SOW.pdf

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Attached to
Tronair Cabin Pressure Tester Federal contract opportunity
Solicitation number
80NSSC26932442Q
Issued by
National Aeronautics and Space Administration Shared Services Center

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This is a Statement of Work (SOW) for the procurement of a ground support equipment (GSE) cabin pressure tester device designed to perform cabin pressure tests on small aircraft cockpit volumes, specifically for use with the X-59 aircraft. The device is identified by Part Number 15-7609-6000-FJ and must be of domestic manufacture.

The cabin pressure tester device shall include the following minimum characteristics: air-based working fluid (shop air or self-generated), a built-in flow meter, separate canopy seal and cabin pressurization circuits, rate of climb indication capability for cabin pressure, a cabin supply output port less than 2 inches in diameter, a pressurization range of 0-15 psig, and flow rate measurement capability as low as 10 SCFM. The equipment is to be delivered to NASA Armstrong Flight Research Center with an acceptable lead time of 2-3 months.

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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.

P/N 15-7609-6000-FJ

2. Characteristics, Scope, and Specs The cabin pressure tester device shall have at minimum the following characteristics:

P/N 15-7609-6000-FJ

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 .