SATPC0036237 Tab 04 4 SOW_Redacted.pdf
PDF 153 KB Posted
- Attached to
- Load Cell Monitoring Device Federal contract opportunity
- Solicitation number
- 80NSSC24879786Q
About this file
This document is a Statement of Work (SOW) for a federal contract opportunity to procure a Load Cell Indicator Straight point Wireless Link system with two compatible 2" shackles, with a capacity of 120,000 lbs. / 55t.
The SOW outlines the background, objectives, and detailed requirements for the load cell indicator system, which is needed by NASA to weigh and assess the center of gravity of heavy industrial items such as aircraft parts and science instruments. The system must meet specifications including an aerospace-grade aluminum construction, wireless range, ability to read multiple load cells, and hazardous area certifications. The vendor is responsible for delivering a new calibrated system, providing all related cables and connectors, and furnishing operation/maintenance manuals. Delivery is required by December 30, 2024. This is a Brand Name or Equal To solicitation, set aside for small businesses, with net 30 FOB Destination terms to the NASA Armstrong Flight Research Center in California.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SATPC0036237 Tab 10 Vendor Question and Customer Response.pdf | ||
| SATPC0036237 Tab 10 Vendor Question and Customer Response.pdf | ||
| SATPC0036237 Tab 10 1 RFQ Open Market.pdf |
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Text version
RFP #
STATEMENT OF WORK
Load Cell Indicator Straight point Wireless Link with two compatible 2" Shackles Capacity 120,000 lbs. / 55t
Code 720, Institutional Safety Branch
National Aeronautics and Space Administration Dryden Flight Research Center
RFP/Contract No. SOW Title Date or Version #
Edwards, California
Table of Contents
1.0 Background
2.0 Objectives
3.0 Requirements
4.0 Deliverables
5.0 Period of Performance
6.0 Travel
7.0 Other Special Requirements and Considerations
RFP/Contract No. Load Moment Indicator for Broderson 8K lbs. Mobile Crane, Model IC-35-2B July 31, 2024
1.0 Background
• Load Cell Indicator, straight point, wireless link with two compatible 2" shackles o System capacity 120,000 lbs. / 55t o The Load Cell’s primary function is to weigh or check the load exerted on Lifting Device Equipment (LDE) and to assist in identifying the Center of Gravity (CG) of loads.
o NASA has many industrial-sized aircraft parts, science instruments, and construction projects for which exact weights and CGs are unknown. The “Load Cell” is an industry-standard tool used to assess heavy loads and detraining CG.
o Other load cell indicator applications are “Proof & Load” testing of new & existing LDE at the center.
o The load cell indicators validate LDE equipment safety margins, assist in identify CG, and ensure the center’s compliance with regulatory requirements of NASA-Std, OSHA, and ASME.
3.0 Requirements
Unit shall meet or exceed the following requirements:
• Load Cell, Straight point, wireless link with two compatible 2" shackles
• System Capacity 120,000 lbs. / 55t o Harden anodized aerospace aluminum o Hardened bushes to accept industry standard shackles o Internal Antennae o Environmental protection IP67 or NEMA6 o Angular ends to reduce weight and snagging when rigged
• Load Cell Handheld Remote o Wireless Range (2.4GHz), Range 1000m to 3280ft o Reads up four load cells simultaneously o Low Battery Level o Signal Strength o Audible Overload Alarm 80dB o Multiple Display Units t/lbs./Kg/KN o Bluetooth output and can be connected to any smart phone running SP’s free HHP app on iOS or Android, at ranges up to 100m or 328ft.
o ATEX/IECEx for hazardous areas, zones 0, 1 & 2.
o Providing a wireless range of up to 500m or 1640ft to SW-HHP-ATEX handheld.
Purchase of a new 2024 model or newer
• 2-year parts labor warranty
Delivery Information:
NASA Armstrong Flight Research Center
Bldg. 4876 Warehouse #6, Lilly Drive Edwards AFB, CA 93523
Business hours of AFRC are Monday thru Thursdays 8-to 3pm daily.
4.0 Deliverables
• Vendor is responsible for the delivery of new Load Cell
• Vendor is responsible for ensuring the new Load is calibrated and fully operational to the requirements in Section 3.0 of this document.
• Vendor is responsible for providing all electrical and data communication cabling and connectors associated with the product upon delivery.
• Vender to provide operator, maintenance and calibration manuals
5.0 Period of Performance
• Delivery is required No later than 30 December 2024.
6.0 Travel
• No travel required
7.0 Other Special Requirements and Considerations
• Deliveries shall be scheduled in advance by calling (661) 276-3255.
REVISIONS
Revision Number Date Brief Summary of Changes
Base
| 1.0 Background |
| o The Load Cell’s primary function is to weigh or check the load exerted on Lifting Device Equipment (LDE) and to assist in identifying the Center of Gravity (CG) of loads. |
| o NASA has many industrial-sized aircraft parts, science instruments, and construction projects for which exact weights and CGs are unknown. The “Load Cell” is an industry-standard tool used to assess heavy loads and detraining CG. |
| o Other load cell indicator applications are “Proof & Load” testing of new & existing LDE at the center. |
| o The load cell indicators validate LDE equipment safety margins, assist in identify CG, and ensure the center’s compliance with regulatory requirements of NASA-Std, OSHA, and ASME. |
| 3.0 Requirements |
| 4.0 Deliverables |
| 6.0 Travel |
| 7.0 Other Special Requirements and Considerations |
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