Surface treatment ams 2416, chromate, modified per pwa-s-2416; 15.199-15.201 in. Id., 8th 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 5930-00-171-5087
NSN 5990-01-612-5323
NSN 5925-01-487-8190
NSN 6240-00-172-8451
NSN 5965-00-899-0453
NSN 6110-00-621-0354
NSN 6130-00-553-8758
NSN 2925-01-014-0118
NSN 6610-00-109-2593
NSN 5920-00-682-0500
NSN 5910-01-443-3016
NSN 5910-00-814-6422