W56HZV19R0059-0001.pdf

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT 1. Contract ID Code Page Of

2. Amendment/Modification No.

3. Effective Date

4. Requisition/Purchase Req No.

5. Project No. (If applicable)

6. Issued By Code 7. Administered By (If other than Item 6) Code

8. Name And Address Of Contractor (No., Street, City, County, State and Zip 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 is extended, is not extended.

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 ____________ copies of the amendments: (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 ONLY APPLIES TO MODIFICATIONS OF CONTRACTS/ORDERS

It Modifies The Contract/Order No. As Described In Item 14.

A. This Change Order is Issued Pursuant To: 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 data, 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.)

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)

16A. Name And Title Of Contracting Officer (Type or print)

15B. Contractor/Offeror 15C. Date Signed 16B. United States Of America 16C. Date Signed

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

NSN 7540-01-152-8070

PREVIOUS EDITIONS UNUSABLE

30-105-02 STANDARD FORM 30 (REV. 10-83)

Prescribed by GSA FAR (48 CFR) 53.243

SEE SCHEDULE

X

Firm Fixed Price

0001 2019NOV13

W56HZV

U.S. ARMY CONTRACTING COMMAND

WARREN, MICHIGAN 48397-5000

KERI SKROBOT

EMAIL: KERI.L.SKROBOT.CIV@MAIL.MIL

W56HZV-19-R-0059

2019NOV05

X

X

/SIGNED/

2 signed

SEE SECOND PAGE FOR DESCRIPTION

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CONTINUATION SHEET

Reference No. of Document Being Continued Page of

Name of Offeror or Contractor:

PIIN/SIIN MOD/AMD

SECTION A - SUPPLEMENTAL INFORMATION

Buyer Name: KERI SKROBOT

Buyer Office Symbol/Telephone Number: CCTA-HCS-A/(586)282-8301

Type of Contract 1: Firm Fixed Price

Kind of Contract: Supply Contracts and Priced Orders

*** End of Narrative A0000 ***

Amendment 0001 to Solicitation W56HZV-19-R-0059 makes the necessary corrections per the Questions & Answers Set #1 - 13 November 2019.

1. Section B - FAT CLINs reflect ASTM E2377-18 Specifications.

2. Section C - Scope of Work numbering is corrected.

3. Section F - Long Term Contracts FOB Destination Clause is included.

*** END OF NARRATIVE A0002 ***

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W56HZV-19-R-0059

PIIN/SIIN

Page of

Name of Offeror or Contractor:

ITEM NO SUPPLIES/SERVICES QUANTITY UNIT UNIT PRICE AMOUNT

Reference No. of Document Being Continued

MOD/AMD

SECTION B - SUPPLIES OR SERVICES AND PRICES/COSTS

0016 FIRST ARTICLE TEST (FAT) UNIT - LMS TYPE I 1 EA $ $ __________________________________________ ______________ __________________

COMMODITY NAME: FAT UNIT LMS TYPE I

Mfr CAGE: 81337

Mfr Part Number: ASTM E2377-18

Packaging and Marking _____________________

PACKAGING/PACKING/SPECIFICATIONS:

SEE PACKAGING CLAUSE

LEVEL PRESERVATION: Military

LEVEL PACKING: A

Inspection and Acceptance _________________________

INSPECTION: Origin ACCEPTANCE: Origin

Government Approval/Disapproval Days: 30

0026 FIRST ARTICLE TEST (FAT) UNIT - LMS TYPE III 1 EA $ $ ____________________________________________ ______________ __________________

COMMODITY NAME: FAT UNIT LMS TYPE III

Mfr CAGE: 81337

Mfr Part Number: ASTM E2377-18

Packaging and Marking _____________________

PACKAGING/PACKING/SPECIFICATIONS:

SEE PACKAGING CLAUSE

LEVEL PRESERVATION: Military

LEVEL PACKING: A

Inspection and Acceptance _________________________

INSPECTION: Origin ACCEPTANCE: Origin

Government Approval/Disapproval Days: 30

0036 FIRST ARTICLE TEST (FAT) UNIT - LMS TYPE V 1 EA $ $ __________________________________________ ______________ __________________

COMMODITY NAME: FAT UNIT LMS TYPE V

Mfr CAGE: 81337

Mfr Part Number: ASTM E2377-18

Packaging and Marking _____________________

PACKAGING/PACKING/SPECIFICATIONS:

SEE PACKAGING CLAUSE

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PIIN/SIIN

Page of

Name of Offeror or Contractor:

ITEM NO SUPPLIES/SERVICES QUANTITY UNIT UNIT PRICE AMOUNT

Reference No. of Document Being Continued

MOD/AMD

LEVEL PRESERVATION: Military

LEVEL PACKING: A

Inspection and Acceptance _________________________

INSPECTION: Origin ACCEPTANCE: Origin

Government Approval/Disapproval Days: 30

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SECTION C - DESCRIPTION/SPECIFICATIONS/WORK STATEMENT

SECTION C - DESCRIPTION/SPECIFICATIONS/WORK STATEMENT

C.1. Background: The intent of this contract is to provide for the design and fabrication of the Lightweight Multi-Purpose Shelter (LMS)

Type I, Type III, and Type V which are designed for transport on the M1152A1 and the M1152A1 with B2 Armor Kit High Mobility Multi-

Purpose Wheeled Vehicle (HMMWV). These shelters are transported by rail, air, marine, and highway when mounted or dismounted from their vehicles. These tactical rigid wall shelters are used to house battlefield electrical systems. The LMS Type I and Type III are

Electromagnetic Interference (EMI) shielded. The LMS Type V is a modified LMS Type I configured with double rear doors and is not EMI shielded.

C.2. General Scope:

C.2.1. The Contractor shall supply all necessary personnel, facilities, equipment, and materials to accomplish the requirements set forth herein. Each LMS, both First Article and Production, shall be equipped with one (1) Shelter To HMMWV Mounting Kit and one (1)

Pintle Extension Kit which are separately boxed and stored inside the shelter. For production units only, one (1) Technical Manual shall also be over-packed in each shelter with each end item delivered to the Government. Copies of the Technical Manual will be provided by the Government. Vehicle drawings and the vehicles themselves (M1152A1 Expanded Capacity Enhanced Integrated Armor Package (IAP)/Armor

Ready HMMWV and M1152A1 with B2 Armor Kit Expanded Capacity Enhanced Armored HMMWV) will not be provided as Government Furnished

Equipment (GFE) under this contract. It shall be the responsibility of the Contractor to secure the use of sufficient HMMWVs and to mount the First Article Test Units on the HMMWVs to test and during validation of Technical Manual. One suggested source to contact is:

U.S. Army Aberdeen Test Center (ATC), Aberdeen, MD, (410) 278-4639. The Contractor may use Government test facilities with Government pricing for necessary testing of the LMS.

C.2.2. Detailed Performance / Interface Requirements: The Contractor shall design, manufacture and furnish all three variants of the LMS

Shelter (Type I, Type III, and Type V). The shelter shall meet the requirements of ASTM E2377-18 Standard Specification for Shelter, Electrical Equipment, Lightweight which can be accessed at the following website http://www.astm.org .) with exceptions as noted below in this Statement of Work (SOW). The drawings listed in Paragraph 2.7 of ASTM E2377-18 detailing the Pintle Extension Kit, the

Shelter to HMMWV Mounting Kit, the Interface Control Drawing, and the Standard Camouflage Pattern for the LMS are provided in Attachment

0003. The exceptions to ASTM E2377-18 for the LMS Type V includes, but not limited to: the requirement for a double door in lieu of a single door, the deletion of the EMI requirements, and an increase to the maximum weight of the shelter to 650 lbs. to accommodate the double door design. The complete list of exceptions to ASTM E2377-18 are provided in Sections C.2.2.1 for all three types and C.2.2.2 for the Type V only and are as follows:

C.2.2.1. Exceptions to ASTM E2377-18 for the LMS Type I, Type III and Type V:

Global Changes: Unless stated otherwise the following changes shall be made throughout the ASTM Specification and all section number references pertain to the corresponding sections of ASTM E2377-18:

Section 2.7 Drawings: 17-1-8584 Mounting Kit Shelter To HMMWV (For Reference Only). The existing mounting kit will have to be redesigned due to the new mounting requirements for the M1152A1 and M1152A1 with B2 Armor Kit HMMWV. All references to 17-1-8584 shall be replaced with the new Mounting Kit, Shelter to HMMWV.

Section 3.2.3.3 Integration - The shelter shall be capable of accepting standard LMS integration configurations without significant modification or rework to the system integration designs. The shelter shall be capable of accepting integration configuration cutouts at various locations. The shelter surfaces, including the door, shall be capable of accepting the installation of individual pieces of equipment installed by system integrators at various locations. For installations where threaded mechanical fasteners are the preferred fasteners, the attaching surfaces shall be capable of resisting the loads listed in Table 4 for the listed sizes of threaded mechanical fasteners, without damage or degradation to the shelter or fastener.

(1) Torque - To determine compliance, a torque load equal to 8 ft-lb (1.11 kg-m) for the 10-32 bolt and 10 ft-lb (1.38 kg-m), for the other bolts shall be applied to all fasteners installed in the shelter, fasteners used to integrate the system (see ASTM E2377-18

4.2.3.3) should be used wherever possible. Failure to meet the torque requirements of 3.2.3.3 shall constitute failure of this test.

(2) Pull-out - To determine compliance, a tensile load equal to 800 lbs. (362.9 kg) for the 10-32 bolt and 1,000 lbs. (453.6 kg) for the other bolts shall be applied to all fasteners installed in the shelter, fasteners used to integrate the system (see ASTM E2377-18

4.2.3.3) should be used wherever possible. Failure to meet the pull-out requirements of ASTM E2377-18 3.2.3.3 shall constitute failure of this test.

Section 4.4.1 Rail Transport - The dismounted shelter and shelter/vehicle combinations (using the M1152A1 with B2 Armor Kit HMMWV), with a simulated payload (see ASTM E2377-18 4.2.1.2), shall be tested in accordance with test method standard MIL-STD-810, Method 526.2, Rail

Impact. When secured to the flatcar, the shelter and shelter vehicle combinations shall then be inspected for conformance to Gabarit

International de Chargement (GIC) gauge envelope as shown in interface standard MIL-STD-1366. Failure to meet the requirements of ASTM

E2377-18 3.4.1 shall constitute failure of this test.

Section 4.4.4 Ground Mobility - The shelter/vehicle combination (using the M1152A1 with B2 Armor Kit HMMWV), with a simulated payload

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(see ASTM E2377-18 4.2.1.2), shall be tested for compliance with ASTM E2377-18 3.4.4. SAE-AS8090, Type V Mobility, shall be used as guidance for this test. Failure to meet the requirements of ASTM E2377-18 3.4.4 shall constitute failure of this test. Table 7 ASTM

E2377-18 in defines the speed/distance requirement for ground mobility testing.

Delete Section 6.2.5 in ASTM E2377-18 in its entirety.

C.2.2.2. Exceptions to ASTM E2377-18 for the LMS Type V ONLY:

Global Changes: Unless stated otherwise the following changes shall be made throughout the ASTM Specification and all section number references pertain to the corresponding sections of ASTM E2377-18: Replace all references of "Interface Control Drawing 17-2-0035" with

"Interface Control Drawing 17-2-0035-Type V" which will define the double door end wall design (See SOW paragraph C.2.4.1.2). Replace all references of "the shelter" with "LMS Type V" which is a modified LMS Type I. Replace all references of "the shelter door" with

"the shelter doors." ASTM Section 3. General Requirements Changes: The following paragraphs shall replace the corresponding paragraphs in Section 3 of ASTM E2377-18:

Section 3.2.1 Weight and Payload - The LMS Type V shelter shall weigh no more than 650 lbs. and shall have a payload of at least 3,300 lbs. The maximum LMS Type V shelter weight listed does not include the weight of the Mounting Kit (90 lbs. maximum) and Pintle Extension

(50 lbs. maximum) and their attaching hardware ASTM E2377-18 (See Table I). The Contractor shall fashion an appropriate simulated payload design to be used for all testing. The payload design shall include a minimum of 40 lbs. interior payload located on each door.

The payload design shall be approved by the procuring agency prior to its use in any test.

Section 3.2.2.1 Spare Parts - The spare parts are listed in ASTM E2377-18 Table 2 and are depicted on interface drawing number 17- 2-

0035-Type V. All spare parts and related assemblies shall be functionally and dimensionally interchangeable without modification or rework of the parts, assembly, or LMS Type V shelter.

Section 3.2.4 Chemical and Biological (CB) Resistance - All shelter surfaces, except weather seals and gaskets, shall be resistant to, and shall not absorb, chemical and biological agent contamination, decontamination fluids, and petroleum products. Weather seals and gaskets shall either meet the requirements above or be easily replaceable.

Section 3.2.8 Doors - The LMS Type V shelter shall be equipped with a primary door and secondary door in the shelter rear end wall. The primary door shall be the right door (when facing the rear end wall from the outside). It shall have an opening of 30 inches wide and 55 inches high and shall be centered on the shelter end wall. The secondary door shall be the left door (when facing the rear end wall from the outside) and shall provide an opening 18 inches wide and 55 inches high. There shall be an un-obstructed opening 48 inches wide by

55 inches high when both doors are opened. The double door design shall allow both doors to open fully (approximately 180 degrees). The secondary door shall have the ability to be locked out such that entry/exit is only allowed through the primary door. Doors must have the ability to be locked from outside but not trap personnel inside.

Doors must not be removable from the outside with the door padlocked shut. The primary door shall be capable of being opened from the ground when the shelter is on the vehicle without the use of a ladder. Commonality of parts shall be maximized for both doors. Both doors shall be capable of accepting threaded fasteners (see ASTM E2377-18 3.2.3.3). Both doors shall have door stops (see ASTM E2377-18

3.2.8.3) at approximately 90 degrees.

Section 3.2.8.1 Door Handle - From inside or outside of the LMS Type V shelter, the primary door shall be capable of being opened and closed with a maximum force of 48 lbs. (21.8kg) applied to the door handle. From inside the shelter, the primary door shall be capable of being opened and closed with a maximum force of 48 lbs. (21.8kg) applied to the door handle with the outside handle locked. The primary door shall be capable of being padlocked from the outside, and when closed the primary door shall prevent the secondary door from opening. If the secondary door is equipped with a handle, it shall also meet these requirements and shall be operable from the inside. The secondary door shall not have an exterior handle.

Section 3.2.8.2 Door Structure and Hinge Assembly - Both door and hinge assemblies shall be capable of supporting a 200 lbs. (90.7 kg) static load applied parallel to the hinge line, along the door edge opposite the hinge, with the door open to 90 degrees, without degradation or damage to the door or door hardware, and the door shall operate freely after such a load is applied.

Section 3.2.8.3 Door Stop - Both doors shall include a doorstop capable of automatically latching the door, when opened, at 90 degrees.

The stop shall automatically prevent the door from swinging beyond 90 degrees when engaged and allow the door to fully open

(approximately 180 degrees) when disengaged. The door stop shall be capable of being disengaged by personnel, while they are standing on the ground, while the shelter is mounted on the HMMWV and shall not obstruct entry/exit through the doors. The doorstop shall be capable of withstanding a static load equal to 10 lb./sqft. (0.0049 kg./sqcm.) times the largest surface area of the door. The load shall be applied to the doors largest surface and on the edge opposite the hinge, with the door latched at 90 degrees. The doors and their hardware shall be capable of withstanding these loads without degradation, damage, or improper door operation.

Section 3.2.8.4 Door Maintainability - Both doors shall not be removable from the exterior when locked and shall be removable with hand tools when unlocked. Hand tools are defined as those found in Tool Kit, General Mechanics, Automotive and Shop Equipment, Automotive

Maintenance and Repair (NSN: 5180-00-177-7033 and 4910-00-754- 0654, respectively).

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Section 3.2.8.5 Door Drip Edge - There shall be a drip edge over the entire width of the double door frame opening. The drip edge shall prevent water rolling down the side of the shelter from entering the shelter.

Section 3.3.2 Electromagnetic Interference (EMI) - Deleted in its entirety for the LMS Type V.

Section 3.4.5 Fording - Deleted in its entirety for the LMS Type V.

ASTM Section 4. Verification Changes: The following paragraphs shall replace the corresponding paragraphs in Section 4 of ASTM E2377-18 for LMS Type V:

Section 4.2.1.1 Weight - Delete the last sentence and replace with: "Any item exceeding maximum weight specified in paragraph ASTM E2377-

18 3.2.1 shall be considered a failure."

Section 4.2.1.2 Payload - After the last sentence, add "The simulated payload shall include a minimum of a 40lb interior payload located on each door."

Section 4.2.8 Doors - The doors shall be inspected to ensure compliance with ASTM E2377-18 3.2.8. Failure to meet the requirements of

3.2.8 shall constitute failure of this test.

Section 4.2.8.1 Door Handle - The shelter doors shall be securely closed. A 48lb (22 kg) load shall be applied to the primary door handle in the direction which best facilitates opening the door. After it has been verified that 48lb is adequate to open the door, the door shall be closed and a 48lb (21.8 kg) force shall be applied in the direction which best facilitates the securing of the door. After is has been verified that 48lbs (21.8 kg) is adequate to secure the door, the outer primary door handle shall be locked and the above procedure shall be repeated. Failure to meet the requirements of ASTM E2377-18 3.2.8.1 shall constitute failure of this test.

Section 4.2.8.2 Door Structure and Hinge Assembly Both doors shall have a 200lb (90.7 kg) static load applied parallel to the hinge line, along the door edge opposite the hinge, with the door open to 90 degrees. After 30 minutes the loads shall be removed from each door and both doors examined. Failure to meet the requirements of ASTM E2377-18 3.2.8.2 shall constitute failure of this test.

Section 4.2.8.3 Door Stop - This test shall be performed on both doors in the open position, held by the door stop mechanism. A fixture shall be attached to the midpoint of the edge of each door opposite from the hinge which shall permit the application of a load equivalent to 10 lb./ft. squared (0.0049 kg./cm. squared) times the largest surface area of the door, normal to the doors surface, using free running pulleys and a 1/4 in. (0.635 cm) diameter steel cable to transmit the load. Failure to meet the requirements of ASTM E2377-

18 3.2.8.3 shall constitute failure of this test.

Section 4.3.2 Electromagnetic Interference (EMI) - Delete in its entirety for the LMS Type V.

Section 4.4.3 Rotary Wing External Air Transport - The shelter and shelter/vehicle combinations, with a simulated payload (see ASTM

E2377-18 4.2.1.2), shall be tested in accordance with interface standard MIL-STD- 209 and Annex A1. Failure to meet the requirements of

ASTM E2377-18 3.4.3 shall constitute failure of the test. The actual Flight Testing detailed in Annex A1 Paragraph A1.2.5 can be waived if it can be demonstrated that the requirement has been previously verified on the same or similar design such as the LMS Type I or the

LMS Type III. Even if the actual Flight Test is waived by the Government for the LMS Type V, the Simulated Helicopter Lift Test must still be performed as part of First Article Testing.

Section 4.4.5 Fording - Deleted in its entirety for the LMS Type V.

ASTM Section 6 Changes: The following paragraphs shall replace the corresponding paragraphs in Section 6 of ASTM E2377-18 for the LMS

Type V:

Section 6.1 Intended Use - The LMS Type V shelters are highly mobile multipurpose shelters. They are suited for housing electronics and communications equipment. They can be mounted on the M1152A1 and M1152A1 with B2 Armor Kit HMMWV. These Shelters are not intended for airdrop.

Section 6.2 Acquisition Requirements - The following acquisition information is provided:

Section 6.2.1 Title, number and date of the specification. The shelter shall meet the requirements of ASTM E2377-18 Type I with exceptions as noted in this SOW.

End of Exceptions to ASTM E2377-18

C.2.3. Contract Management

C.2.3.1. Program Manager (PM): The Contractor shall assign a Program Manager (PM). This individual shall serve as primary Point of

Contact (POC) between the Government and the Contractor and shall be responsible for the coordination of all Contractor activities

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related to the contract. This person shall have the authority to commit the Contractor to specific courses of action and accept direction from the Contracting Officer. This person shall be responsible for coordinating all meetings between the Government and the

Contractor. The PM shall be responsible for bringing to the Contracting Officer's attention any conflicts in the Contractor's interpretation of the contract requirements 5 business days (first by telephone and then followed up in writing) or problems that could adversely affect the Contractor's ability to meet the stated quality, cost, or production/delivery schedule requirements.

C.2.3.2. Configuration Management (CM): The Contractor shall implement and maintain an internal configuration management program for the

LMS throughout the life of the contract. Military Handbook, Configuration Management Guide, MIL-HDBK-61A(SE), Paragraph 5.2 may be used as a guide for the Contractor's configuration management program, which can be found at https://assist.daps.dla.mil .

C.2.3.2.1. The Contractor shall establish and use configuration control procedures to manage proposed changes, beginning with the submission of the First Article Test items. Configuration control shall be used to document the proposed changes, the purpose and the impact of proposed changes, and to update configuration documentation. The Contractor shall include evaluation of human system integration, safety, system safety, and logistical impact(s) of alternative Engineering Change Proposals (ECP) associated with design tradeoffs. Following Government-acceptance of First Article Test (FAT) units, the Contractor shall not alter the design in form, fit, or function without submitting an ECP, a Request for Variance (RFV), a Value Engineering Change Proposal (VECP), or a Notice of Revision

(NOR) to the Contracting Officer and receiving written approval from the Contracting Officer to proceed. Once approved, a contract modification will be prepared by the Contracting Officer to incorporate the change into the contract, as well as an equitable adjustment

(if appropriate) to the contract price or other contract terms and conditions as a result. Such changes shall be made in accordance with the applicable contract clauses(s).

C.2.3.2.2. The Contractor shall control the Physical Configuration Baseline (PCBL) using the change control and engineering release processes. The PCBL is the product performance requirement for replacement assemblies and spare/repair parts, engineering drawings, parts lists, process specifications and computer software configuration items. It shall be in the Contractor's own format. The

Contractor PCBL shall support interchangeability and interoperability to a replaceable part level. All baselines shall be documented in the configuration status accounting database.

C.2.3.3. Meetings / Reports: The Contractor shall prepare minutes of all program meetings detailed below in accordance with (IAW) CDRL

A022. The Contractor shall have available a stable drawing base which reflects the current item configuration for use during all meetings held at the Contractor's facility.

C.2.3.3.1. Post Award Conference (PAC): The Government shall coordinate, schedule and conduct a Post Award Conference (PAC) with the

Contractor at the Contractor's facility. The Government anticipates this conference to be conducted within 30 calendar days of the contract award. The purpose of the conference will be the discussion of project orientation, transfer of background information, and contractual requirements. The Contractor shall be prepared to:

a. Conduct a review of the system requirements to ensure that they have been completely and properly identified and that there is a mutual understanding of the system requirements between the Government and the Contractor.

b. Conduct a review of the design to verify its capability to meet this SOW.

c. Make available to Government representative(s) the documentation for production planning, manufacturing methods and controls, material and manpower resource allocation, production engineering, quality control and assurance program, production management organization, and controls over major subcontractors within 30 calendar days after award.

C.2.3.3.2. Logistics Guidance Conference: The contractor shall participate in a Logistics Guidance Conference, the Government anticipates this conference to be conducted within 30 calendar days of the contract award. The purpose of this Conference is to discuss the specified contractual requirements to ensure a common understanding and to clarify any logistics issues.

C.2.3.3.3. In-Process Reviews (IPR): IPRs will be held at the discretion of the Government. During preparation of equipment publications and provisioning documentation, these IPRs will be used to clarify requirements. IPRs are not a part of the Verification Conference and shall not be used to take the place of it. The Government will notify the Contractor 10 business days prior to each IPR. IPRs shall be held at the Contractor's site. The Contractor shall make available adequate space, facilities and personnel for Government scheduled

IPRs at no additional cost to the Government. The Contractor shall be prepared to host IPRs at their facility to review the progress of the effort throughout the contract. IPRs shall be conducted on dates mutually agreed upon between the Government and the Contractor's

Program Manager. The Contractor's PM shall be prepared to brief the program status, schedule and any issues related to contract execution.

C.2.3.4. Incorporation of Proposal: Parts of the Contractor's Technical Proposal, as negotiated and accepted by the Government, may be incorporated by reference into the resultant contract. Some or all of the information furnished by the Contractor may be subject to disclosure under the Freedom of Information Act. For this reason the Contractor shall identify information contained in the proposal that the Contractor specifically does not want to be incorporated by reference. In the event of any conflict or ambiguity between the

Contractor's Technical Proposal and the Government's SOW, the Government's SOW shall govern.

C.2.4. Contract Performance: The LMS contract shall consist of three areas of effort that involve development and delivery of Technical

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Data and Hardware. The areas of effort are:

(1) \*()The design, manufacture, and delivery of three (3) Type I LMS, three (3) Type III LMS, and three (3) Type V LMS for FAT;

(2) Verification and Validation of Technical Data and Hardware; and

(3) LMS Production.

C.2.4.1. Design: The LMS Type I, Type III, and Type V shall be manufactured in accordance with the end item specification ASTM E2377-18 with exceptions cited in this SOW. The use of these documents shall allow for the manufacture of interchangeable components and end items and shall enable spare part re-procurement and logistical support without recourse to the Government.

C.2.4.1.1 Engineering Change Proposal (ECP): The Contractor shall maintain configuration control of the LMS design throughout the life of the contract. The Contractor shall prepare and submit to the Government an ECP for any proposed change to the LMS design once the FAT

Unit and FAT Report are approved by the Government the contractor cannot change the design unless they submit an ECP approved by the government prior to entering the production phase of the contract. Following acceptance of the FAT units, the Contractor shall not alter the design in form, fit or function without prior approval from the Contracting Officer. After acceptance of the FAT units, an ECP shall be prepared and submitted to the Government for any proposed change to the technical drawing package using the Engineering Change

Proposals (Short Form), DD Form 1693. Each ECP shall be numbered consecutively by the Contractor using a three digit number beginning with 001. Revisions to initial submissions of an ECP, submitted either to expand the supporting information or to override the initial submission shall carry the original ECP number, with sequential revision designators R1, R2, etc. ECPs shall be prepared in contractor format; however, at a minimum each ECP shall include the following:

a. Date Prepared

b. Originator Name

c. Title of Change

d. ECP Number

e. Cage Code

f. Class of ECP (Class I for form, fit or function, Class II compatibility and editorial changes)

g. Justification Code (i.e. Interface, Compatibility, Deficiency, etc.)

h. Priority Code (i.e. Emergency, Urgent, Routine)

i. Drawings Affected

j. Configuration Item Nomenclature (i.e. System Designation, Model, P/N)

k. Lowest Assembly Affected (Name of Part)

l. Description of Change

m. Need for Change

n. Effect on Associated Equipment (i.e. Integrated Logistics Support)

o. Production Effectivity (Serial Number at which the proposed change shall occur)

p. Estimated Total Costs/Savings

C.2.4.1.2. Interface Control Drawings: The Contractor shall prepare and deliver one top assembly drawing with parts list comprised of both the Type I LMS and the Type III LMS IAW CDRL A019. The Contractor shall also prepare a separate top assembly drawing with parts list of the Type V LMS only IAW CDRL A020. Both drawings, when combined with the end item specification ASTM E2377-18 with exceptions cited in this SOW and the Governments existing LMS Interface Control Drawing 17-2-0035 (Attachment 0003), shall allow for the manufacture of interchangeable components and end items and shall enable spare part re-procurement and logistical support without recourse to the Government. Design detail shall only be provided to the extent necessary to attain the required interfaces of the end item and performance of each spare/repair part. Drawings of military or commercial standard items, which are adequately covered by existing approved military drawings and/or military or commercial specifications shall not be redrawn and shall be incorporated directly into the drawing package. The interface drawings shall be made available to the Government prior to the start of FAT.

C.2.4.2. First Article Test (FAT) Plans: The Contractor shall provide a separate FAT Plan/Procedures for each LMS variant that describes the Contractors First Article Testing for the Type I LMS (IAW CDRL A010), the Type III LMS (IAW CDRL A011) and the Type V LMS (IAW CDRL

A012). As a minimum, the FAT plans/procedures shall include all of the verifications that are listed in Section 4 of ASTM E2377-18. The

Contractor shall propose a test weight configuration plan which incorporates the full 3,300 lb. payload which is required for FAT on this contract. The Contractor shall submit the test weight configuration plan to the Government for approval prior to the start of FAT.

The test weight configuration plan shall be submitted as part of the FAT Plan. Two FAT Units of each LMS Type may be used to expedite the overall FAT Schedule in accordance with C.2.4.4.; however, all structural tests requiring the test weight payload shall be performed on the primary FAT Unit of each LMS variant. The Contractor must obtain approval from the Government prior to the start of FAT for all

FAT that will be performed on the secondary FAT Unit.

C.2.4.2.1. FAT Plans/Procedures: The Contractor shall provide test plans/procedures that describe the Contractor's First Article Testing for the Type I LMS (IAW CDRL A010), the Type III LMS (IAW CDRL A011), and the Type V LMS (IAW CDRL A012). At a minimum, the FAT plans/procedures shall include all of the verifications that are listed in Table 5 in Section 4 of ASTM E2377-18 with the exception of:

4.2.3.3 Integration

4.2.4 Chemical and Biological (CB) Resistance

4.2.5 Pressurization

4.3.1 Marine Atmosphere

4.3.3.1 Temperature Range

4.3.3.2 Temperature Shock

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4.3.3.4 Sunshine (Ultraviolet Effects)

4.3.3.5 Humidity

4.3.5 Blowing Dust/Sand

4.4.2 Fixed-wing Air Transport Test

4.4.3 Rotary-wing Air Transport (actual flight test portion only)

4.4.5 Fording

For the list of verifications directly above, the Contractor shall be given the opportunity in their proposal to identify and justify the test, demonstration, analysis, inspection or other method of verification of the corresponding requirement listed in Section 3 of

ASTM E2377-18. For the Rotary-wing Air Transport Test, all of the static lift tests must be performed by the Contractor; however, the actual helicopter flight test portion of this requirement can be verified through analysis. All other requirements of Section 3 of ASTM

E2377-18 shall be verified by the actual performance of a First Article Test. For the Electromagnetic Interference (EMI) Tests, the

Government will thoroughly review the Contractor's EMI Testing capabilities. The Government reserves the right to conduct independent verification testing of the FAT Units EMI capabilities at the Redstone Technical Test Center, Redstone Arsenal, AL, or any other location of its choosing. Such testing, if conducted, may be used to determine the acceptability of the Contractor's FAT Units, notwithstanding any other provision in this contract relating to FAT.

C.2.4.3. Build FAT Units: The Contractor shall fabricate three (3) LMS FAT Units of each LMS Type (Type I, Type III, and Type V) which results in a total of nine (9) FAT Units produced under this contract. The test units shall be fabricated in accordance with ASTM E2377-

18 with the exceptions cited herein. The units shall be production representative (i.e. fabricated using all materials, processes, fixtures, and tooling intended for use during the production phase). Each LMS FAT Unit shall be equipped with one (1) Shelter to HMMWV

Mounting Kit and one (1) Pintle Extension Kit which are separately boxed and stored inside the shelter.

C.2.4.3.1. System Safety: The Contractor shall certify that the safety inherent in the design and fabrication of the LMS provided for

FAT is achieved in accordance with industry standards. The Contractor shall establish system safety processes and procedures to integrate hazard identification, assessment, and elimination or control into the product design and production effort required by this contract. MIL-STD-882D may be used as guidance. The Contractor shall perform a comprehensive and detailed evaluation of the safety risk being assumed by the Government through the operation and maintenance of the LMS. The Contractor's evaluation shall identify all safety features and any procedural or design related hazards that may be present in the LMS. In addition, the Contractor shall develop specific controls and precautions that should be followed to prevent personnel injury or death to user/operators or maintainers of the LMS. The

Contractor shall identify all hazardous materials that are used in the design, operation, or maintenance of the LMS and assess why a nonhazardous or less hazardous material could not be used. Health related hazards (e.g., noise, hazardous chemicals, toxic substances), as well as physical hazards, shall be addressed. Any hazards subsequently discovered during production and fielding shall be reduced to acceptable levels or eliminated, and appropriate warnings shall be provided to the Government for incorporation into the TMs by the

Contractor at no additional cost to the Government.

C.2.4.3.2. The results of the Contractor's safety evaluation for the LMS Type I, Type III and Type V shall be submitted to the

Government in a Safety Assessment Report (SAR) in accordance with CDRL A021. Contractor format may be used, but the content shall include the information specified in DI-SAFT-80102C. The hazard list specified in DI-SAFT-80102C shall include the following information for each hazard, at a minimum:

a. Description of the hazard.

b. Initial hazard risk assessment code (see C.2.4.3.3 below).

c. Actions taken or required to eliminate or control the hazard (e.g., design changes, warning or caution signs on the equipment, safe procedures and precautions in technical manuals).

d. Final hazard risk assessment code, which takes into account the control measure.

e. Status of corrective action (i.e., indicate if actions are complete, or identify any remaining Contractor or Government actions necessary to resolve the hazard).

C.2.4.3.3. The hazard risk assessment code for each hazard identified shall be assigned by using the definitions below.

a. Definitions for hazard severity:

(1) Category 1 - Catastrophic: the total destruction of the system, or an injury or occupational illness resulting in a fatality or permanent total disability.

(2) Category 2 - Critical: major system damage requiring system overhaul, or severe injury or occupational illness resulting in a permanent partial disability.

(3) Category 3 - Marginal: minor system damage requiring maintenance that would cause down time beyond the day, minor injury causing loss of time from work beyond the day or shift, or minor occupational illness causing loss from work or disability at any time.

(4) Category 4 - Negligible: system damage, injury or occupational illness less than that specified in categories I, II, and III.

b. Definitions for hazard probability:

(1) Category A - Frequent: likely to occur frequently (continually experienced in the inventory).

(2) Category B - Probable: occur several times (occurs frequently within the inventory).

C.2.4.4. Contractor FAT: The Contractor shall perform FAT IAW the Government approved FAT Plan/Procedures (C.2.4.2). The Contractor shall be required to perform First Article Testing on one (1) Type I LMS, one (1) Type III LMS, and one (1) Type V LMS shelter. The

Contractor may choose to use up to two (2) FAT Units of each type of LMS in order to expedite the overall FAT Schedule. Testing may be split between two of the FAT Units of each LMS Type; however, all structural tests requiring the test weight payload shall be performed

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on the primary FAT Unit of each LMS Type. The Contractor must obtain approval from the Government prior to the start of FAT for all

Tests that will be performed on the secondary FAT Unit. The Government will witness all testing unless a specific waiver to this requirement is granted by the Contracting Officer. The Contractor shall be responsible for coordinating and scheduling all Contractor

FAT utilizing the appropriate commercial or Government owned facilities, equipment and procedures. The FAT shall verify conformance to the requirements in ASTM E2377-18. Any nonconformance shall be corrected by the Contractor at no additional cost to the Government.

C.2.4.5. FAT Reports: The Contractor shall prepare and submit separate FAT Reports, one (1) for the Type I LMS IAW CDRL A013, one (1) for the Type III LMS IAW CDRL A014, and one (1) for the Type V LMS IAW CDRL A015. Each FAT Report must document the results of all

Contractor testing. Upon approval of the FAT Report, the Contractor shall refurbish the FAT units to their pre-test condition to the maximum extent possible. Refurbishment shall include but not be limited to repair of any damage, touch-up or re-painting of the unit, and incorporation of all corrective actions described in the FAT Report.

C.2.4.5.1. Shelter-To-Vehicle Mounting Kit Detailed Drawings: Upon approval of the FAT Reports, the Contractor shall deliver to the

Government detailed drawings for the Shelter-To-Vehicle Mounting Kit IAW CDRL A023. These drawings shall contain all information required to fabricate the mounting kit including all material and component definition. The Contractor shall prepare Level III drawings and parts lists for all mounting kit components and assemblies necessary for stand-alone re-procurement of the full mounting kit as a

Spare/Repair Part through the Defense Logistics Agency (DLA). These drawings, when used for the manufacture of, shall produce a finished part complete with all holes and hardware necessary for installation on the LMS variants. Drawings shall reference a separate finish drawing, and shall not contain specific finish requirements. The Contractor shall provide a master drawing list (drawing tree) so that the Government can determine the location and function of each mounting kit component and its relationship to the next higher assembly.

C.2.4.5.2. Rights In Technical Data: Any and all data submitted by the Contractor pursuant to the requirements of Section C.2.4.5.1 shall be provided with unlimited rights in accordance with the Rights in Technical Data clause of this contract.

C.2.4.6. Production Units

C.2.4.6.1. Production Test Plans and Procedures: The Contractor shall provide a separate Production Test/Inspection Plan for each LMS variant that describes the Contractors Production Testing for the Type I LMS (IAW CDRL A016), the Type III LMS, (IAW CDRL A017) and the

Type V LMS (IAW CDRL A018).

C.2.4.6.2. Production: The Contractor shall fabricate production quantities of the LMS in accordance with ASTM E2377-18 with the exceptions cited herein. The shelters shall include all changes resulting from First Article Testing. The production units shall be tested in accordance with the approved Test Plans and Procedures.

C 2.5 Technical Publications

C.2.5.1 The Contractor shall develop and produce an Operator Manual for the Lightweight Multipurpose Shelter (LMS) (TM XX-XXXX-XXX-13&P)

(CDRL A004). The Contractor shall also submit a Validation Plan and a Validation Report for the Operator Manual (CDRL A005 and A006).

The stated documents shall be developed and produced in accordance with this section, applicable military standards (MIL-STDs) and regulations, and the attached TM Content Selection Matrix (Attachment 0002, Content Selection Matrix). The contractor shall acquire and deliver the copyright releases in writing. The copyright releases shall be written for the Government's use. The contractor shall ensure that the Government has the unlimited right to use, copy, and distribute the images, manuals, technical data and electronic data files delivered under this contract

C.2.5.2 Applicable Documents. The Contractor shall reference other Army Technical Manuals as appropriate throughout the technical manual submissions in accordance with the authority cited in MIL-STD-40051-2C, including all changes, DI-CMAN-80792A, and DI-MISC-

80711A.

C.2.5.3 Publication Requirements. The Contractor shall produce an Operator Manual for the Lightweight Multipurpose Shelter (LMS) (TM XX-

XXXX-XXX-13&P) in accordance with this section C 2.4.7 (CDRL A004) and the appropriate TM Content Selection Matrix (Attachment 0002) in accordance with this SOW. Development of the TM will be supported by a Contractor-managed Validation effort. The Contractor shall develop a Validation Plan and Validation Report for the Operator Manual in accordance with this section C 2.4.7 and (CDRLs A005 and

A006).

C.2.5.4 Technical Manual. The Contractor shall produce an Initial, Second, and Final Reproducible Copy (FRC) Submission of TM XX-XXXX-

XXX-13&P. All submissions must conform to format and content requirements outlined in the applicable military standards and specifications detailed in C.2.5 and requirements detailed in CDRLs A004, A005, and must be fully illustrated, referenced, and have a working table of contents. TMs shall be developed against the Government approved design after the Critical Design Review. Once the design is approved the OEM shall deliver an initial review at 30 percent TM complete (to include TM outline per the Content Selection

Matrix with all work packages identified and at least one complete work-package) a second review at TM 70 percent complete, and at TM

100 percent complete in three phases, validation, verification, and final reproducible copy. Contractor shall base the TM development off outputs of the FMECA, MTA, LORA, and MAC. The contractor shall incorporate all Test Incident Reports during developmental and operational test into the TMs.

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C.2.5.5 TM Content Selection Matrix Compliance. The TM Content Selection Matrix from MIL-STD-40051-2C, (CDRL A004 - Attachment 0002, Content Selection Matrix), shall be used to organize and develop technical manual content. All items marked R in the matrix are required to support the equipment and shall be included in the order established in the matrix. All shaded items shall be included as required to support the equipment. If shaded items are included, they shall be provided in the order established in the matrix. All items marked P in the attached matrix are prohibited and shall not be included in the manual. Submissions with out-of-sequence or prohibited content items will be rejected.

C.2.5.6 Maintenance Allocation Chart (MAC). The Government approved MAC (CDRL A001) will be used for structuring content within the

Operator and Field Maintenance Manual Including Repair Parts and Special Tools List.

C.2.5.7 Illustrations. All technical manual submissions shall be fully illustrated IAW this section and MIL-STD 40051-2C. Digital photography, computer graphics, and line art are acceptable illustration media to support procedural and descriptive text.

C.2.5.8 Photographic Support. The Contractor shall use photographs as required by the Government to ensure text is sufficiently supported with accurate and clear illustration. In producing the TM as outlined in this SOW, the Contractor shall ensure that personnel in photographs, when visible, will be attired in proper and current U.S. Army work/utility uniform. All personnel, when photographed, will be wearing all safety equipment necessary to perform the procedure being illustrated, and will be photographed complying with all safety requirements as specified in the procedural text; to comply with this requirement, photographed personnel may not be depicted wearing watches, rings, or any other visible jewelry.

C.2.5.9 Graphics Worksheet. The Contractor will deliver a graphics worksheet in electronic format (MS-Word or equivalent format) with each submission IAW CDRL A004. This worksheet sequentially lists all graphics used in the technical manual and, as a minimum, will list in tabular format, the following information: Work Package (WP) identification number (see 4.8.9.1. in MIL-STD-40051-2C ), WP sequence number (see 4.8.9.2. in MIL-STD-40051-2C), Figure Number, Figure Title, Unique Illustration Number (see paragraph 7.6 in this SOW), Width in inches (reprowid), Height in inches (reprodep).

C.2.5.10 Delivery Requirements

C.2.5.11 The Contractor shall submit for the initial submission a TM that has content development and task analysis that trace to the logistics support analysis and approved Maintenance Plan. The Operator & Field Maintenance Manual Including Repair Parts and Special

Tools List (-13&P) initial submissions shall be derived from the two-level MAC and shall meet all format and style requirements as detailed in the listed MIL-STD and provided TM Requirements Matrix (Attachment 0002).

C.2.5.11.1 The initial submission shall have at least one fully developed, technically accurate WP must be present in all the applicable publication chapters (Troubleshooting, PMCS, Operator Maintenance, Maintainer Maintenance, RPSTL, and Supporting Information). The fully developed WPs shall have accurate references to the Supporting Information chapter and any other placeholder WPs.