SA-ALC/BC, 303 S Crickett Dr., STE 4, Kelly AFB TX 78241-6025

15 -- F-5A/B SPARE WING DESIGN SOL JT12. POC Joe Torres. SOURCE QUALIFICATION NOTICE: THIS IS NOT A SOLICITATION. This notice is to publicize the availability of Qualification Requirements for certification of F-5A/B Aircraft Improved Wing Design. The requirement for a certification of design and qualification of manufacturer is based on the advanced age of the F-5A/B fleet, the susceptibility of the current spare wing design to fatigue, corrosion and stress corrosion cracking and in anticipation of future requirements. The F-5A/B Aircraft is a supersonic tactical fighter. The F-5A/B wing is a fully cantilevered, stressed skin assembly constructed as a single unit composed of spars, ribs and milled skins that are continuous from tip to tip. Honeycomb assemblies also exist in the form of wing panel assemblies. The basic material used during construction is aluminum with the exception of a couple of steel ribs. Information and complete copy of the Qualification Requirements can be obtained by submitting a written or FAX request to the Attention of Mr. Joe Torres; SA-ALC/BC; 303 S. Crickett Dr., Ste, 4; KELLY AFB, TX 78241-6025; FAX: (210) 925-0235. (324)

Loren Data Corp. http://www.ld.com (SYN# 0150 19961121\15-0005.SOL)