7th stage, surface treatment ams 2416 chromate
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 6220-01-502-1852
NSN 6610-01-314-3659
NSN 5975-00-258-7396
NSN 6135-01-540-2403
NSN 5905-00-117-4693
NSN 2925-01-394-9658
NSN 5965-01-025-5129
NSN 6105-01-409-1432
NSN 6650-01-129-2886
NSN 6645-00-456-7653
NSN 5990-01-386-8051
NSN 6150-01-251-7120