Surface treat, ams 2416 chromate, modified per pwa-s-2416, 15.199-15.201in. Id., 5th stage
A rigid item designed to maintain a predetermined space between two rotor, compressor, aircraft gas turbine engine. It may be a complete 360 degrees or a section thereof.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5910-01-653-8699
NSN 5920-01-065-1824
NSN 5965-00-256-8687
NSN 2925-01-267-1598
NSN 5998-00-701-9143
NSN 5999-01-408-1108
NSN 5925-01-093-5961
NSN 6610-00-102-9226
NSN 5996-00-142-5697
NSN 5990-00-404-9567
NSN 5945-01-338-5368
NSN 6150-01-058-3570