RB-M Engine Container SOW FINAL.docx

Statement Of Work (SOW) Response Boat-Medium (RB-M) Engine Assembly Long Life Reusable Containers (LLRCs) HSCG23-12-R-PAP058 Attachment 1 7/24/2012

Table of Contents

Section Description Page

1.0 Purpose

1.1 The U.S. Coast Guard (USCG) RB-M asset line requires LLRCs to be developed and provided for the storage of the RB-M engine assembly. Upon completion of the efforts described herein, the new LLRCs will be introduced to the USCG inventory for the spare and repair part packaging, handling, storage, and transportability requirements of the RB-M Engine Assembly. The Government requirements of the container are contained in Society of Automotive Engineers (SAE®) Aerospace Recommended Practice (ARP) 1967A (section 2.1) with the exceptions listed in section 6 of this document.

1.2 The Nomenclature, Part Number (PN), Commercial And Government Entity (CAGE) and National Stock Number (NSN) of the item(s) to be containerized:

1.2.1 Nomenclature: Engine, RB-M (MTU 60 Series DDEC IV Engine)

1.2.1.1 The engine assembly consists of the MTU engine coupled with Marine Gear (Twin Disc Reduction Gear), PN MG-5114SC, CAGE 61208, NSN 3010-01-590-4163

1.2.2 PN: Port (Left) Side- 6062HK30, Starboard (Right) Side- 6062HK31.

1.2.3 CAGE: Port (Left) Side- 72582, Starboard (Right) Side- 72582

1.2.4 NSN: Port (Left) Side- 2895-01-590-7317, Starboard (Right) Side- 2895-01-590-7303

1.2.5 Engine Assembly Dimensions (Length, Width and Height) and Weight:

2.0 Applicable Documents

2.1 Society of Automotive Engineers (SAE®) Aerospace Recommended Practice (ARP) 1967A- The LLRC shall be developed in accordance with SAE® ARP 1967A and this SOW. SAE® ARP 1967A will not be provided by the USCG. Interested parties are responsible for obtaining this specification at their cost. Section 6 of this SOW addresses revisions and exceptions to SAE® ARP 1967A.

2.2 RB-M Engine Assembly Drawing 45-RB-M-084-003 will be available to interested parties as an attachment to the solicitation.

2.3 Department of the Army Technical Bulletin (TB) 9-289, Reconditioning of Type I and Type II Reusable Metal Containers- will be made available to interested parties as an attachment to the solicitation.

2.4 ASME-Y14.100 and ASME-Y14.5M and ASME Y14.24- will not be provided by the USCG. Interested parties are responsible for obtaining these specifications at their cost.

2.5 USCG Commandant Instruction 4130.6A, CG CM Policy- will be made available to interested parties as an attachment to the solicitation.

3.0 Specific Tasks

3.1 LLRC Development- The LLRC for the RB-M Engine Assembly shall be in accordance with SAE® ARP 1967A. Exceptions from this practice are noted in section 6. In developing the LLRC, the contractor is responsible for all planning, development, designing, prototype construction, validations, and any other work involved with providing a USCG approved LLRC.

3.1.1. This container shall:

3.1.1.1 Only be fabricated from steel, aluminum or composite material and must be corrosion resistant (either inherently or through the use of protective coatings). The use of wood in the design and fabrication of this reusable container is forbidden except for the container skids.

3.1.1.2 As required, incorporate energy absorbing systems, dehumidification systems and other special features to ensure protection of the item.

3.1.1.3 Be capable of being repaired and/or retrofitted to prolong container service life or modification to adapt the reusable container for shipment of items other than for which it was originally intended. Department of the Army Technical Bulletin (TB) 9-289, Reconditioning of Type I and Type II Reusable Metal Containers shall be used as a guide.

3.1.1.4 Have a minimum size consistent with the size of the contents and the performance requirements of SAE® ARP 1967A. During the life of the LLRC, it will experience multi-modal transportation (truck, rail, air and ocean movement), so size considerations shall include all modes of transportation.

3.1.1.5 Account for the engine assembly mounts. The government will provide drawing 45-RB-M-084-003 detailing the engine mount locations.

3.1.2 The contractor shall develop a design plan that requires USCG approval prior to the construction of the LLRC.

3.1.2.1 The design plan shall be in electronic format as an editable AutoCAD® 2009 drawing package or an AutoCAD® 2009 compatible 3-D model.

3.1.2.2 The design plan shall include engineering drawings and associated parts and materials lists, in sufficient detail to provide the USCG the ability to procure the LLRC in the future.

3.1.2.2.1 The Engineering drawings shall comply with the most recent versions of ASME-Y14.100 and ASME-Y14.5M and ASME Y14.24.

3.1.2.2.2 Configuration Management (CM) data shall comply with USCG Commandant Instruction 4130.6A, CG CM Policy. Electronic drawing file format shall be submitted in AutoCAD® 2009.

3.1.3 The contractor shall submit their LLRC design plan to the USCG. The USCG will approve or require changes to the submitted LLRC design plan.

3.1.4. After the contractor receives USCG approval of their LLRC design plan, the contractor shall being the first article construction.

3.1.5 After first article construction, the contractor shall conduct a first article test (FAT) IAW SAE® ARP 1967A.

3.1.6 The contractor shall receive first article acceptance from the USCG at the contractor’s site. The contractor shall not start construction of the remaining LLRCs until they receive first article acceptance from the USCG.

3.2 Construction and Delivery of LLRCs

3.2.1 The contractor shall start construction of the 27 remaining LLRCs after receiving USCG first article acceptance. The contractor shall provide 28 LLRCs total, 1 first article and then 27 more.

3.2.2 The contractor shall provide delivery of the LLRCs IAW section 5 of this SOW and the delivery schedule below (subject to change prior to award of contract):

4.0 Deliverables

4.1 Design plan- NLT 15 days after date of contract award.

4.2 Engineering data in section 3.1.2.2- Due with the design plan

4.3 First article- NLT 30 days after USCG design plan approval

4.4 Remaining 27 LLRCs- IAW section 3.2.2

5.0 Delivery, Packaging, and Marking Requirements

5.1 Delivery shall be FOB destination to:

U.S. Coast Guard Surface Forces Logistics Center Receiving Department, Bldg # 88 2401 Hawkins Point Road Baltimore, MD 21226-1797

(410) 762-6353

OR

Inland Power Group Attn: Gerry Dolphin 13015 W. Custer Avenue Butler, WI 53007-0500

(262) 783-8717

5.2 Delivery schedule shall be IAW section 3.2.2.

5.3 Marking is governed by MIL-STDs-129P and -130N (cited in SAE® ARP 1967A), and other marking requirements in SAE® ARP 1967A as applicable.

6.0 Revisions and Exceptions to SAE® ARP 1967A

The following addresses Section 6, Ordering Data, of the SAE® ARP 1967A specification:

a. SAE® ARP 1967A

b. RB-M Engine Assembly as specified in Section 1.0 of this SOW.

c. Applicable drawing: 45-RB-M-084-003

d. 28 containers

e. FAT to be performed at contractor/vendor facility

f. N/A

g. Yes; no prototype required.

h. Yes; First Article required.

i. Primary construction material described in Section 2.0 of this SOW.

j. Parts/surfaces that shall not be plated or painted are gasket sealing surfaces, pressure relief valves and humidity indicators per Section 3.2.1.

k. Type and level of detail required in drawings shall be as described in Section 4.0 of this SOW.

l. No

m. 110+ Gs Fragility Factor per MIL-STD-2073-1;mass proprieties 4,054 lb m per Section 1.0 of this SOW.

n. N/A

o. Fasteners: Non-captive nuts/bolts per Section 3.3.3.2.1.c.

p. Pressure/vacuum per Section 3.3.3.2.2.

q. Maximum assembly/disassembly time shall be 2 man-hours per Section 3.3.3.2.3.

r. Handling provisions required are Sections 3.3.4.1-3.3.4.3. and 3.3.4.5.

s. Lifting rings shall be a minimum of 2.5”/64mm Inside Diameter per Sections 3.3.4.1. and 3.3.4.2.

t. No unitized load requirements.

u. Lifting provision shall be on container base per Section 3.3.4.1.1.

v. N/A

w. N/A

x. N/A

y. Only fully enclosed fork tine pockets are required per Section 3.3.4.5.

z. No.

aa. An alternate desiccant port is acceptable, provided it permits full replenishment of desiccant material.

ab. Humidity indicator per Section 3.3.5.2.

ac. No.

ad. N/A

ae. Yes, per Section 3.3.5.5.

af. Yes, per Section 3.3.5.8.

ag. N/A

ah. N/A

ai. Finishing shall be as described in Section 3.7.1.

aj. Finish and color shall be as described in Section 3.7.2., with the exception of the exterior, which shall be Camouflage Gray, Color Number 36170, per the most recent version of FED-STD-595.

ak. No CARC painting is required.

al. No.

am. A data plate is required per Section 3.10.1.

an. No.

ao. Yes. The TDP will include product drawings/data and production specifications (including a Bill Of Materials), per ASME Y14.100, ASME Y14.5M and ASME Y14.24. Production level AND MONO DETAIL DRAWINGS are also required per Section 3.12.

ap. Yes, FAT will be will be used for qualification test and for validation and verification, per Section 4.2.2.

aq. The following data items in Section 4.3.1. are required:

4.3.1.d.

4.3.1.e.

4.3.1.f

ar. No dynamic analysis as described in Section 4.3.1.c. is required.

as. No high and low temperature testing as described in Section 4.5.3. is required.

at. Distribution Cycle 18, Assurance Level I shall apply to the following Sections only: 4.5.7.1., 4.5.8.3.1. and 4.5.8.3.2. Tests in Sections 4.5.3.1., 4.5.3.2., 4.5.3.3., 4.5.3.4., 4.5.4., 4.5.5. and 4.5.6. shall not be conducted.

au. No 18” drop required.

av. No tipover test required.

aw. No overpack required.

ax. No special accessories

ay. No.