Questions and Answers.pdf

PDF 100 KB Posted

Attached to
HYDRAULIC POWER UNIT Federal contract opportunity
Solicitation number
80NSSC26939776Q
Issued by
National Aeronautics and Space Administration Shared Services Center

About this file

This is a Questions and Answers document that clarifies key requirements for a federal contract opportunity involving aircraft hydraulic system servicing and testing.

The procurement involves hydraulic system testing and servicing for multiple military aircraft models, specifically F-18, King Air, TG-14, X-59, and T-34. The contractor must provide a power unit capable of testing hydraulic systems installed in aircraft rather than individual components on a test stand. The equipment specifications have been confirmed as a 3-Phase, Soft-Start Electric Motor operating at 480 VAC with 60Hz frequency. This document provides authoritative answers to bidder inquiries and establishes the technical parameters and scope of aircraft models that will require hydraulic system support under this contract.

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Other files attached to HYDRAULIC POWER UNIT, newest first.
File Type Posted
RFQ.pdf PDF
Specs.pdf PDF

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Questions and Answers

1. Is a test stand needed to test the hydraulics on components, or is a power unit needed to test the hydraulic system in an aircraft?

Hydraulics system in an Aircraft

2. What is the exact aircraft model being serviced?

Multiple A/C. F-18, King Air, TG-14, X-59, T-34

3. Can you confirm if the motor specs are: 3-Phase, Soft-Start Electric Motor at 480 VAC (60Hz)?

Motor specs confirmed

File details come from the government source that posted it. Updated .