Statement_of_Work.doc
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- ALIC Chasis Federal contract opportunity
- Solicitation number
- N6893617T0007
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Statement of Work
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STATEMENT OF WORK
FOR THE
AIRCRAFT LAUNCHER INTERFACE COMPUTER (ALIC)
CHASSIS AND MECHANICAL ASSEMBLIES
15 August 2016
1. SCOPE
Naval Air Warfare Center Weapons Division (NAWCWD) Point Mugu Code 486M00E intends to procure the Aircraft Launcher Interface Computer (ALIC) Chassis and the mechanical assemblies. The ALIC Chassis houses all of the Electronic Assemblies, Power Supply and the Wiring Harness. The ALIC is an avionics assembly which provides a functional interface between the F-16C/D Block 40/50/52 aircraft and the AGM-88 HARM Missile. The ALIC is attached to the aft end of the LAU-118(V) 4/A launcher. The ALIC provides the necessary power and control interface for the AGM-88B/C/F Missile. NAWCWD Code 486M00E has a requirement to fabricate ALIC’s for the customer. Listed in paragraph 2.1 are the applicable drawings for the ALIC Chassis and the mechanical assemblies.
2. APPLICABLE DOCUMENTS
2.1 Drawings
ALIC Chassis and the Mechanical Subassemblies consist of the following drawings (available on CD):
2959150-4 Rev. M Aircraft Launcher Interface Computer 2959140-4 Rev. AD Aircraft Launcher Interface Computer (ALIC) Assembly
2959055-1 Rev. N Chassis, Aircraft Launcher Interface Computer (Machined) 2959054-1 Rev. M Chassis, Aircraft Launcher Interface Computer (Casting)
2959111-1 Rev. F Gasket, Strip
2959118-1 Rev. G Cover Assembly, Pylon 2959119-1 Rev. J Cover, Pylon
2959113-1 Rev. K Cover Assembly, Motherboard (A9)
2959114-1 Rev. H Cover, Motherboard
2959115-1 Rev. E Bracket, Motherboard, Cover
2959120-1 Rev. L Cover Assembly, Relay 2959121-1 Rev. K Cover, Relay
2959109-1 Rev. F Cover Assembly, Daughterboard 2959110-1 Rev. G Cover, Daughterboard 2993004-1 Rev. G Adapter, Ejector, AFT 2993003-1 Rev. G Adapter, Ejector, FWD
2959107-1 Rev. C Nutplate, Time Meter
2993012-1 Rev. G Insert, Forward Bulkhead
2959034-1 Rev. D Pin, Guide 2981788-1 Rev. C Gasket, Bulkhead Connector
2981790-1 Rev. D Gasket, ETM
2981791-1 Rev. C Gasket, Pylon Connector
2959148-1 Rev. B Plate, Warranty
2959149-1 Rev. D Plate, Identification
2959131-1 Rev. B Nut Plate, Relay Bracket 2959064-1 Rev. E Bracket, Relay, Side
2959130-1 Rev. E Bracket, Relay, Top
2964482-1 Rev. H Spring, Flat 2964524-1 Rev. F Card Retainer, Wedge Lock
2964483-1 Rev. H Ejector
2964481-1 Rev. G Stiffener, Vertical
2964480-1 Rev. F Stiffener, Horizontal
2981788 Rev. C
Gasket, Bulkhead Connector 2981791 Rev. C
Gasket, Pylon Connector 3038392 Rev. C
Primer, Silicon Rubber
3042154-1 Rev. U Circuit Card Assembly, Relay (A7)
2261693-1 Rev. -
Pad, Rubber
3100828-1 Rev. R Circuit Card Assembly, 286 CPU (A5) (PROD) 3100848-1 Rev. B Heat Sink 3116054-1 Rev. B Insulator, Thermally Conductive
2959070-1 Rev. W Circuit Card Assembly, System I/O (A3)
2959075-1 Rev. N Circuit Card Assembly, Memory (A4)
3042172-1 Rev. J
Circuit Card Assembly, Mux Bus (A2) (PROD)
2959080-1 Rev. AJ Circuit Card Assembly, Video (A1)
2959039-1 Rev. E Label, Temperature Indicating
3. REQUIREMENTS
The Contractor shall manufacture, package and deliver twelve (12) sets of ALIC Chassis and the mechanical assemblies so that twelve (12) complete ALIC units (p/n 2959150) can be assembled together. For each of the drawings listed in the Table I – Procurement Part List, the contractor shall deliver all parts that are called out on the drawings unless they are noted as exception in Table I. The quantity for each of these parts shall be adequate to make twelve (12) complete ALIC units (p/n 2959150). All parts shall be done in accordance with the drawings listed in paragraph 2.1 and also with the requirements listed below:
3.1 Items must meet all drawing dimensions, tolerances, specifications requirements and performance requirements. The Government shall perform the First Article Acceptance Test (FAAT) on the first set of ALIC Chassis and the mechanical assemblies delivered by the Contractor unless the Contractor had previously manufactured them and the Government had accepted the deliveries from the Contractor. The Contractor shall not continue with the next set fabrication until the Government grants the FAAT approval. Form, fit and function shall be conducted during FAAT to ensure total compliance with the drawing 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 ALIC Chassis and the mechanical assemblies is a requirement. Late delivery shall not be accepted. Quality assurance processes and methods on completed ALIC Chassis and the 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 ALIC Chassis and the mechanical assemblies The Contractor shall manufacture and deliver one (1) set of ALIC Chassis and the mechanical assemblies IAW paragraph 2 four months after award of contract. The Government shall perform form, fit and function check at a Government facility to ensure ALIC Chassis and the 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 ALIC Chassis and the mechanical assemblies 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 fifteen days apart following the initial acceptance of the First Article Unit. The acceptance inspections of these 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: Options for Deliverable Units for ALIC Chassis and the mechanical assemblies Within 30 days prior to delivery of the last unit of the ALIC Chassis and the mechanical assemblies, the Government may exercise the option by written notice to the contractor. The options call for one (1) to ten (10) sets of the ALIC Chassis and the mechanical assemblies each year for the next five years.
Delivery of the added items shall continue at the same rate as the items called for under Task 2 of this
SOW.
3.5 The contractor is responsible to install the following parts onto the Government supplied Circuit Card Assemblies that are needed to make 12 sets of ALIC units:
a. 2964482-1 Spring, Flat
b. 2964524-1 Card Retainer, Wedge Lock
c. 2964483-1 Ejector
d. 2964481-1 Stiffener, Vertical
e. 2964480-1 Stiffener, Horizontal
3.6 The contractor shall ensure adequate consideration of packaging, handling, storage, and transportation (PHS&T) requirements for the ALIC Chassis and its mechanical assemblies in accordance with industry standards.
4. DATA REQUIREMENTS
The Contractor shall provide a Quality Assurance Certification with the delivery of each set of the ALIC
Chassis and the mechanical assemblies 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 A00A
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: XXXXX
6. DELIVERY INSTRUCTION
***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
*** To be completed at contract award.
Drawing Number
| Description |
| Remarks |
| 2959150-4 |
| Aircraft Launcher Interface Computer |
| 2959140-4 |
| Aircraft Launcher Interface Computer (ALIC) Assembly |
| Except Item No. 2, 3, 4, 9 |
| 2959055-1 |
| Chassis, Aircraft Launcher Interface Computer (Machined) |
| 2959054-1 |
| Chassis, Aircraft Launcher Interface Computer (Casting) |
| 2959111-1 |
| Gasket, Strip |
| 2959118-1 |
| Cover Assembly, Pylon |
| Except Item No. 2, 3, 4, 5, 8, 9,11, 13, 14 |
| 2959119-1 |
| Cover, Pylon |
| 2959113-1 |
| Cover Assembly, Motherboard (A9) |
| Except Item No. 3 through 31 |
| 2959114-1 |
| Cover, Motherboard |
| 2959115-1 |
| Bracket, Motherboard, Cover |
| 2959120-1 |
| Cover Assembly, Relay |
| 2959121-1 |
| Cover, Relay |
| 2959109-1 |
| Cover Assembly, Daughterboard |
| 2959110-1 |
| Cover, Daughterboard |
| 2993004-1 |
| Adapter, Ejector, AFT |
| 2993003-1 |
| Adapter, Ejector, FWD |
| 2959107-1 |
| Nutplate, Time Meter |
| 2993012-1 |
| Insert, Forward Bulkhead |
| 2959034-1 |
| Pin, Guide |
| 2981788-1 |
| Gasket, Bulkhead Connector |
| 2981790-1 |
| Gasket, ETM |
| 2981791-1 |
| Gasket, Pylon Connector |
| 2959148-1 |
| Plate, Warranty |
| 2959149-1 |
| Plate, Identification |
| 2959131-1 |
| Nut Plate, Relay Bracket |
| 2959064-1 |
| Bracket, Relay, Side |
| 2959130-1 |
| Bracket, Relay, Top |
| 2964482-1 |
| Spring, Flat |
| 2964524-1 |
| Card Retainer, Wedge Lock |
| 2964483-1 |
| Ejector |
| 2964481-1 |
| Stiffener, Vertical |
| 2964480-1 |
| Stiffener, Horizontal |
| 2981788 |
| Gasket, Bulkhead Connector |
| 2981791 |
| Gasket, Pylon Connector |
| 3038392 |
| Primer, Silicon Rubber |
| 3042154-1 |
| Circuit Card Assembly, Relay (A7) |
| Except Item No. 1, 5 through 41 |
| 2261693-1 |
| Pad, Rubber |
| 3100828-1 |
| Circuit Card Assembly, 286 CPU (A5) (PROD) |
| Except Item No. 1, 6 through 39, 52, 59, 60, 61, 62, 63, 64, 65, 66, 67 |
| 3100848-1 |
| Heat Sink |
| 3116054-1 |
| Insulator, Thermally Conductive |
| 2959070-1 |
| Circuit Card Assembly, System I/O (A3) |
| Except Item No. 1, 6 through 51, 60, 61, 64, 65, 68, 69 |
| 2959075-1 |
| Circuit Card Assembly Memory (A4) |
| Except Item No. 1, 6 through 25, 34, 39, 40, 41, 42, 43 |
| 3042172-1 |
| Circuit Card Assembly, Mux Bus (A2) Prod |
| Except Item No. 1, 6 through 32, 41, 48 through 52 |
| 2959080-3 |
| Circuit Card Assembly, Video (A1) |
| Except Item No. 1, 6 through 50, 59, 60, 63, 64, 67, 71, 75, 76, 77 |
| 2959039-1 |
| Label, Temperature Indicating |
Table I - Procurement Part List
CONTRACT DATA REQUIREMENTS LIST
(1 Data Item) Form Approved
OMB No. 0704-0188
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.
| A. CONTRACT LINE ITEM NO. |
| B. EXHIBIT |
| C. CATEGORY: |
| A |
| TDP TM OTHER: MISC |
| D. SYSTEM/ITEM |
| E. CONTRACT/PR NO. |
| F. CONTRACTOR |
ALIC Chassis and mechanical assemblies
| 1. DATA ITEM NO. |
| 2. TITLE OF DATA ITEM |
| 3. SUBTITLE |
| A001 |
| TECHNICAL REPORT – STUDY/SERVICES |
| Quality Assurance Certification |
| 4. AUTHORITY (Data Acquisition Document No.) |
| 5. CONTRACT REFERENCE |
| 6. REQUIRING OFFICE |
| di-misc-80508b |
| SOW Para 4 |
| NAWCWD Code 486M00E |
| 7. DD 250 REQ |
| 9.DIST STATEMENT REQUIRED |
| 10. FREQUENCY |
| 12. DATE OF FIRST SUBMISSION |
| 14. |
DISTRIBUTION
| LT |
| SEE BLK |
| ASREQ |
| SEE BLK 16 |
b. COPIES
| 8. APP CODE |
| 16 |
| 11. AS OF DATE |
| 13. DATE OF SUBSEQUENT |
SUBMISSION
| a. ADDRESSEE |
| Draft |
| Final |
N/A
| N/A |
| SEE BLK 16 |
| Reg |
| Repro |
Block 16 Remarks
Block 4: May be in Contractor format as long as DID is used for guidance.
Block 9: Distribution Statement F. Further dissemination only as directed by NAWCWD Point Mugu, Code 486M00E or higher DoD Authority.
Blocks 12 & 13: Shall be delivered concurrent with hardware.
Block 14: Report shall be submitted in an electronic format agreed upon by both Government and Contractor prior to 1st submittal.
| Code 486M00E |
| 0 |
| 1 |
| 0 |
Code 254300E
| LTR |
| ONLY |
15. TOTAL
| 0 |
| 1 |
| 0 |
| G. PREPARED BY |
| H. DATE |
| I. APPROVED BY |
| J. DATE |
| Naval Air Warfare Center, Weapons Division, China Lake, CA 93555-6100 |
| 08/12/2016 |
| DRRB Chairperson |
File details come from the government source that posted it. Updated .