29--Engine Fuel System Comps, Aircraft

NA NSN: 2915-01-113-8523, P/N: 2-300-908-01, PRON: AX3T6125AX, NOUN: Flow Divider, Fuel, Quantity: 41 each plus 2 years 100% option total quantity=123 each, applicable to T-55 (CH-47) Turbine Engine. F.O.B. Source. Delivery to Texarkana, TX 75507-5000. Required delivery is 180 days after award of contract. The approved source are: Honeywell Defense & Space Cage Code 02LU7, and Delavan Incorporate Cage Code 71895. This part must be acquired from a manufacturing source(s) specified on a source control o r selected item drawing as defined by the current version of DoD-STD-100. All offerors must meet prequalification requirements in order to be eligible for award. Firms that recognize and can produce the required item described above are encouraged to id entify themselves. Firms are encouraged to seek source approval in order to compete for future solicitations by accessing the website www.redstone.army.mil/cmo and looking under Qualification Procedures for Aviation Requirements. All responsible sources may submit an offer, which shall be considered by the Agency. The closing date annotated is an estimated date and may be adjusted dependent upon the date of release for solicitation; however, the solicitation will not close prior to the date stated above . Foreign Firms are reminded that all requests for solicitation must be processed through their respective embassies. No telephone request will be accepted. You may mail your request ATTN: AMSAM-AC-LS-C, Pam Myres, Contracting Officer, fax number 256-9 55-7725. NOTES: 23 and 26