16 -- EA-6B NOZZLE, ENGINE TEST, DRAWING PWA34985

Notice Date

December 17, 2001

Contracting Office

NUWC Division Keyport, ATTN: C/182, 610 Dowell Street, Keyport, WA 98345-7610

ZIP Code

98345-7610

Response Due

January 15, 2002

Point of Contact

lkono@kpt.nuwc.navy.mil

E-Mail Address

Technical Point of Contact for Questions (lkono@kpt.nuwc.navy.mil)

Description

EA-6B Nozzle, Engine Test, drawing PWA34985. This is a short lead-time, and possibly a one-time requirement for 10-20 parts with a First Article. The supplier of this part shall be ISO 9000 or equivalent certified and be able to show a successful history of past performance with this type of aircraft component. Certification documents shall be required for all processes, including materials, heat treat, machining, welding, NDT and Quality Assurance. The material is in accordance with AMS 5599 and AMS 5666, welding in accordance with PWA 15&16, AWS C1.1-66&D1.1 or MIL-STD 2219&MIL-STD 6858. The configuration is a welded seam, cone shaped sheet part approximately 27 inches in diameter at the large end and 18 inches at the small end, by 16 inches long. The exterior skin has welded stiffener ribs, 3 places that extend around the circumference of the part. The large end, on the face of the part, has a welded ring, conforming to the circular configuration, fabricated from AMS 5599 plate or AMS 5666 Inconel bar and butt welded. There is a machined 25.496 +.002-.000 step machined in the end of the ring with a 32 finish and .002 flatness requirement (free state), with a series of 72 X .281 (positional location of .010) holes around the face. First Article evaluation will consist of destination dimensional, documentation, Metallurgical, NDT and a functional test run to the engine. The delivery for the First Article and the production parts will be critical to the award of the contract. After review of this announcement; if qualified and interested, you may contact Lew Kono via email.

Record

Loren Data Corp. 20011219/16SOL012.HTM (D-351 SN5153F8)