15RJQ82_0004.pdf

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT

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

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

30-105-04EXCEPTION TO SF 30

APPROVED BY OIRM 11-84

STANDARD FORM 30 (Rev. 10-83) Prescribed by GSA

FAR (48 CFR) 53.243

The purpose of this amendment is to revise the part numbers in the price matrix associated to CLINs 0008 - 0015 and the detailed descriptions - SOW #3 Descriptions and to revise SOW #1 in Section C. The closing remains 29 July 2015 at 2:00 PM EDT.

1. CONTRACT ID CODE PAGE OF PAGES

J 1 14

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

16C. DATE SIGNED

BY 28-Jul-2015

16B. UNITED STATES OF AMERICA15C. DATE SIGNED15B. CONTRACTOR/OFFEROR

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

8. NAME AND ADDRESS OF CONTRACTOR (No., Street, County, State and Zip Code) X N00164-15-R-JQ82

X 9B. DATED (SEE ITEM 11)

10-Jun-2015

10B. DATED (SEE ITEM 13)

9A. AMENDMENT OF SOLICITATION NO.

11. THIS ITEM ONLY APPLIES TO AMENDMENTS OF SOLICITATIONS

X The above numbered solicitation is amended as set forth in Item 14. The hour and date specified for receipt of Offer is extended, X is not extended.

Offer 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 copies of the amendment; (b) By acknowledging receipt of this amendment on each copy of the offer submitted;

or (c) By separate letter or telegram which includes a reference to the solicitation and amendment numbers. FAILURE OF YOUR ACKNOWLEDGMENT 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.

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.

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

CONTRACT ORDER NO. IN ITEM 10A.

B. THE ABOVE NUMBERED CONTRACT/ORDER IS MODIFIED TO REFLECT THE ADMINISTRATIVE CHANGES (such as changes in paying office, appropriation date, etc.) SET FORTH IN ITEM 14, PURSUANT TO THE AUTHORITY OF FAR 43.103(B).

C. THIS SUPPLEMENTAL AGREEMENT IS ENTERED INTO PURSUANT TO AUTHORITY OF:

D. OTHER (Specify type of modification and authority)

E. IMPORTANT: Contractor is not, is required to sign this document and return copies to the issuing office.

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

10A. MOD. OF CONTRACT/ORDER NO.

2. AMENDMENT/MODIFICATION NO. 5. PROJECT NO.(If applicable)

6. ISSUED BY

3. EFFECTIVE DATE

28-Jul-2015

CODE

NAVAL SURFACE WARFARE CENTER CRANE DIV

D.PEARSON (812-854-5201)

BLG. 3373

300 HIGHWAY 361

CRANE IN 47522-5001

N00164 7. ADMINISTERED BY (If other than item 6)

4. REQUISITION/PURCHASE REQ. NO.

CODE

See Item 6

FACILITY CODECODE

EMAIL:TEL:

N00164-15-R-JQ82

SECTION SF 30 BLOCK 14 CONTINUATION PAGE

SUMMARY OF CHANGES

SECTION B - SUPPLIES OR SERVICES AND PRICES

The following have been modified:

PRICE MATRICES

PROPOSED PRICES

CLIN 0001 - H-1 TSS - P/N 770E001

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

106 - 115

116+

CLIN 0003 – MTS-TU – 3717AS100

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

CLIN 0004 – MTS-TU – PN 85000000-1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

CLIN 0005 – MTS-TU – PN 85001160-2

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

CLIN 0006 – MTS-TU – PN 85000152-2

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

CLIN 0008 – MTS – SE – 85000758-1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

CLIN 0009 – MTS –SE – 85000368-1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15 16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95

96 - 105 106 – 115

CLIN 0010 –MTS – SE - 85000246‐1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

CLIN 0011 –MTS – SE – 85000244‐1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15 16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95

96 - 105

ROPOSED PRICES

CLIN 0012 –MTS – SE – 85000046-1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

CLIN 0013 –MTS – SE – 85000034-1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15 16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95

96 - 105

CLIN 0014 –MTS – SE – 85000024-1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15

16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95 96 - 105

CLIN 0015 –MTS – SE – 85001295-1

Quantity YR 1 YR 2 YR 3 YR 4 YR 5 1 – 5 6 - 15 16 - 25 26 - 35 36 - 45 46 - 55 56 - 65 66 - 75 76 - 85 86 - 95

96 - 105 106 - 115

116+

Contract Years - The anniversaries for the contract years consist of 365 days per year, with the exception of leap years, which consist of 366 days per year. The years commence upon contract award.

SECTION C - DESCRIPTIONS AND SPECIFICATIONS

The following have been modified:

SOW #3 DESCRIPTIONS

Multi-Spectral Targeting System - SE Detailed Descriptions – SOW #3 Descriptions

CLIN 0008 - CONTAINER, SHIPPING & STORAGE, HD ELECTRONICS ASSEMBLY (GRAY):

P/N 85000758-1 Rev - High Definition (HD) Electronics Assembly (EA) Shipping and Storage Container (gray) P/N 85000758-1 (Highest assembly drawing), 85000759-1 Rev A HD EA Container Inserts (Foam Inserts), 85000760-1 HD EA Container Name Plate (Metal UID label). The case material is Polyethylene molded Plastic with reinforced corners; it has Stacking male/female stacking ribs (top/bottom); Gray in color; A hinged lid (3 hinges (rear) and 5 latches (3 in front and 1 per side); hardware is zinc plated steel, 2 plastic handles, 140 lb rating, 90 degree stop (1 per side); Seal in a rubber gasket that is splash and rain resistant; Inside Dimensions 26.00”x 17.25”x14.75”, outside 29.00”x20.25”x16.94” high, Base inside Depth 11.00”, Lid inside depth 3.75”; cube shaped.

CLIN 0009 - CASE ASSEMBLY, AIRCRAFT MAINTENANCE FIXTURE (GRAY):

P/N 85000368-1 Rev – Aircraft Maintenance Fixture Case Assembly (Extended uprights Handles Container, gray) P/N 85000368-1 Rev - (Highest assembly drawing), 85000369-1 Rev - Aircraft Maintenance Fixture Inserts (Foam Inserts), 85000371-1 Rev – ACFT MAINT FIXT Container Nameplate (Metal UID label). The case material is Polyethylene molded Plastic with reinforced corners; it has Stacking male/female stacking ribs (top/bottom); Gray in color; A hinged lid (3 hinges (rear) and 5 latches (3 in front and 1 per side); hardware is zinc plated steel, 2 plastic handles, 150 lb rating, 90 degree stop (1 per side); Seal in a rubber gasket that is splash and rain resistant; Inside Dimensions 19.87”x 13.00”x12.25”, outside 22.87”x16.00”x13.94” high, Base inside Depth 9.25”, Lid inside depth 3.00”;

cube shaped.

CLIN 0010 - CASE ASSEMBLY, BORESIGHT EQUIPMENT (WHITE)

P/N 85000246-1 Rev D (Highest assembly drawing), 85000247-1 Rev B Boresighting Equipment Inserts (Foam Inserts), 85000277-1 Rev B Navy SE Contents Label (Contents Metal Label), 85000190-1 Rev B Boresighting Container Nameplate (Metal UID label). The case material is Polyethylene molded Plastic with reinforced corners, it has Stacking male/female stacking ribs (top/bottom), White in color, A hinged lid (3 hinges (rear) and 5 latches (3 in front and 1 per side), hardware is Stainless steel hinges, 2 plastic handles, 150 lb rating, 90 degree stop (1 per side), Seal a rubber gasket that is air tight, Breather valve single 0.5x0.5 PSIG w/manual RELEASE, Inside Dimensions 18.00”x 14.62”x18.86”, outside 21.00”x17.62”x20.55” high, Base inside Depth 14.93”, Lid inside depth 3.93”, cube shaped.

CLIN 0011 - CASE ASSEMBLY, AIRCRAFT MAINTENANCE FIXTURE (WHITE)

P/N 85000244-1 Rev E (Highest assembly drawing), 85000251-1 Rev B Aircraft Maintenance Fixture Inserts (Foam Inserts), 85000294-1 Rev B Navy ACFT MAINT FIXT Nameplate (Metal UID label), 85000243-2 Rev E Navy SE Contents Label (Metal contents label). The case material is Polyethylene molded Plastic with reinforced corners, it has Stacking male/female stacking ribs (top/bottom), White in color, A hinged lid (3 hinges (rear) and 5 latches (3 in front and 1 per side), hardware is Stainless steel hinges, 1 Stainless Steel handle with a rubber sleeve on front, 90 degree stop, Seal a rubber gasket that is air tight, Breather valve single 0.5x0.5 PSIG w/manual RELEASE, Inside Dimensions 19.87”x13.00”x7.00”, outside 22.87”x16.00”x8.69” high, Base inside Depth 4.00”, Lid inside depth.

CLIN 0012 - CONTAINER, SHIPPING & STORAGE, CSP ELECTRONICS ASSEMBLY (GRAY)

P/N 85000046-1 Rev A (Highest assembly drawing), 85000047-1 Rev A CSP EA Container Inserts (Foam Inserts), 85000048-1 Rev – CSP EA Container Nameplate (Metal UID label). The case material is Polyethylene molded Plastic with reinforced corners, it has Stacking male/female stacking ribs (top/bottom), Gray in color, A hinged lid (3 hinges (rear) and 5 latches (3 in front and 1 per side), hardware is Zinc Plated steel hinges, 2 plastic handles, 150 lb rating, 90 degree stop (1 per side), Seal a rubber gasket that is splash and rain resistant, Inside Dimensions 26.00”x 17.25”x14.75”, outside 29.00”x20.25”x16.94” high, Base inside Depth 11.00”, Lid inside depth 3.75”, cube shaped.

CLIN 0013 - CASE ASSEMBLY, AIRCRAFT MAINTENANCE FIXTURE (GRAY)

P/N 85000034-1 Rev H (Highest assembly drawing), 85000033-1 Rev B Aircraft Maintenance Fixture Inserts (Foam Inserts), 85000230-2 Rev D SE Container Nameplate (Metal UID label). The case material is Polyethylene molded Plastic with reinforced corners, it has Stacking male/female stacking ribs (top/bottom), Gray in color, A hinged lid (3 hinges (rear) and 5 latches (3 in front and 1 per side), hardware is Zinc Plated steel hinges, 1 Zinc Plated steel handle with a rubber sleeve on front, 90 degree stop, Seal a rubber gasket that is splash and rain resistant, Inside Dimensions 19.87”x13.00”x7.00”, outside 22.87”x16.00”x 8.69” high, Base inside Depth 4.00”, Lid inside depth 3.00”.

CLIN 0014 - CASE ASSEMBLY, BORESIGHT EQUIPMENT (GRAY)

P/N 85000024-1 Rev H (Highest assembly drawing), 85000027-1 Rev D Boresighting Equipment Inserts (Foam Inserts), 85000230-1 Rev D SE Container Nameplate (Metal UID Label). The case material is Polyethylene molded Plastic with reinforced corners, it has Stacking male/female stacking ribs (top/bottom), Gray in color, A hinged lid (3 hinges (rear) and 5 latches (3 in front and 1 per side), hardware is Zinc Plated steel hinges, 2 plastic handles, 150 lb rating, 90 degree stop (1 per side), Seal a rubber gasket that is splash and rain resistant, Inside Dimensions 18.00”x 14.62”x18.86”, outside 21.00”x17.62”x20.55” high, Base inside Depth 14.93”, Lid inside depth 3.93”, cube shaped.

CLIN 0015 - CONTAINER, SHIPPING AND STORAGE, C130 ELECTRONICS ASSEMBLY

P/N 85001295-1 Rev - (Highest assembly drawing), 85001296-1 Rev - Base Insert, EA Container and 85000752-1 Rev - Lid Insert, EA Container (Foam Inserts), 85001326-1 Rev -, Nameplate, C130 EA Container SE. The case material is Polyethylene molded Plastic with reinforced corners, it has Stacking male/female stacking ribs (top/bottom), Grey in color, a hinged lid (3 hinges (rear) and 5 latches (3 in front and 1 per side), hardware is Stainless Steel, 2 plastic handles, 150 lb rating, 90 degree stop (1 per side), Seal a rubber gasket that is airtight, Single 0.5x0.5 PSIG w/Manual Release Breather Valve, Inside Dimensions 26.00”x 17.25”x14.75” High, Outside Dimensions 29.00”x20.25”16.94” high, Base inside Depth 11.00”, Lid inside depth 3.75”, cube 5.8.

STATEMENT OF WORK #1

STATEMENT OF WORK (#1)

Target Sight Systems - TSS

1. SCOPE

1.1 This Statement of Work (SOW) defines the requirements and tasks to be performed by the Contractor, including, and in support of, the production and sustainment of shipping and storage containers for the AN/AAQ-30 Target Sight System (TSS). Articles to be furnished hereunder shall be manufactured, repaired, tested and inspected in accordance with the drawings and documents specified in Section 2, and this SOW.

2. APPLICABLE DOCUMENTS

Unless otherwise specified, the most current version of the documents listed in the Department of Defense Index of Specifications and Standards, DODISS, or as identified by the appropriate industry office, shall be applicable.

2.1 DoD Standards

MIL-STD-130N Identification Marking of U.S. Military Property 16-NOV-12 (w/Change 1) MIL-STD-2073-1E Standard Practice for Military Packaging 07-JAN-11 (w/Change 1) MIL-STD-3464E Desiccants, Activated, Bagged, Packing Use and 21-APR-87

Static Dehumidification MIL-DTL-5541F Chemical Conversion Coatings on Aluminum 11-JUL-06 and Aluminum Alloys MIL-STD-81381 Wire, Electric, Flourocarbon/Polymide Insulated Various (all versions)

MIL-W-22248A Weldments, Aluminum and Aluminum Alloy 06-JUN-85

2.2 Government Documents

Drawings:

770E001 H-1 Targeting Sight System Shipping Container 09-JUL-10 (16 drawings in package)

2.3 Industry Documents

AS9100 Rev C Quality Systems - Aerospace - Model for Quality 15-JAN-09

Assurance in Design, Development, Production, Installation and Servicing

ANSI/AWS D17.1:2001 Specification for Fusion Welding for 09-JAN-01

Aerospace Applications

ASQC-Q9001 Quality Systems, Model for Quality Assurance 02-JAN-00 in Design, Development, Production, Installation and Servicing

ASTM B841-99 Standard Specification for Electrodeposited 2010 Coatings for Zinc Nickel Alloy Deposits

AWS D1.2/D1.2M:2008 Structural Welding Code – Aluminum 23-JUN-08 ISO 10012:2003 Measurement Management Systems - Requirements 1-APR-03 for Measurement Processes and Measuring Equipment ANSI/NCSL-Z540.3-2006 Requirements for the Calibration of Measuring and 3-AUG-06

Test Equipment SAE-AS22759 Wire, Electrical, Fluoropolymer-Insulated, 01-OCT-14

Copper or Copper Alloy

3. REQUIREMENTS

3.1 The Contractor shall produce or repair and deliver TSS Shipping Containers, Drawing 770E001 (hereinafter referred to as the TU Container) as specified by individual orders placed on this contract, in accordance with the drawings listed in 2.2.

3.1.2 When discrepancies exist between these requirements and the drawings in 2.2, these requirements shall prevail.

3.1.3 Unless expressly provided for elsewhere in this section, equipment such as fixtures, jigs, dies, patterns, special tooling, test equipment, or any other manufacturing aid required for the manufacture and/or testing of the subject item(s) will not be provided by the Government or any other source, and is the sole responsibility of the Contractor.

The foregoing applies notwithstanding any reference to such equipment or the furnishing thereof that may be contained in any drawing or referenced specification.

3.1.4 THE USE OF MIL-STD-81381 WIRE IN ANY ITEM TO BE DELIVERED UNDER THIS

PROCUREMENT IS PROHIBITED. The foregoing prohibition applies notwithstanding any reference to MIL-STD- 81381 wire that may be made in any of the drawings or specifications for this procurement. SAE-AS22759 latest revision series wire shall be used in lieu of MIL-STD-81381 wire in any place where MIL-STD-81381 wire is cited in this procurement. Any questions concerning this requirement should be directed to the NSWC Crane Division Technical POC.

3.1.5 Packaging shall be in accordance with MIL-STD-2073-1E.

3.2 TU CONTAINER The following requirements and paragraph 3.3.6 are specific to the production of TU Containers built to Drawing 770E001.

3.2.1 TU Containers shall mitigate shock and vibration to a maximum allowable limit of 15 g’s.

3.2.2 The Contractor shall complete test requirements specified in Paragraph 3.3.

3.2.3 The Contractor is required to ensure one third (1/3) unit of desiccant (MIL-STD-3464E, Type II non-dusting) per cubic foot of container interior volume shall be placed in desiccant holder of each TU Container at time of shipment.

3.2.4 The Contractor shall use the shock mount specified on Drawing 770E001 for the shock mitigation system of this container. No other shock mount may be substituted, no other mount is an approved alternate mount.

3.2.5 The Contractor shall affix a nameplate that includes a Unique Identification (UID) marking as referenced in the drawing package for Drawing 770E001, and in accordance with MIL-STD-130N, per Paragraph 3.1, on each TU container. The Contractor shall contact the NSWC Crane Division Technical POC for the alphanumeric sequential serial number group that makes up part of the UID. The UID will be included on the nameplate in data matrix format.

At the time of delivery, the Contractor shall report the bar code data for all items marked under this paragraph.

CDRL A001, Bar Code Report / UID Plan.

3.2.6 WELDING. (Aluminum). The Contractor shall use proper controls to prevent melt through or burn through.

The Contractor shall ensure welder qualifications are to ANSI/AWS D17.1:2001. The Contractor shall ensure that filler for welding 6061 alloy shall be 4043, and filler for welding 5000 series alloys to themselves or to 6061 shall be 5356 or 5556. Welding and weld inspection shall be in accordance with MIL-W-22248A, Class 4, except that:

(A) visual inspection shall include 5X (5 power) magnification when a suspect condition is to be examined beyond the capability of normal vision; and

(B) critical and major welds may be subjected to further non-destructive testing (such as dye penetrant inspection) as prescribed by the buying activity.

3.2.7.1 CLEANING. The Contractor shall ensure that parts to be welded are chemically cleaned to remove surface soils such as oils, waxes, grease, inks, etc. The Contractor shall not use uninhibited alkaline solutions such as sodium hydroxide in cleaning.

3.2.7.2 DEOXIDIZING. The Contractor shall ensure that cleaned parts are chemically deoxidized NO MORE THAN 10 CONSECUTIVE DAYS (240 hours) PRIOR TO WELDING to remove thick surface oxide films. [If the material or work is exposed to an outdoor environment, this time limit shall be reduced to a maximum of 3 consecutive days (72 hours), to account for atmospheric effects.] The Contractor shall apply mechanical cleaning methods (per 3.2.7.4) just prior to the actual start of welding, to remove any re-oxidation or residual thin oxide films.

3.2.7.3 CHEMICAL TREATMENT. The Contractor shall apply an acid deoxidizing treatment by either immersion or brushing/wiping. The Contractor shall use one of the following deoxidizers: nitric acid, sulfuric chromic, phosphoric chromic, or equivalent solutions. Sodium hydroxide solutions shall not be used. The Contractor shall ensure that 100% solution coverage of the area to be welded is applied, which includes an area extending at least 2 inches from the weld site, or ending at any closer adjacent edge.

3.2.7.4 MECHANICAL MEANS. Immediately prior to welding, the Contractor shall apply mechanical cleaning methods to previously chemically treated weld areas to assure removal of residual or reformed oxides, if any.

Acceptable methods of mechanical cleaning include stainless steel wire brushing, scraping, filing, or sanding.

However, the Contractor shall not use abrasives containing iron and its oxides, steel wool and wire, and copper alloy based wire, which may become embedded with galvanically active metals and accelerate corrosion of aluminum alloys. The Contractor shall ensure that mechanical methods are vigorous enough to adequately remove any residual oxide films, but gentle enough to avoid forming an excessively rough surface in the comparatively soft metal underneath. The Contractor shall ensure that welding and welder qualifications meet AWS D1.2/D1.2M:2008 standards. Additionally, the Contractor shall ensure that cleaning preparations are in accordance with MIL-DTL- 5541F and paragraph 3.2.7.2.

3.3 QUALITY ASSURANCE – TU Container

3.3.1 FIT CHECK. The Fit Check specified in paragraph 3.3.4 must be successfully completed for the initial container from the contractor. Quality Assurance (QA) Inspections are to be completed by the Contractor for every TSS Turret Container, as detailed in paragraph 3.3.5 and listed in Appendix A of this Statement of Work. The container shall be tested in accordance with paragraphs specified herein, using processes recommended in SAE APR1967 Rev B, to ensure shock and vibration does not exceed the allowable limit of 15 g’s.

3.3.2 GOVERNMENT FURNISHED PROPERTY. For the Fit Check of the initial TU container referenced in 3.3.1, the Contractor shall ship the TU container to a site designated by the Government upon completion of the initially built container. The Government will ensure a TSS turret assembly (part number 79705501) and top plate assembly (part number 85000742) are available at the designated site for installation in the TU container as part of the Fit Check process. The Fit Check of the initial TU container will be witnessed by NSWC Crane or DCMA as determined at the time of the Fit Check. If the TU container passes the Fit Check, the container will remain at the Government designated site for immediate use. If the TU container does not pass the Fit Check, the container will be returned to the Contractor for repairs, corrections and/or changes.

3.3.3 INSPECTION. Inspection for compliance with Drawing 770E001 and specifications referenced therein will be conducted by the NSWC Crane or DCMA as required by each Delivery Order (DO).

3.3.4 FIT CHECK LOCATION. The Fit Check will be conducted by the Government at a site and facility to be determined by the Government. The Contractor should plan for the fit check to take approximately one week.

3.3.4.1 FIT. An end item shall be mounted in the TU Container. When secured, the end item shall not make contact with any part of the container, including the isolation frame, other than the mounting points specified on the Drawing, at any point in time. The cover shall fit securely and not be constrained by the end item. The container is to be moved and rotated in all axes. The container shall be inspected for clearance between the bottom of the end item and the bottom of the container. The fit of the top plate in the isolation frame shall be firm and not strained in any way. The end item shall be installed into and removed from the container utilizing the top plate handle tubes and current specified procedures (per Drawing 770C005) to ensure that the container is fully functional in this respect.

3.3.5 QA Inspection shall be conducted using an empty container.

a. Drop Test, Unloaded, 18-inches above the floor

b. Visual Exterior inspection as listed on the QA Inspection Data Sheet in Appendix A

c. Visual Interior inspection as listed on the QA Inspection Data Sheet in Appendix A

d. Leak Test as listed on the QA Inspection Data sheet and explained in Paragraph 3.3.6.

At the time of delivery, the Contractor shall report the inspection results for all containers. CDRL A002, Test/Inspection Report.

3.3.6 LEAK TESTING. All turret containers shall be leak tested. The container shall be prepared for testing by sealing all breathing devices and inserting suitable pressurizing fittings and gauges. The container shall be closed and sealed in accordance with normal procedures. The Pneumatic-Pressure Technique of Method 5009 of Federal Test Method Standard Number 101C shall be used to detect leakage. An initial pressure setting equal to 0.5 + 0.1 - 0 pounds per square inch, gauge, (PSIG) shall be used. After stabilization, pressure shall be monitored for thirty minutes. Any loss in pressure in excess of 0.05 PSIG shall be cause for rejection. DCMA will witness a minimum of three percent (3%) sample or a minimum of one (1) examination/leak test. The DCMA representative shall be notified 14 calendar days in advance of the test schedule. NSWC Crane Division reserves the right to designate a representative to witness testing. The contractor shall notify the NSWC Crane Division technical point of contact 14 days in advance of the test schedule.

3.3.7 The Contractor shall comply with the AS9100 higher-level Quality System.

3.3.8 Measuring and Test Equipment - The Contractor shall use a calibration system that meets the requirements of ANSI/NCSL-Z540.3-2006, or ISO 10012:2003.

3.4 REPAIR

3.4.1 The Contractor shall repair or replace non-warranty repairable items on the containers to ready for issue (RFI) condition. Repairs are to be effected to the requirements identified on the applicable drawings in section 2.2. See Section B of the Contract for further detail regarding repair procedures.

4. The NSWC Crane Division’s technical point of contact is Daniel Reinhart, Code JXQL, telephone (812) 854- 4515 or email daniel.reinhart@navy.mil.

5. DATA DELIVERABLES

CDRL A001 IUID Report 3.2.5 DI-MGMT-81858 CDRL A002 Test/Inspection Report 3.3.5 DI-NDTI-80809B

(End of Summary of Changes)