28--ENGINE,GAS TURBINE,NONAIRCRAFT

This contract involves the procurement of 11 gas turbine engines, specifically non-aircraft engines designed for use in C-130H and U aircraft as part of the C-130 Aircraft Avionics Modernization Program. The engines, part number 3800599-1, are FAA-approved models with specifications including a nominal size of approximately 28.2 by 26.7 inches, pneumatic/shaft configuration, and suitable for human-use bleed air with a flow rate of 162.7 PPM at sea level and ambient temperature of 59 degrees Fahrenheit. Key technical details include a shaft horsepower rating of 0.0, rated speed of 42,100 RPM, air horsepower rating of 150, discharge pressure rating of 62.5 PSI, and operating voltage of 24 volts DC. The engines come with various furnished items such as a power output drive, oil pump assembly, fuel control assembly, cooling air fan, tachometer generator, and DC electrical start system, but do not include an enclosure. Deliveries are scheduled in two batches, with five units due by July 31, 2010, and six units by August 31, 2010, to the destination in Ogden, Utah. Honeywell International Inc. in Phoenix, Arizona, is the designated recipient for this solicitation, with an open invitation for all responsible sources to submit capability statements, proposals, or quotations for consideration. The solicitation process is managed electronically, and the contract pertains to NAICS code 336412, covering aircraft engine and engine parts manufacturing. The contract point of contact is Nathan J. Flinders, reachable via phone or email for further inquiries.