DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 19.131 INCHES MINIMUM AND 19.141 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, special_features: T.O 2J-F100-24, FIG 117, IND 46; USE ONLY ON P/N 4068443 AND4070833, end_item_identification: ACFT ENG F100, engine_section_location: COMPRESSOR. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-01-020-8704, 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.
| diameter | 19.131 INCHES MINIMUM AND 19.141 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY OVERALL |
| stage_number | 3 |
| special_features | T.O 2J-F100-24, FIG 117, IND 46; USE ONLY ON P/N 4068443 AND4070833 |
| end_item_identification | ACFT ENG F100 |
| engine_section_location | COMPRESSOR |
| NSN | 2840-01-020-8704 |
| ENGINE SECTION LOCATION | COMPRESSOR |
| MATERIAL | TITANIUM ALLOY OVERALL |
| END ITEM IDENTIFICATION | ENGINE,AIRCRAFT,MODEL NO. F100 PW 100 |