SATPC0040493 Tab 04 4 SOW.pdf
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- Solicitation number
- 80NSSC26926483Q
About this file
This is a Statement of Work for the procurement of an aircraft weighing system for NASA Langley Research Center. The objective is to provide a means of weighing the NASA Langley Boeing 777 aircraft in compliance with Boeing Continuing Airworthiness requirements and NASA procedures.
The vendor must deliver an aircraft weighing system that is capable of weighing a Boeing 777 aircraft up to 480,000 pounds. The system shall incorporate jacks with load cells that enable weighing functionality while also allowing the jacks to lift aircraft axles to facilitate maintenance operations such as tire changes. The system must be powered by either 120V AC power and/or standard shop air not exceeding 120 psi. The vendor is responsible for delivering the complete weighing system to NASA Langley Research Center no later than July 1, 2026. This is a tool procurement only with no on-site performance requirements beyond system delivery.
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Other files
| File | Type | Posted |
|---|---|---|
| SATPC0040493 Tab 07 Capability Statement.pdf | ||
| SATPC0040493 Tab 04 4 SPECS.pdf | ||
| SATPC0040493 Tab 06 RDSS..pdf |
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STATEMENT OF WORK
1. Objective/Requirements To comply with Boeing Continuing Airworthiness requirements and NASA Procedures, a means of weighing the NASA Langley Boeing 777 aircraft is required.
2. Characteristics, Scope, and Specs
The vendor shall provide an aircraft weighing systems that meets or exceeds the following:
a) Capable of weighing a Boeing 777 aircraft up to 480,000 lbs
b) Use of jacks w/ load cells that allow for weighing but can also be used to lift an aircraft axle to facilitate other maintenance (e.g. tire change)
c) Powered by 120V AC power and/or standard shop air not to exceed 120 psi.
The vendor shall deliver the weighing system to NASA Langley Research Center.
3. Place of Performance Not applicable. Tool procurement only
4. Period of Performance
Delivery of weighing system no later than July 1, 2026.
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