SA-ALC/Contracting Directorate/LDKTE; 485 Quentin Roosevelt Road Suite 12; Kelly AFB, TX 78241-6419

49 -- F-16 ACCESSORY DRIVE GEARBOX TEST STAND (TURKEY) SOL F41608-98-R-14027 DUE 071598 POC The Point of Contact is Bill Kaufman, LDKTE, Phone: (210) 925-0190, FAX: (210) 925-1059 WEB: SA-ALC, Kelly AFB Business Opportunities, http://www.kelly-afb.org/links/proc/index.html. E-MAIL: Send your E-Mail request to the POC, whkaufma@ldgate1.kelly.af.mil. 0001 4920-01-083-0428 F-16 Accessory Drive GearBox Test Stand P/N: 746090 Applicable to: F-16 Accessory Drive Gear Box Qty: 1 EA Approved Sources: H3444/AAR Aircraft Component Systems/Hoofdorp Netherlands 99167/Sundstrand Aerospace/Rockford IL 07486/Sverdrup Technologies/Tullahoma TN DESCRIPTION: The ADG Test Stand is utilized to check the F-16 ADG material and functional integrity as part of depot level overhaul acceptance test requirements after the ADG has been overhauled. This test stand consists of a base assembly, a control assembly, and various accessories. The base assembly provides rigid mounting support for the test article and test stand drive components including an absorption dynamometer, prime mover, speed increasing gearbox, inertial load flywheel, and necessary support bearings and disconnect couplings. The control console provides the operating controls, instrumentation, aircraft controller, and safety circuits necessary for controlling and monitoring the test article and test stand operating parameters. Electrical Harnessing connects the test stand control and monitoring devices to the test article sensor and solenoid valve electrical connector receptacles. A separate unit to the control console assembly is a host computer, and data-acquisition system with programmed software and a printer housed within its own cabinet enclosure. The accessories provide electrical and hydraulic load capability, lubrication and cooling of test article and test stand components. Lubricating oil and hydraulic oil systems can be replenished. In operation, the test stand simulates the F-16 aircraft engine start system function and operating conditions and is designed and built to test the F-16 ADG. Control Console area: 110" L X 51" W X 88" H. Equipment Area: 30' L X 25' W X 14' H. Predominante matl: Steel/electronics. Delivery on 30 Nov 1999 is a critical requirement. Solicitations will be issued around 15 Jun 98, with proposals due 15 Jul 98. Government furnished drawings are not available. Qualification requirements apply. All potential offerors should contact the buyer/PCO identified in this notice for additional information and/or to communicate concerns, if any, concerning this acquisition. If your concerns are not satisfied by the contracting officer, an Ombudsman has been appointed to hear concerns from offerors or potential offerors during the proposal development phase of an acquisition. The Ombudsman does not diminish the authority of the program director or Contracting Officer, but communicates Contractor concerns, issues, disagreements, and recommendations to the appropriate Government personnel. When requested, the Ombudsman shall maintain strict confidentially as to the 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 SA-ALC Acquisition Ombudsman at AC 210-925-5133 or send E-Mail to: ombudsman@www.kelly-afb.org. See Note(s) 23, 26,26 (0152)

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