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COMMERCE BUSINESS DAILY ISSUE OF MARCH 8,2000 PSA#2552U.S. Army Aviation and Missile Command, Acquisition Center, Bldg 4488,
Redstone Arsenal, AL 35898-5280 15 -- STRUT ASSEMBLY, ENGINE SOL DAAH23-00-B-0034 DUE 042400 POC James
Lang, (256) 955-9237, or 955-9196 Due to a change in acquisition
strategy, the previously released Presolicitation Notice, identified as
CBD Submission Number 431038, is hereby changed as follows: Agency
Solicitation Number DAAH23-00-R-0419 is replaced by Agency Solicitation
Number DAAH23-00-B-0034. All other aspects of the procurement action
remain unchanged. The new synopsis narrative is shown below: SYNOPSIS:
Invitation for Bids (IFB) Number: DAAH23-00-B-0034; PRON: AX0F0095AX;
NSN: 1560-01-158-5815; Quantity: 430 each; Part Number:
70305-02105-043, STDP Revision C; Noun: Strut Assembly, Engine; SIC
Code: 3728; Business Size Standard: 1000 employees; Closing Date: 2000
April 24; Applicable to the UH-60 Aircraft. Deliveries are F.O.B.
Destination to New Cumberland, PA. Required delivery with First Article
Testing (FAT) is 215 each 333 Days After Contract Award (DACA), and 215
each per month thereafter until delivery is complete, First Article
Test Report (FATR) due 198 DACA. Required delivery without FAT is 215
each 210 DACA, and 215 each per month thereafter until delivery is
complete. Point of Contact: James Lang, Telefax: (256) 955-9237, or
955-9196; Office: AMSAM-AC-AL-C. This is a 100% Small Business
Set-Aside procurement. To obtain this solicitation package, send a
telefax to the person shown above, being sure to include company name,
address, telephone number, and solicitation/IFB number. The Government
has rights to the technical data, the data package is complete, and
there are no technical data, engineering, tooling, or manufacturing
restrictions. Item Number 0001AA requires two bids, (1) Bid A, with
First Article Test Report (FATR), and (2) Bid B, No FATR required. See
Number Notes 1, 22, 23, and 26. Posted 03/06/00 (W-SN431315). (0066) Loren Data Corp. http://www.ld.com (SYN# 0157 20000308\15-0001.SOL)
15 - Aircraft and Airframe Structural Components Index Page
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