Attachment 1 - SOW Manikin Replacement Parts.pdf

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Statement of Work for

Manikin Replacement Parts at the

704th Test Group/846th Test Squadron

26 January 2026

1.0 PURPOSE

The 846 TS operates the Holloman High Speed Test Track (HHSTT) and performs rocket sled testing of USAF aircraft emergency escape sytems using mechanical surrogates known as biofidelic instrumented anthropomorphic test devices (ATDs, or “manikins”) in the place of live aircrew. The two main types of manikins used are Joint Primary Aircraft Training System (JPATS) Case-1 Reduced Weight, also known as the Lightest Occupant in Service (LOIS) weighing 103 lb and the JPATS Case-6, also known as the Large Anthropomorphic Research Dummy (LARD) weighing 245 lb. These are custom-made manikins which have specific anthropometry and mass properties of individual body parts and limb segments. Because the LOIS and LARD ATDs are custom-made for the Department of War (DoW), most replacement parts are not commercially available off-the-shelf.

The DoW requires using ATDs with sled testing for the qualification of egress systems and other aircrew equipment prior to fielding, in accordance with the Crew Systems Engineering Bulletin EZFC-CSB-16-001 (Revision of MIL-HDBK-516C Airworthiness Certification Criteria, AFLCMC/Crew Systems Engineering, 28 November 2016).

As expected, these HHSTT manikins have parts that break during the execution of these particularly severe escape system tests. This document explains the requirements for purchase of unique replacement manikin mechanical parts designed and manufactured by Humanetics Innovative Solutions, Inc. (“Humanetics”) that will return two particular manikins (LOIS-9 and LARD-23) back to service after they were damaged in egress testing (see tables-1 and -2 for required parts listing description and quantities). Part numbers in tables-1 and -2 are proprietary Humanetics part numbers for LOIS and LARD manikins, of the same type contained in the manikin assemblies recently delivered under contract# FA860624CB002, ATD Solution.

1.1 LOIS Part Numbers, Descriptions and Quantities:

Table 1: Required LOIS Parts Humanetics Item Part Number

Description Unit Quantity

880105-439-FT FEMUR ASSEMBLY, MACHINED, RIGHT EA 1

200-4901-2-PR FEMUR COVER, RIGHT, LOIS EA 1

5001054-FT SCREW LHCS M4 X 0.7 X 12 EA 1

240-6110-H UPPER ARM MOLDED ASSEMBLY EA 1

240-6510-H LOWER ARM ASSEMBLY, MOLDED EA 1

240-6150 UPPER ARM LOWER PART EA 1

880105-344-DN RUBBER STOP ASSEMBLY EA 1

880105-717-DN LOWER ARM STOP ASSEMBLY EA 2

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1.2 LARD Part Numbers, Descriptions and Quantities:

Table 2: Required LARD Parts

Item Part Number Description Unit Quantity

78051-198-DN STOP ASSEMBLY LOWER ARM EA 4

190-6510-H LOWER ARM MOLDED ASSY EA 1

890520-0611-FT OUTBOARD ASSY,STRUCTURAL REPLACEMNT KNEE EA 1

190-102 CAP SKIN JSF-LM110 EA 1

79051-34-H ROTATION STOP COVER EA 1

2.0 SCOPE

The Contractor shall deliver the manikin parts listed in table-1 and table-2 in section 1.0 above. These parts will meet the following minimum requirements: .

2.1 Mechanical Requirements:

2.1.1 Parts will have the proper dimensions, weight, center of gravity, hardness, and biofidelity (if applicable) as defined by 711 HPW/RH, AFLCMC/ROU, AFLCMC/EZFC and 704 TG/846 TS and implemented for production by Humanetics via their manufacturing process specifications for JPATS-based LOIS and LARD entire manikin assemblies (see contract# FA860624CB002).

2.1.2 Parts will have the same characteristics (enumerated in 2.1.1), which were previously characterized and verified by 711 HPW/RH. .

2.2 Documentation and Support:

2.2.1 Parts illustrations and nomenclature will be included in the exploded assembly diagrams contained with the LOIS and LARD product manuals.

2.2.2 Parts handling, installation procedure and maintenance details (if applicable) as described in the LOIS and LARD product manuals.

3.0 MILESTONES

The contractor shall deliver the prescribed manikin parts within 20 to 24 weeks (or better) after receiving the order.

4.0 DELIVERABLES

The contractor shall deliver all hardware and documentation to 846 TS/TGTMI, Attn: Timothy Gros, at 1521 Test Track Road, building 1179, Holloman Air Force Base, New Mexico 88330-7850.