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COMMERCE BUSINESS DAILY ISSUE OF JANUARY 8,1996 PSA#1505U.S. Army Aviation and Troop Command, 4300 Goodfellow Blvd., St. Louis,
MO 63120-1798 16 -- BLADE, ROTARY RUDDER SOL DAAJ09-96-Q-0486 DUE 022996 POC Point
of contact is Mr. Mike Perez, A/C 314-263-0564, datafax A/C 314
263-9012. Contracting Officer is Ms. Ruth M. Williams, A/C 314-263
0796. NSN: 1615-01-312-2387, P/N: 7-311422050-7, Qty: 192 each, in
accordance with McDonnell Douglas Helicopter Systems technical data,
applicable to the AH-64 aircraft. FOB Origin with delivery of 96 each
to Red River Army Depot, Texarkana, TX; 48 each to Defense Distribution
Region West, Lathrop, CA; and 48 each to Defense Distribution Depot
Susquehanna, New Cumberland, PA. This procurement requires
prequalification. Contractors who desire to be prequalified must submit
qualification documentation in accordance with procedures contained in
Section I of the solicitation. This proposed contract action is for
supplies for which the Government does not own specifications or
drawings. It is restricted to the following approved and tested source:
McDonnell Douglas Helicopter Systems, Mesa, AZ. Engineering and fatigue
testing are required for this flight safety part. Only approved sources
who have passed fatigue and engineering testing requirements will be
considered eligible for award. Firms that recognize and can produce the
required item described above are encouraged to identify themselves to
the Contracting Officer and provide supporting evidence which will
permit their participation in the current or future solicitations. All
responsible sources are encouraged to submit a proposal which shall be
considered by the Agency. This requirement is being procured under the
authority of 10 U.S.C. 2304(c)(1), Only One Responsible Source or Only
a Limited Number of Responsible Sources and No Other Supplies or
Services Will Satisfy the Agency Requirement. See Notes 12 and 22.
(0004) Loren Data Corp. http://www.ld.com (SYN# 0133 19960105\16-0001.SOL)
16 - Aircraft Components and Accessories Index Page
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