SPACER,COMPRESSOR ROTOR,AIRCRAFT. Key specifications include material: STEEL, overall_length: 3.185 INCHES MINIMUM AND 3.189 INCHES MAXIMUM IN, outside_diameter: 17.240 INCHES MINIMUM AND 17.250 INCHES MAXIMUM IN, special_features: SURFACE TREAT,AMS 2416 CHROMATE, MODIFIED PER PWA-S-2416, 15.199-15.201IN. ID., 5TH STAGE IN, end_item_identification: TF-33 AIRCRAFT ENGINE, reference_data_and_literature: 2J-TF33-4.
This product is currently in active production with full OEM support. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-966-8083, indicating validated use in U.S. government and defense logistics supply chains.
Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.
| material | STEEL |
| overall_length | 3.185 INCHES MINIMUM AND 3.189 INCHES MAXIMUM IN |
| outside_diameter | 17.240 INCHES MINIMUM AND 17.250 INCHES MAXIMUM IN |
| special_features | SURFACE TREAT,AMS 2416 CHROMATE, MODIFIED PER PWA-S-2416, 15.199-15.201IN. ID., 5TH STAGE IN |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| reference_data_and_literature | 2J-TF33-4 |
| criticality_code_justification | AGAV |
| NSN | 2840-00-966-8083 |
| MATERIAL | STEEL |
| SPECIAL FEATURES | SURFACE TREAT,AMS 2416 CHROMATE, MODIFIED PER PWA-S-2416, 15.199-15.201IN. ID., 5TH STAGE IN |
| OUTSIDE DIAMETER | 17.240 INCHES MINIMUM AND 17.250 INCHES MAXIMUM IN |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| REFERENCE DATA AND LITERATURE | 2J-TF33-4 |
| OVERALL LENGTH | 3.185 INCHES MINIMUM AND 3.189 INCHES MAXIMUM IN |