| Program Summary |
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| Description |
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General Information
| Document Type: |
Modification to a Previous Notice |
| Solicitation Number: |
FA8104-08-R-0168 |
| Posted Date: |
Feb 29, 2008 |
| Original Response Date: |
Mar 03, 2008 |
| Current Response Date: |
Apr 14, 2008 |
| Original Archive Date: |
Jul 13, 2008 |
| Current Archive Date: |
Jul 13, 2008 |
| Classification Code: |
J -- Maintenance, repair & rebuilding of equipment |
| Set Aside: |
N/A |
| Naics Code: |
336412 -- Aircraft Engine and Engine Parts Manufacturing |
Contracting Office Address
DEPARTMENT OF THE AIR FORCE; 3001 STAFF DR;BLDG 3001 STE 2AH1109B; TINKER AFB; OK; 73145
Description
THIS SYNOPSIS IS MODIFIED TO REFLECT THE EXISTENCE OF F108 MODULE 13/15 QUALIFICATION REQUIREMENTS. ALL INTERESTED VENDORS ARE ADVISED TO CONTACT THE SOURCE DEVELOPMENT OFFICE FOR THE QUALIFICATION REQUIREMENTS. REMANUFACTURE F108-100/200 TURBINE ASSEMBLY (MODULE 13/15) LOW PRESSURE UNION ASSEMBLY SOL FA8104-08-R-0168 PR FD2030-08-03889 OC-ALC/PKA TINKER AFB OK 73145-3015, For additional information contact Billie Kindschuh/PKA/(405) 734-8107. A firm fixed-price Requirements type commercial contract is contemplated with one basic year and 4 (four) one year options for remanufacture of F108/CFM 56-2A/2B Module 13/15. Item 0001: NOUN: Remanufacture F108 Module 13/15 (USAF) Input/Output NSN 2840-01-229-5786PN, P/N: 305-482-301-0 and/or 305-482-302-0, and/or 305-482-303-0. BEQ as follows: 20 EA Basic Year; 20 EA OPT I; 20 EA OPT II; 20 EA OPT III; 20 EA OPT IV. Item 0002: NOUN: Remanufacture F108 Module 13/15 (USN) Input/Output NSN 2840-01-229-5786PN, P/N: 305-482-303-0-2A. BEQ as follows: 3 EA Basic Year; 3 EA OPT I; 3 EA OPT II; 3 EA OPT III; 3 EA OPT IV. Applicable to: F108 Engine, KC-135R Aircraft. Destn: Tinker Air Force Base OK 73145-3032. Item 0003: CEMS Reporting IAW CDRL and DID. Item 0004: AFMC Form 413 Depot Production Maintenance Report IAW CDRL and DID. Item 0005: CAVAF Reporting IAW CDRL and DID. Description: The LP Turbine Rotor and Stator Module is a 4-stage axial-type mechanical assembly composed of both rotating and non-rotating components. These components consist of abradable materials and high strength nickel alloys. The Turbine Frame Module is a structural assembly consisting of a hub and a multisided outer casing connected through slanted struts. It is a weldment composed of a nickel alloy material. Function: The LP Turbine rotor and Stator module converts hot gas pressure and velocity downstream of the HPT into mechanical power to drive the fan rotor and booster assembly. The turbine frame assembly supports the low pressure turbine rotor rear section and provides for engine rear mounting on the airframe. Delivery: Item 0001: 2 EA per month 30 days ARO and receipt of reparable assets. Item 0002: 2 EA per month 30 days ARO and receipt of reparable assets. Qualification requirements: Sources must be qualified prior to being considered for award. Qualification requirements are not available for this acquisition. These qualification requirements apply to line item(s) 0001 and 0002. The approximate solicitation issue date is 01 FEB 2008 and the estimated solicitation response date will be 03 MAR 2008. The anticipated award date will be 21 MAY 2004. RMC: R2Z. History: last buy Nov 03, Chromalloy Component Services Inc., QTY: 20 EA Unit price:
Point of Contact
Billie L Kindschuh, Phone 405-734-8107, Fax 405-734-8106, Email Billie.Kindschuh@tinker.af.mil
Email your questions to Billie Kindschuh at Billie.Kindschuh@tinker.af.mil
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