SOW.pdf
PDF 206 KB Posted
- Attached to
- Tronair Cabin Pressure Tester Federal contract opportunity
- Solicitation number
- 80NSSC26932442Q
About this file
This is a Statement of Work (SOW) for the procurement of ground support equipment (GSE) for NASA Armstrong Flight Research Center.
The primary objective is to obtain a cabin pressure tester device capable of performing cabin pressure tests on small aircraft cockpit volumes, specifically for the X-59 aircraft. The device must utilize air as the working fluid (either shop air or self-generated), include a built-in flow meter, and feature separate canopy seal pressurization and cabin pressurization circuits. The tester must provide rate of climb indication for cabin pressure, maintain a cabin pressurization range of 0-15 psig, accommodate flow rate measurements as low as 10 SCFM, and have a cabin supply output port with a diameter less than 2 inches. The device must be of domestic manufacture. Delivery is required to NASA Armstrong Flight Research Center with an acceptable lead time of 2-3 months.
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Text version
STATEMENT OF WORK
1. Objective / Requirements To obtain a ground support equipment (GSE) cabin pressure tester device used to perform cabin pressure tests on a small aircraft cockpit volume, such as X-59.
2. Characteristics, Scope, and Specs The cabin pressure tester device shall have at minimum the following characteristics:
Working fluid is air, whether shop air or self-generated Built-in flow meter Canopy seal pressurization circuit Cabin pressurization circuit Rate of climb indication for cabin pressure Cabin supply output port of less than 2 inches diameter 0-15 psig cabin pressurization range Flow rate measurement range as low as 10 SCFM Of domestic manufacture
3. Place of Performance
The cabin pressure tester is to be delivered to NASA Armstrong Flight Research Center.
4. Period of Performance Acceptable lead time is 2-3 months.
File details come from the government source that posted it. Updated .