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COMMERCE BUSINESS DAILY ISSUE OF OCTOBER 20,1995 PSA#1456Oc-Alc/Dir Of Contracting/Propulsion, 3001 Staff Dr Ste 1ag81, Tinker
Air Force Base Ok 73145-3032 28 -- DIVERGENT FLAP SOL F34601-96-49448 DUE 120795 POC For copy,
OC-ALC/PKXDA TINKER AFB OK 73145-3015, For additional information
contact Willie Roberts/Lpdpb/(405)739-4346 Item 0001 NSN
2840-01-381-5393PR P/N: 5051M72G09, DIVERGENT FLAP IS A COMPONENT OF
THE EXHAUS NOZZLE. IT IS HINGEDTO THE AF T END OF THE PRIMARY FLAP AT
THE FORWARD END AND IS CONNECTEDTO THE OUTER FLAP WITH SLOTTED CAMSAND
SLIDERS AT THE AFT END. ITS POSITION CONTROLS THE FLOW OF EXHAUST
GASES OUT THE EXHAUST NOZZLE ASSEMBLY. DIMENSIONS ARE: 5 .5 IN. WIDE BY
22 IN. LONG. 2.5 IN. HIGH AT THE TALLEST POINT. MATERIAL; RNE 41 12EA.
Applicable to: F110. Destn: DTK0002. Delivery: 31 OCT 97 12 ea Item
0002 NSN 2840-01-381-5393PR Divergent Flap P/N: 5051M72G09, DIVERGENT
FLAP IS A COMPONENT OF THE EXHAUS NOZZLE. IT IS HINGEDTO THE AF T END
OF THE PRIMARY FLAP AT THE FORWARD END AND IS CONNECTEDTO THE OUTER
FLAP WITH SLOTTED CAMSAND SLIDERS AT THE AFT END. ITS POSITION CONTROLS
THE FLOW OF EXHAUST GASES OUT THE EXHAUST NOZZLE ASSEMBLY. DIMENSIONS
ARE: 5 .5 IN. WIDE BY 22 IN. LONG. 2.5 IN. HIGH AT THE TALLEST POINT.
MATERIAL; RNE 41 102EA. Applicable to: F110. Destn: DTK002. Delivery:
31 OCT 97 102 ea Item 0003 NSN 2840-01-381-5393PR Divergent Flap P/N:
5051M72G09, DIVERGENT FLAP IS A COMPONENT OF THE EXHAUS NOZZLE. IT IS
HINGEDTO THE AF T END OF THE PRIMARY FLAP AT THE FORWARD END AND IS
CONNECTEDTO THE OUTER FLAP WITH SLOTTED CAMSAND SLIDERS AT THE AFT END.
ITS POSITION CONTROLS THE FLOW OF EXHAUST GASES OUT THE EXHAUST NOZZLE
ASSEMBLY. DIMENSIONS ARE: 5 .5 IN. WIDE BY 22 IN. LONG. 2.5 IN. HIGH
AT THE TALLEST POINT. MATERIAL; RNE 41 40EA. Applicable to: F110.
Destn: DGR002. Delivery: 28 NOV 97 40 ea FMS REQUIREMENT The
approximate issue/response date will be 07 Nov 95. To: Aba Industries
Inc, Pinellas Park Fl 34666-9000. To: Electro-Methods Inc, South
Windsor Ct 06074-2422. To: Twigg Corp, Martinsville In 46151-2549. To:
Associated Aerospace Activities Inc, San Leandro Ca 94577-3194. To:
Alloytek Inc, Chadds Ford Pa 19317-0198. First article test required.
No telephone requests. Only written or faxed requests received directly
from the requestor are acceptable. All responsible sources may submit
a bid, proposal, or quotation which shall be considered. Award will be
made only if the offeror, the prodct/service, or the manufacturer
meets qualification requirements at the time of award in accordance
with FAR clause 52.209-1. The solicitation identifies the office where
additional information can be obtained concerning qualification
requirements as cited in each individual solicitation. It is suggested
that small business firms or others interested in subcontracting
opportunities in connection with the described procurement make contact
with the firm(s) listed. Note: While price will be a significant factor
in the evaluation of offers, the final contract award decision may be
based upon a combination of price and past performance factors as
detailed in the solicitation. Note: An Ombudsman has been appointed to
hear concerns from offerors or potential Offerors during the proposal
development phase of this acquisition. The purpose of the Ombudsman is
not to diminish the authority of the program director or contracting
officer, but to communicate contractor concerns, issues, disagreements,
and recommendations to the appropriate government personnel. When
requested, the Ombudsman will maintain strict confidentiality as to
source of the concern. The Ombudsman does not participate in the
evaluation of proposals or in the source selection process. Interested
parties are invited to call the Ombudsman at (405) 736-3273. DO NOT
CALL THIS NUMBER FOR SOLICITATION REQUESTS. Note: Faxed solicitation
requests can be submitted to OC-ALC/PKXDA, Tinker AFB OK 73145-3015,
FAX NUMBER (405)739-5411. See Note (s) 1. (0291) Loren Data Corp. http://www.ld.com (SYN# 0143 19951019\28-0001.SOL)
28 - Engines, Turbines and Components Index Page
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