit. (CLIN 0003). The objective of

Development Test Plan and Procedures is for the Contractor to prove that the CMM CCA meets all specifications, and all FFF requirements. The Government will review the Development Test

Plan and Procedures within 30 days after receipt.

All other deliverables under CLIN 0004 are due to the FAA within 90 days of FAA approval of the pre-production units. (CLIN 0003)

6.1 First Article Test

The FAA will perform First Article testing on the delivered CMM CCAs to confirm functionality of the units.

First Article Test will include:

1. Functional Configuration Audit (FCA) and Physical Configuration Audit (PCA)

2. Operational Functional Testing

3. Burn-In or Reliability Testing

4. Execute regression and compatibility testing (i.e., one CMM or two CMMs in system)

The FAA has 60 days to perform First Article Testing after receiving the First Article CMM

CCAs. If First Article Testing is successful, the FAA will write a Release for Production document at which time the Contractor may begin production. There may be conditional acceptance or approval.

6.2 First Article Unit Acceptance Criteria

Once the FAA has verified that the first articles have passed a PCA as well as installation and system tests, a written approval will be issued to the Contractor by the Contracting Officer (CO)

IAW AMS Clause 3.10.9-2 First Article Approval – Government Testing (July 2003) and AMS

Clause 3.10.4-2 Inspection of Supplies, Fixed Price (November 1997). The Contractor must provide resolution, or an acceptable plan for resolution, of all comments no later than 30 days from receipt of Government comments. Upon Contractor delivery of the First Article units the

Government will inform the Contractor of its determination no later than 30 days from receipt.

7.0 Production Units (CLIN 0005) FFP

Upon acceptance of First Article units, and upon direction by the FAA, the Contractor must commence production of the thirty (30) CMM CCA units. The Contractor must manufacture and test the required contract quantity of CMM CCAs utilizing the Government-approved First Article as the production quantity standard along with the FAA-approved specification, drawings and other defining documentation.

The Contractor must test each completed CMM IAW the approved FAT Plan prior to release for shipment to the FAA.

Deliverables include:

1. Final BOM;

2. Final manufacturing specifications;

3. Final schematics, PCB layout design (e.g., Altium Designer format), JDEC (if applicable) and output files (e.g., Gerber);

4. Final programmable logic source code (if applicable); and

5. Final FAT data sheets and report. The Contractor must include a FAT data sheet for each

CMM CCA delivered. The FAT data sheet should include the serial number of each

CCA, quality conformance inspection results, and the result of the FAT verification.

2. Schematics and PCB design file in Altium Designer format.

3. All mechanical drawings in Adobe pdf and AutoCAD drawing format.

4. All other documents in Adobe pdf and MS word format.

Under CLIN 0005, the Government requires 10 units per month (based on a total of 30 CMM

CCA units) with delivery commencing 90 days after Government acceptance of First Article units.

8.0 Material Procurement and Fabrication

1. Upon receipt of first article approval, the Contractor must procure the materials required to manufacture the remaining production contract quantity of CMM CCAs.

2. The Contractor should use caution and not deviate from the materials or manufacturers used in the first article unless such deviation has been previously approved by the CO.

3. The Contractor must include a FAT data sheet for each CMM CCA delivered. The FAT data sheet must include the serial number of each CCA, quality conformance inspection results, and the result of the FAT verification.

9.0 Test Equipment (CLIN 0006) (FFP)

The Contractor must provide any test tools developed with the test procedures and custom software and/or hardware for board level testing and troubleshooting. Custom hardware may include prototype CCAs that may contain standalone circuitry or partially integrated circuitry as well as interfaces to interface or communicate with the prototype circuitry and/or diagnostic test equipment. This would include all test tools used from development to prototype/pre-production.

Offerors must propose test equipment as fully integrated. Test tools must be delivered at First

Article and an updated set of deliverables provided with the production units. This would also include any updates made after First Article.

10.0 Optional Production Units (CLIN 0007) FFP

The Government reserves the right to purchase additional production units as required during the term of this contract, and may exercise this option within ten (10) days from the date of delivery of the final production unit.

11.0 Data Rights

The Contractor must provide the Government with rights to all data, drawings and specifications associated with CMM CCA as defined in AMS Clause 3.5-13 Rights in Data-General (October

2014).

12.0 Government Furnished Equipment

The Government will furnish the Contractor, as Government Furnished Property, a legacy CMM

CCA to support design and development within 15 days after contract award. The legacy CMM

CCA must be returned to the Government when directed by the FAA or upon Contractor delivery and Government acceptance of production units.

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PART I - SECTION E 693KA7-18-R-00010-0004

Inspection and Acceptance CMM

E.1 CLAUSES AND PROVISIONS INCORPORATED BY REFERENCE

3.1-1 Clauses and Provisions Incorporated by Reference (July 2011): This Screening Information Request

(SIR) or contract, as applicable, incorporates by reference the provisions or clauses listed below with the same force and effect as if they were given in full text. Upon request, the CO will make the full text available or Offerors and contractors may also obtain the full text via the Internet at: http://conwrite.faa.gov

(on this webpage, select “Search and View Clauses”, then “Download All Clauses”).

FAA Acquisition Management System Clauses by Reference:

3.10.4-2 Inspection of Supplies – Fixed Price (November 1997)

3.10.4-4 Inspection of Supplies – Both Firm Fixed Price and Cost Reimbursement (April 1996)

3.10.4-14 Assignment of a Quality Reliability Officer (QRO) (October 2015)

3.10.4-15 Certificate of Conformance (April 1996)

3.10.4-16 Responsibility for Supplies (April 1996)

E.2 INSPECTION AND ACCEPTANCE

(a) The Government reserves the right to have its authorized representative inspect the material at the Contractor's plant prior to shipment. To facilitate such inspection, the Contractor must give the CO a written notice at least 15 working days prior to readiness for inspection. Such notice must include FAA delivery order number, FAA contract number, and date of proposed inspection. The Contractor must indicate in the following space the location of the plant where the material will be available for inspection.

Plant

Location

Address

(b) Final Government inspection and acceptance is at the Destination point, as defined by the

Government.

(c) In the event First Article/Production units are determined to be nonconforming, the Government must return said units to the Contractor for repair/replacement at the Contractor’s expense.

The provisions of this clause must in no way be construed to limit the rights of the Government under the clause entitled “Inspection of Supplies—Fixed-Price” (AMS 3.10.4-2.)

(d) The offeror’s inspection system must ensure conformance to the specifications, drawings, and other applicable documents. Inspection must include general mechanical tests, visual inspection, and physical examinations as necessary to demonstrate that deliverables are free of defects and meet physical requirements. The Offeror must maintain records of inspection results.

E.3 FAA Acquisition Management System Full Clauses and Provisions

3.10.4-13 Higher-Level Contract Quality Requirement (October 2015)

(a) The Contractor must comply with the standard titled ISO 9001:2008, Quality management systems –

Requirements , which is hereby incorporated into this contract.

(b) The Contractor must establish and maintain a Quality System in accordance with the above referenced standard(s) and the contractor's Quality System Plan (QSP). This QSP is hereby incorporated into this contract when approved by the CO. If the QSP is submitted as part of a response to a Screening

Information Request (SIR) submission and approved before award, then the QSP is hereby incorporated into this contract at time of award. The QSP must describe the Contractor's provisions for quality assurance, inspection and test of all supplies to be provided under this contract, in accordance with the terms of this contract, including but not limited to the contract specifications and the above referenced standard.

(c) In the event of conflict between the Quality System Plan (QSP) and the above referenced standard(s), the applicable standards must control.

(d) Calibration systems and measuring and test equipment must be controlled in accordance with a nationally recognized standard, such as ISO 10012.

(e) Government Furnished Property must be controlled to assure acceptability upon receipt, preclude degradation, damage or misuse during storage, use or test, and assure proper final disposition in accordance with the contract.

(f) Site installation activities, maintenance, and support services must be controlled in accordance with contract requirements.

(End of Clause)

E.4 Quality

Overall quality of the CMM CCA must be commensurate with industry-accepted standards for commercial quality products.

The following are examples, not all-inclusive:

1. Wire crimps to cabling/wire assemblies are gas tight; calibrated and certified crimp tools only.

2. All flux removed from any solder work.

3. Component leads are neatly trimmed.

4. Any screws, nuts appropriately torqued.

5. Final product free from dirt, chemicals, scratches, etc.

6. Strain reliefs on cables act as strain reliefs.

7. Components assembled neatly on baseboards, parts numbers visible when possible.

8. Serial numbers must be inscribed onto the CMM circuit card with indelible ink or permanent labels in the appropriate place: (S/N 2001 is starting number in this manufacturing sequence)

STARTING WITH: MONTH-YEAR-2001

EXAMPLE FOR JANUARY 2011 01-11-2001

9. PC bare board fabrication must comply with IPC (Institute for Interconnecting and

Packaging Electronic Circuits) standard IPC-A-600J class “3”.

The baseboards must be FR4, specification IPC-4101B/26, Tg=170C), 0.0625” +.014” / -.000”, one (1) ounce copper, manufactured solder mask over bare copper. The baseboards must be manufactured and tested to insure no opens or shorts in the deliverables.

The PC board assemblies must be soldered in accordance with J-STD-001F (class 3) and visually inspected to insure no opens or shorts in the deliverables. PC board assembly must comply with IPC standard IPC-A-610F Class 3, and IPC-A-600. This certification applies to the Offeror, as well as, subcontractors at any tier (LACW IPC-A -610 Class 3, and LACW IPC-A-600).

Any CMM assembly or system component which does not meet these qualifications may be rejected.

In addition to the requirements contained in FAA AMS Clause 3.10.4-13 (ISO 9001-2008), for production and manufacturing the Contractor must also provide certification as evidence of IPC-

A-610 Class 3 compliance. ISO 9001-2008 certifications must be applicable to NAICS Code

3344…