COMMERCE BUSINESS DAILY ISSUE OF JUNE 6, 2001 PSA #2866
SOLICITATIONS
28 -- 220E ENGINE UPGRADE PROGRAM
- Notice Date
- June 4, 2001
- Contracting Office
- 2145 Monahan Way Wright-Patterson AFB OH, 45433-7017
- ZIP Code
- 45433-7017
- Solicitation Number
- 220E_UPGRADE
- Response Due
- June 18, 2001
- Point of Contact
- Julie K. Hall,(937) 255-3507 x3004
- E-Mail Address
- Julie.Hall@wpafb.af.mil (Julie.Hall@wpafb.af.mil)
- Description
- Background "Solicitation notice, Propulsion Development Systems Office (DSO), Attn: ASC/LPKB. -220E Engine Upgrade Program. The Propulsion DSO is seeking sources for acquisition of F100- PW-220 Equivalent (-220E) engine upgrade kits. Contractor must provide fully developed and tested modification kits or Maintenance Upgrade Packages (MUPs) required to upgrade United States Air Force (USAF) F-15 aircraft F100-PW-100 engines (-100), USAF F-16 aircraft F100-PW-200 (-200) engines, and Foreign Military Sales (FMS) and European Participating Government (EPG) -100/-200 engines to an F100- PW-220 Equivalent (-220E) configuration. To be considered responsive, contractors must indicate their capability to start deliveries of the below-listed MUP kits no later than October 2002. Due to a Congressionally mandated requirement, in order to procure the F100/-220E engine kits, the USAF must include a warranty in the contract on the reliability of the complete engine. The F100-PW-100, F100-PW-200, and F100-PW-220E engines are designed and manufactured by Pratt & Whitney of East Hartford Connecticut. The Government anticipates extending the current five year, $485M contract ceiling, firm fixed price, indefinite delivery indefinite quantity Contract F33657-97-D-2013, dated 26 Jun 97, by seven years and increasing the contract ceiling to $833M. Contract F33657- 97-D-2013 was awarded via other than full and open competition to Pratt & Whitney of East Hartford, Connecticut and was a follow-on to Contract F41608-90-D- 1538, dated 28 Sep 90. The -220E upgrade capitalizes on the significant technological advances associated with the -220 engine. In addition to being more reliable, maintainable and durable; the -220E upgrade provides an improved margin of flight safety and unrestricted throttle movement through the flight envelope for both F-15 and F-16 aircraft. The -220E upgrade is accomplished by upgrade of essentially the entire engine, to include inlet fan, core, fan-drive turbine, augmentor, selected external components, outer fan ducts and installation of an enhanced digital electronic engine control system. The USAF will award a single contract/contract extension for the -220E upgrade program which consists of the following MUP kits and National Stock Numbers: MUP 1, Engine Assembly Upgrade Kit, 2840K0214742APT; MUP 1A, Engine Assembly Upgrade Kit, 2840K0214742WPT; MUP 2, Inlet Fan Upgrade, 2840K0214767APT; MUP 2A, Inlet Fan Mod, 2840K0214767BPT; MUP 2B, Redesigned CIVV SQ Drive, 2840K0214767CPT; MUP 2C, Inlet Fan Upgrade Kit, 2840K0214767DPT; MUP 2D, 3rd Stage Fan Blade Kit, 2840K0214767EPT; MUP 3, Core Mod Upgrade, 2840K0214771APT; MUP 3A, Fuel Manifold Kit, 2840K0214771BPT; MUP 3B, Fuel Manifold ""J"" Bracket Kit, 2840K0214771CPT; MUP 3C, Fuel Manifold Kit (Gold Nickel), 2840K0214771DPT; MUP 3D, RCVV Bracket Axial Stop, Brackets/Pump Handle Kit, 2840K0214771EPT; MUP 3E, Fuel Nozzle Kit, 2840K0217492CPT; MUP 3F, Bleed Rod Kit, 2840K0217457APT; MUP 3G, Intermediate Case Kit For Core Mod Upgrade, 2840K0214771FPT; MUP 4, Fan Drive Turbine Upgrade Kit, 2840K0214775CPT; MUP 4A, FTIT Vane Kit, 2840K0214775DPT; MUP 4B, FDT Upgrade Kit (Redesigned Hardware), 2840K0214775EPT; MUP 6, Front Fan Reop Kit (Honey Comb), 2840K0214761APT; MUP 6A, Front Fan Duct Chem Milled Kit, 2840K0214761DPT; MUP 7, Rear Fan Duct Reop Kit (Honey Comb), 2840K0214760APT; MUP 7A, Rear Fan Duct Chem Milled Kit, 2840K0214760IPT; MUP 9, Flame Holder Reop, 2840K0214762APT; MUP 10, Exciter Reop Kit, 2925K0801567APT; MUP 11, Aug. Nozzle Act. Reop Kit, 2915K1600777APT; MUP 12, Aug Fuel Pump Re0p Kit, 2915K0602834APT; MUP 13, Mfgp Reop Kit (Canted Filter, F15 & F16), 2915K0602833APT; MUP 14, FDT Case Reop Kit, 2840K0214772APT; MUP 4C, Rear Turbine Case, 2840k0214775GPT; MUP 16, F-15, Ejector Cooling Kit, 2840K0214766APT; MUP 17, No. 2 Bearing Seal Kit, 2840K0214572APT; MUP 18, Fan Exit Guide Vane Reop Kit, 2840K0214165BPT; MUP 19, P & D Valve Reop Kit, 2840K0214165CPT; MUP 21A, Baseline Kit, 2840K0214742GPT; MUP 21B, Baseline Kit, 2840K0214742XPT; MUP 21C, No.5 Bearing Post Shutdown Kit, 2840K0214742YPT; MUP 27A, Nomex Cables /Attaching Hardware Kit, 2840K0214742ZPT; MUP 28, Aug. Duct Reop Kit, 2840K0214778BPT; MUP 28A, Aug. Duct Finger Seal Kit, 2840K0214778EPT; MUP 28B, Aug. Convergent Nozzle Segment Seal Kit, 2840K0214778FPT; MUP 28C, Mod Augmentor Nozzle 4k (New), 2840K0214778GPT; MUP 28D, Mod Augmentor Nozzle 4k (Composite), 2840K0214778IPT; MUP 28E, Mod Augmentor Nozzle 4k (Max Reop), 2840K0214778HPT; MUP 28F, Parts Augmentor Actuator 4k (Rebuild), 2840K0214778JPT; MUP 28G, Parts Augmentor Actuator 4k (Expendable), 2840K0214778KPT; MUP 28H, Mod Augmentor Divergent Seal 4k, 2840K0214778LPT; MUP 28I, Mod Augmentor External Nozzle Segment 4K, 2840K0214778MPT; MUP 28J, Parts Augmentor Misc. 4K, 2840K0214778NPT; MUP 28K, Mod Augmentor Liner 4K, 2840K0214778OPT; MUP 28L, Mod Augmentor Nozzle Support, 2840K0214778PPT; MUP 28M, Mod Augmentor Balance, Divergent Segment 4K, 2840K0214778QPT; MUP 28N, Augmentor Nozzle Support 4K Upgrade Kit, 2840K0214778RPT; MUP 280, Augmentor Module Chem-Milled Duct Installation Kit, 2840K0214778SPT; MUP 28P, Augmentor Conv. Seg. Liner Kit (4K Aug), 2840K0214778UPT; MUP 28Q, Augmentor Nozzle Hardware (4K) Upgrade Kit, 2840K0214778VPT; MUP 29, Aug. Liner Reop Kit, 2840K0214778CPT; MUP 30, Aug. Duct Assembly Kit, 2840K0214778DPT; MUP 32, F-15 Fuel Pump Filter, 2915K0602833BPT; MUP 33B, Sprayrings/Flameholder Kit, 2840K0214742VPT; MUP 33C, Sprayrings Hardware Kit, 2840K0214742NPT; MUP 35, Sprayrings/Attaching Hardware Kit, 2840K0214742MPT; MUP 36, Intermediate Level Kit (Support Equip.), 2840K0214765APT; MUP 36A, Intermediate Level Kit, (SE-FMS), 2840K0214765CPT; MUP 36B, 4K Fan Drive Turbine Support Equipment (JEIM), 2840K0214765EPT; MUP 37, Organizational Level Kit (Support Equip.), 2850K0214765BPT; and MUP 37A, Organizational Level Kit, (SE-FMS), 2840K0214765DPT. All MUP kits provided must be supplied by USAF qualified sources. Interested contractors must provide a capability statement within 15 days of the date of this notice. The contractor shall indicate size status in relation to NAICS Code 336412, 1000 employees. The capability statement shall address the contractor's ability to meet each of the requirements stated above no later than 18 Jun 01. This capability statement will be used to develop a potential source list. An Ombudsman has been established for this acquisition. The only purpose of the Ombudsman is to receive and communicate serious concerns from potential offerors when an offeror prefers not to use established channels to communicate his/her concern during the proposal development phase of this acquisition. Potential offerors should use established channels to request information, pose questions, and voice concerns before resorting to use of the Ombudsman. Potential offerors are invited to contract ASC's Ombudsman (Mr. Stephen Plaisted, ASC/SY, 1790 10th Street, Room 102.01, Wright-Patterson AFB, OH 45433-7642, email Stephen.Plaisted@ascsy.wpafb.af.mil, phone number (937) 255- 9095, with serious concerns only. Routine communication concerning this acquisition should be directed to the point of contact listed below. Interested firms should submit sufficient information which will permit evaluation of technical capabilities in writing to ASC/LPKB, Bldg 28, ATTN: Ms Julie Hall, 2145 Monahan Way, Wright-Patterson AFB, OH 45433-7017. The point of contact is Julie K. Hall (937) 255-3507, ext 3004, the Contracting Officer is Barbara E. Liptak (937) 255-3507, ext 3001. "
- Web Link
- 220E_UPGRADE -- 220E Engine Upgrade Program (http://www.pixs.wpafb.af.mil/pixslibr/220E_UPGRADE/220E_UPGRADE.asp)
- Record
- Loren Data Corp. 20010606/28SOL009.HTM (D-155 SN50N867)
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