SOW.doc

STATEMENT OF WORK

FOR THE AVIONICS MECHANICAL ASSEMBLIES

1. SCOPE

Introduction Naval Air Warfare Center Weapons Division (NAWCWD) Point Mugu Code 486M00E intends to procure the Avionics Mechanical Assemblies. The Avionics Mechanical Assemblies house all of the Electronic Assemblies and the Cable Assemblies to make complete test sets. These test sets are used to test Avionics. NAWCWD Code 486M00E has a requirement to fabricate the following Avionics Mechanical Assemblies for the customers. Listed in paragraph 2.1 are the applicable drawings for the Avionics Mechanical Assemblies:

Three (3) Sets of Avionics Mechanical Assemblies (Drawing 3156193-10 Configuration)

Four (4) Sets of Avionics Mechanical Assemblies (Drawing 3156193-4 Configuration)

2. APPLICABLE DOCUMENTS

2.1 Drawings

2.1.1 Avionics Mechanical Assemblies consist of the following drawings (available on CD):

2289616 Rev. -, Transit Case Assembly, RIA/PIA

2902331 Rev. Y, Decal Safety Hazards

2959106 Rev. C, Gasket, Connector

2964480 Rev. F, Stiffener, Horizontal

2964481 Rev. G, Stiffener, Vertical

2964482 Rev. H, Spring, Flat

2964483 Rev. H, Ejector

2964524 Rev. F, Card Retainer, Wedge Lock

3100828 Rev. R, Circuit Card Assembly, 286 CPU (A5) (Prod)

3100848 Rev. B, Heat Sink

3116053 Rev. D, Adhesive, Heat Sink

3116054 Rev. B, Insulator, Thermally Conductive

3156152 Rev. D, Cable Assembly, Tether

3156170 Rev. J, Family Tree, Guided Missile – Launcher Test Set AN/GSM-396

3156175 Rev. F, Circuit Card Assembly, Critical Signals/Power Control (1A2A1)

3156180 Rev. N, Circuit Card Assembly, Analog I/O (1A2A2, 1A2A3)

3156185 Rev. R, Circuit Card Assembly, HARM Communication (1A2A4)

3156189 Rev. K, Circuit Card Assembly, GMLTS Motherboard (1A2A7)

3156193 Rev. D, Test Set, Guided Missile-Launcher, AN/GSM-396

3156194 Rev. H, Adapter Unit Assy, Interface 3156195 Rev. M, Panel Assembly, IAU

3156214 Rev. L, Panel, Interface

3156215 Rev. E, Wall, CCA Chassis

3156216 Rev. F, Gasket, Enclosure

3156217 Rev. B, Panel, CCA Chassis

3156218 Rev. C, Leg, Support

3156219 Rev. B, Cover, CCA Chassis

3156220 Rev. C, Gasket, Connector

3156221 Rev. E, Support, Harness

3156233 Rev. M, Transit Case Assembly, Computer

3156234 Rev. K, Case, Transit

3156235 Rev. G, Interface Assembly, Reprogramming (RIA)

3156239 Rev. J, Saver, Connector Circular

3156244 Rev. B, Decal, Interface Panel

3156248 Rev. K, Circuit Card Assembly, Smart Card

3156255 Rev. F, Enclosure, Lower

3156256 Rev. G, Enclosure, Upper

3156266 Rev. D, Cover, Enclosure

3156267 Rev. B, Housing, Enclosure

3156268 Rev. D, Hinge, Computer Tray

3156269 Rev. E, Tray, Computer

3156270 Rev. C, Hinge, Arm

3156271 Rev. E, Arm, Computer Tray

3156272 Rev. G, Identification Plate, Guided Missile-Launcher Test Set 3156273 Rev. C, Decal, Interface Panel

3156275 Rev. F, Contact, Connector

3156287 Rev. D, Connector Assembly (J2)

3156288 Rev. C, Adapter, Connector

3156289 Rev. E, Clip

3156305 Rev. B, Cable, Retaining

3156307 Rev. B, Spacer, Connector

3156310 Rev. D, Cap, Protective

3156312 Rev. D, Gasket, Bulkhead Connector

3156313 Rev. H, Decal Inventory 3156316 Rev. C, Nut, Receptacle

3156317 Rev. C, Guard, Connector

3156324 Rev. J, Housing Assembly, RF Source 3156325 Rev. D, Transit Case Assembly, RF/ATR 3156331 Rev. D, Housing, Modified, RF Source

3156332 Rev. E, Shield, Dunnage, RF

3156333 Rev. B, Support, RF Component

3156336 Rev. E, Bracket, Support, RF

3156337 Rev. F, Support, Circuit Card Assembly

3156340 Rev. F, Bracket Assembly, RF

3156341 Rev. C, Dunnage Assy, Shield RF

3156342 Rev. B, Screw, Captive, Modified

3156344 Rev. D, Guard Corner

3156345 Rev. C, Block, Bungee, RF

3156347 Rev. G, Circuit Card Assembly – ATR (1A2A6)

3156389 Rev. A, Decal, RIA, Caution

3156392 Rev. E, Shield, RF

3156393 Rev. D, Plate, Reflection

3156394 Rev. D, Plate, Holding, RF

3156395 Rev. E, Hinge

3156396 Rev. F, Holding Assembly, RF

803786 Rev. D, Washer, Spring Curved

704AS3916 Rev. -, Plate Identification Serial Number

704AS12153 Rev. -, Guard, Switch

1164AS452 Rev. D, Captive Fastener

3. REQUIREMENTS

The Contractor shall manufacture, package and deliver all Avionics Mechanical Assemblies as listed below in accordance with the drawings listed in paragraph 2.1.

A. Three (3) sets of Avionics Mechanical Assemblies (Drawing 3156193-10 Configuration). Each set consists of the following items with the quantity per set as listed below:

1. One (1) Interface Adapter Unit Assembly (Drawing 3156194-5) except Find Numbers 6, 19, 20. IAU Panel Assembly (Drawing 3156195-1), the contractor is not responsible to provide Find Numbers 16, 17, 18, 19, 20, 21, 22, 33, 34, 35, 83.

2. One (1) Computer Transit Case Assembly (Drawing 3156233-8) except Find Numbers 4, 8, 9, 11, 20, 21, 24, 25, 26, 34, 35, 36, 38.

3. One (1) RF/ATR Transit Case Assembly (Drawing 3156325-1) except Find Numbers 6, 7, 16. RF Source Assembly 3156324-2 shall be used instead of 3156324-1. In RF Source Assembly (Drawing 3156324-2), the contractor is not responsible to provide Find Numbers 9, 25. In RF Bracket Assembly (Drawing 3156340-1), the contractor is not responsible to provide Find Numbers 2, 3, 4, 5, 6, 7, 9, 10, 18, 19, 20. In Reprogramming Interface Assembly (Drawing 3156235-1), the contractor is not responsible to provide Find Numbers 3, 28.

4. Five (5) Spring, Flat (Drawing 2964482-1)*.

5. Ten (10) Card Retainer, Wedge Lock (Drawing 2964524-1)*.

6. Ten (10) Ejector (Drawing 2964483-1)*.

7. Five (5) Stiffener, Vertical (Drawing 2964481-1)*.

8. Five (5) Stiffener, Horizontal (Drawing 2964480-1)*.

9. One (1) Heat Sink (Drawing 3100848-1).

10. One (1) Insulator (Thermal) (Drawing 3116054-1).

* The contractor is responsible to install the above items 4, 5, 6, 7 and 8 onto the Government supplied Circuit Card Assemblies.

B. Four (4) sets of Avionics Mechanical Assembly (Drawing 3156193-4 Configuration). Each set consists of the following items with the quantity per set as listed below:

1. One (1) Interface Adapter Unit Assembly (Drawing 3156194-4) except Find Numbers 3, 6, 8. IAU Panel Assembly (Drawing 3156195-2), the contractor is not responsible to provide Find Numbers 16, 17, 18, 19, 20, 21, 22, 33, 34, 35, 83, 95.

2. One (1) Computer Transit Case Assembly (Drawing 3156233-4) except Find Numbers 2, 4, 8, 9, 11, 12, 16, 20, 21, 22, 23, 24, 25, 26, 28, 29, 30.

3. One (1) RF/ATR Transit Case Assembly (Drawing 3156325-2) except Find Numbers 6, 7, 8, 9, 10, 16. RF Source Assembly 3156324-2 shall be used instead of 3156324-1. In RF Source Assembly (Drawing 3156324-2), the contractor is not responsible to provide Find Numbers 9, 25. In RF Bracket Assembly (Drawing 3156340-1), the contractor is not responsible to provide Find Numbers 2, 3, 4, 5, 6, 7, 9, 10, 18, 19, 20. In Reprogramming Interface Assembly (Drawing 3156235-1), the contractor is not responsible to provide Find Numbers 3, 28.

4. Six (6) Spring, Flat (Drawing 2964482-1) **.

5. Twelve (12) Card Retainer, Wedge Lock (Drawing 2964524-1) **.

6. Twelve (12) Ejector (Drawing 2964483-1) **.

7. Six (6) Stiffener, Vertical (Drawing 2964481-1) **.

8. Six (6) Stiffener, Horizontal (Drawing 2964480-1) **.

9. One (1) Heat Sink (Drawing 3100848-1).

10. One (1) Insulator (Thermal) (Drawing 3116054-1).

** The contractor is responsible to install the above items 4, 5, 6, 7 and 8 onto the Government supplied Circuit Card Assemblies

3.1 Items must meet all drawing dimensions, tolerances, specifications requirements and performance requirements in this Section. The Government shall perform the First Article Acceptance Test (FAAT) on the first set of each Configuration of the Avionics Mechanical Assemblies delivered by the Contractor unless the Contractor had previously manufactured these items and the Government had accepted the deliveries from the Contractor. The Contractor shall not continue with the production quantity until the Government grants the FAAT approval. Form, fit and function shall be conducted during FAAT to ensure total compliance with the drawing requirements and SOW requirements.

The contractor’s risk mitigation plan shall be addressed in the proposal and shall be enforced by the contractor upon early detection of risk occurring and shall be mitigated by the contractor to avoid negative impact on delivery schedules. On time delivery of the Avionics Mechanical Assemblies is an absolute requirement. Late delivery shall not be accepted. Quality assurance processes and methods on completed Avionics Mechanical Assemblies are the sole and full responsibilities of the contractor.

Periodic Task Review Meetings to review status of deliverables, progress, quality assurance checks and inspect shall be conducted by NAWCWD Point Mugu representatives at the Contractor’s Facility on a mutually agreed upon meeting schedule.

3.2 Task 1: First Article Unit for Avionics Mechanical Assemblies 3156193-10 Configuration The Contractor shall manufacture and deliver one (1) set of Avionics Mechanical Assemblies IAW paragraph 2 four months after award of contract. The Government shall perform form, fit and functional check at a Government facility to ensure mechanical assemblies were built correctly and met all drawing requirements. Contractor participation is not required. Discrepancies shall be documented and provided to the Contractor for corrective actions.

3.3 Task 2: Deliverable Units for Avionics Mechanical Assemblies 3156193-10 Configuration Upon successful completion of FAAT, the Government shall notify the Contractor to proceed with the manufacture and delivery of the remaining sets. Each remaining set shall be delivered thirty days apart following the initial acceptance of the First Article Unit. The acceptance inspections of the remaining sets shall be done at NAWCWD Point Mugu. Contractor participation is not required. Discrepancies shall be documented and provided to the Contractor for corrective actions.

3.4 Task 3: First Article Unit for Avionics Mechanical Assemblies 3156193-4 Configuration The Contractor shall manufacture and deliver one (1) set of Avionics Mechanical Assemblies IAW paragraph 2 four months after award of contract. The Government shall perform form, fit and functional check at a Government facility to ensure mechanical assemblies were built correctly and met all drawing requirements. Contractor participation is not required. Discrepancies shall be documented and provided to the Contractor for corrective actions.

3.5 Task 4: Deliverable Units for Avionics Mechanical Assemblies 3156193-4 Configuration Upon successful completion of FAAT, the Government shall notify the Contractor to proceed with the manufacture and delivery of the remaining sets. Each remaining set shall be delivered thirty days apart following the initial acceptance of the First Article Unit. The acceptance inspections of the remaining sets shall be done at NAWCWD Point Mugu. Contractor participation is not required. Discrepancies shall be documented and provided to the Contractor for corrective actions.

3.6 Task 5: Options for Deliverable Units for Avionics Mechanical Assemblies 3156193-10 Configuration Within 30 days prior to delivery of the last unit of this configuration, the Government may exercise the option by written notice to the contractor. The options call for one to ten Avionics Mechanical Assemblies (Drawing 3156193-10 Configuration). Delivery of the added items shall continue at the same rate as the items called for under Task 2 of this SOW.

3.7 Task 6: Options for Deliverable Units for Avionics Mechanical Assemblies 3156193-4 Configuration

Within 30 days prior to delivery of the last unit of this configuration, the Government may exercise the option by written notice to the contractor. The options call for one to ten Avionics Mechanical Assemblies (Drawing 3156193-4 Configuration). Delivery of these items shall be at the same rate as the items called for under Task 4 of this SOW.

3.8 The contractor shall ensure adequate consideration of packaging, handling, storage, and transportation (PHS&T) requirements for all deliverable items in accordance with industry standards.

4. DATA REQUIREMENTS

The Contractor shall provide a Quality Assurance Certification with the delivery of each unit to certify that quality control and inspection have been performed to ensure the proper materials were used and the parts made are in full compliance with the drawing requirements. CDRL A001

5. ***GOVERNMENT TECHNICAL REPRESENTATIVE

Commander, NAWCWD

Code XXXXXXX, Bldg. XXX

Point Mugu, CA. 93042

Attn: XXXXX

Tel #: XXX-XXX-XXXX

Fax #: XXX-XXX-XXXX

Email Address:

6. DELIVERY INSTRUCTION

6.1 ***The First Article Unit shall be shipped to the following address for First Article Acceptance Test to be performed by the Government:

Commander, NAWCWD

Code XXXXX, Bldg. XXX

Point Mugu, CA. 93042

Attn: XXXXX 6.2 The deliverable units shall be shipped to the same address listed in paragraph 6.1

To be completed at contract award.

CONTRACT DATA REQUIREMENTS LIST

(1 Data Item) Form Approved

Public reporting burden for this collection of information is estimated to average 110 hours per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA. 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188), Washington, DC 20503. Please DO NOT RETURN your form to either of these addresses. Send completed form to the Government Issuing Contracting Officer for Contract/PR No. listed in Block E.

Avionics Mechanical Assemblies

DISTRIBUTION

SEE BLK 16

b. COPIES

8. APP CODE

SUBMISSION

N/A

Block 4: Contractor format is acceptable as long as DID is used for guidance.

Block 9: Use Distribution Statement E: Distribution Statement E. Distribution authorized to DoD components only, Administrative or Operational Use, 1 September 2016, Other requests for this document shall be referred to NAWCWD Point Mugu, Code 486M00E.

Blocks 10, 12 & 13: Shall be delivered concurrent with hardware.

Block 14: Submit in an electronic format agreed upon by both Government and Contractor prior to 1st submittal.

See Contract Clause 5252.247-9505, Technical Data and Information for distribution address.

15. TOTAL

Naval Air Warfare Center, Weapons Division Point Mugu, CA 93042

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