SATPC0039416 Tab 04 SOW-Rigging-Hardware-REV2.pdf
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- Attached to
- Rigging Hardware for HLS MLT
- Solicitation number
- 80NSSC25911966Q
About this file
This Statement of Work (SOW) details NASA's requirements for rigging hardware for the Human Landing Systems Moon Landing Test at the Landing and Impact Research Facility at NASA's Langley Research Center. The document specifies precise hardware requirements from three sole-source manufacturers: The Crosby Group, Green Pin®, and ANYLOAD, with detailed specifications for each item, including:
Crosby Group items include multiple wide body shackles (ranging from 18t to 75t), welded master link assemblies, turnbuckles, and screw pin shackles (totaling 29 pieces). Green Pin® requires 5 sling shackles, and ANYLOAD needs 6 load cells. An additional requirement is for 4 soft shackles with specific strength and diameter specifications. All hardware must be proof load tested at 200% of rated load for 30 seconds and inspected per ASME B30 series standards, with vendors required to provide comprehensive test reports and certifications. The delivery deadline is September 30, 2025, with the solicitation (80NSSC25911966Q) issued by the NASA Langley Research Center, and proposals must strictly adhere to the listed requirements without additional options.
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| SATPC0039416 Tab 12 RFQ Open Market Template 4-18-2024.pdf |
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STATEMENT OF WORK
For Rigging Hardware for HLS MLT
1 Objective 2 Requirements
2.1 Sole Brand – The Crosby Group
2.2 Sole Brand – Green Pin®
2.3 Sole Brand – ANYLOAD
2.4 Remaining Items
3 Shipping Details 4 Period of Performance 5 Proposal Instructions and Additional Information 6 Revisions
1 Objective
The objective of this contract is to obtain lifting hardware for the Human Landing Systems Moon Landing Test at the Landing and Impact Research (LandIR) Facility at NASA’s Langley Research Center.
2 Requirements
NASA requires the following hardware. Part numbers and quantities are provided along with the item name.
NOTE: NASA Requires the hardware test reports and certifications for each individual piece of hardware as outlined below.
2.1 Sole Brand – The Crosby Group
NASA requires the exact parts outlined in the following table manufactured by The Crosby Group. All hardware shall be proof load tested (hold load at 200% of rated load for a minimum of 30 seconds) and then inspect hardware in accordance with appropriate ASME B30 series standard. Vendor shall provide test reports and certifications for each piece of hardware.
# Brief Description Product Details Part Number QTY
2.1.1 Welded Master Link
Assembly
Crosby® Grade 100 A-1345 Welded Master Link Assembly, 147,600 lb WLL
1256973 3
2.1.2 Turnbuckle (37.5t) Crosby® HG-228 Jaw & Jaw Turnbuckles, 37.5 Metric Tonne
1033090 4
2.1.3 Wide Body Shackle
(18t)
Crosby® G-2160 Wide Body Shackle, 18 Metric Tonne
1021274 4
2.1.4 Wide Body Shackle
(30t)
Crosby® G-2160 Wide Body Shackle, 30 Metric Tonne
1021283 3
# Brief Description Product Details Part Number QTY
2.1.5 Wide Body Shackle
(40t)
Crosby® G-2160 Wide Body Shackle, 40 Metric Tonne
1021285 10
2.1.6 Wide Body Shackle
(75t)
Crosby® G-2160 Wide Body Shackle, 75 Metric Tonne
1021290 2
2.1.7 Screw Pin Shackle (35t) Crosby® G-209 Screw Pin Anchor Shackle, 35 Metric
1018650 7
2.2 Sole Brand – Green Pin®
NASA requires the exact parts outlined in the following table manufactured by Green Pin®. All hardware shall be proof load tested (hold load at 200% of rated load for a minimum of 30 seconds) and then inspect hardware in accordance with appropriate ASME B30 series standard. Vendor shall provide test reports and certifications for each piece of hardware.
# Brief Description Product Details Part Number QTY
2.2.1 Sling Shackle BN (40t) Green Pin® Sling Shackle BN - 40 Metric
SLGPF0040 5
2.3 Sole Brand – ANYLOAD
NASA requires the exact parts outlined in the following table manufactured by ANYLOAD Weigh & Measure Inc. All hardware shall be proof load tested (hold load at 200% of rated load for a minimum of 30 seconds) and then inspect hardware in accordance with appropriate ASME B30 series standard. Vendor shall provide test reports, certifications, and calibrations for each individual piece of hardware.
# Brief Description Product Details Part
Number QTY
2.3.1 Load Cell (110 klb) ANYLOAD 110-BH, 50 Metric Tonne Load Cell - 6
2.4 Remaining Items
NASA requires the following items. All hardware certifications shall be provided as part of the shipment.
# Brief Description Product Details Part Number QTY
2.4.1 Soft Shackle (125klb) Equivalent to Tactical Recovery Equipment – Extreme Soft Shackle – 125,000 lb Breaking Strength
• Breaking Strength greater than 90,000 lb
• Shackle thickness: diameter less than 2.4 inches
- 4
• Inside diameter: between 5 inches – 13 inches
• Will not be used for overhead lifting.
3 Shipping Details
Please ship to the following Address
NASA Langley Research Center CO: L. J. Hantsche
MS 495
12 West Bush Road Hampton VA, 23681
4 Period of Performance
All items requested to be delivered by September 30, 2025. If a few items are long lead, please indicate in your proposal.
5 Proposal Instructions and Additional Information
Please only quote the required items listed. If a vendor provides additional options that are not requested by NASA, they will not be considered and may cause the proposal to be disregarded. Please ensure that each requirement is specifically addressed in your proposal.
6 Revisions
Revision Number Date Brief Summary of Changes Base 7/21/2025 Initial Release.
1 7/28/2025 Added NOTE regarding certifications in Section 2.
2 7/31/2025 Clarified NOTE in Section 2.
| 1 Objective |
| 2 Requirements |
| 2.1 Sole Brand – The Crosby Group |
| 2.2 Sole Brand – Green Pin® |
| 2.3 Sole Brand – ANYLOAD |
| 2.4 Remaining Items |
| 3 Shipping Details |
| 4 Period of Performance |
| 5 Proposal Instructions and Additional Information |
| 6 Revisions |
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