MODIFICATION
95 -- ENGINE SECTION TEST - UPPER SPIDER ASSEMBLY
- Notice Date
- 8/25/2014
- Notice Type
- Modification/Amendment
- NAICS
- 332312
— Fabricated Structural Metal Manufacturing
- Contracting Office
- NASA/George C. Marshall Space Flight Center, Procurement Office, Marshall SpaceFlight Center, AL 35812
- ZIP Code
- 35812
- Solicitation Number
- NNM14520350Q
- Response Due
- 9/2/2014
- Archive Date
- 8/25/2015
- Point of Contact
- Andrea Tobias, Contract Specialist, Phone 256-544-7519, Fax 256-544-9081, Email andrea.b.tobias@nasa.gov - Artra C House, Contracting Officer, Phone 256-544-3507, Fax 256-544-6560, Email artra.c.house@nasa.gov
- E-Mail Address
-
Andrea Tobias
(andrea.b.tobias@nasa.gov)
- Small Business Set-Aside
- N/A
- Description
- THIS NOTICE CONSTITUTES AMENDMENT NO. 02 TO THE COMBINED SYNOPSIS/RFQ FOR ENGINE SECTION TEST - UPPER SPIDER ASSEMBLY. Companies shall acknowledge all amendment(s) in their quote. This notice serves as the official amendment to subject synopsis/RFQ and a written amendment will not be issued. The purpose of this amendment is to provide Questions and Answers, correct an acronym reference, and extend the due date of offers. The Questions and Answers are as follows: 1Q: Would a flatness of.25 be possible on the 16 bottom pads without machining? The drawing states no machining in that area. 1A: Since the parts are to be matched drilled, it was intended that the surface be used as a basis for lining up the mating weldments.For example, FN-2 being mated to the four FN-3s.Each pad is resting on this surface. It would be expected that FN-2 would be supported so its beams would be as inline and parallel to the surface as feasible to aid in the remaining fit up with FN-3s and to reduce shim production. The three pads of each FN-4 would similarly rest on the surface during fit up. 2Q: Does a flatness tolerance of.25 which is called for on the bottom flange of the W36 x 441 beams on drawing 90M14149, sheet 2, apply to every beam, the entire flange of every beam, or just a certain area ? 2A: The solicitation provides the tolerances for every beam similarly, jigged as Item 1. 3Q: Will connections for all locations required, as per the drawings have match drilling of mating parts? 3A: Per drawing 90M13931, note 5, holes can be match marked, then drilled separately. Special jigs/equipment may be necessary to achieve some holes, however, due to stress constraints these holes must be in their current locations. Acronym correction is: all references to "UTF" should read "UTS", for Ultimate Tensile Strength. The due date for receipt of offers is extended to September 2, 2014. Companies shall provide the information stated in the synopsis/RFQ posted on the NASA Acquisition Internet Service (NAIS) on September 2, 2014. Documents related to this procurement are available over the Internet. These documents reside on a World Wide Web (WWW) server which may be accessed using a WWW browser application. The Internet site, or URL, for the NASA/MSFC Business Opportunities home page is http://prod.nais.nasa.gov/cgi-bin/eps/bizops.cgi?gr=D&pin=62
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/NASA/GMSFC/POVA/NNM14520350Q/listing.html)
- Record
- SN03478754-W 20140827/140825235608-e5eb06b06cec52de0b83e87bf33e7e34 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
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