1277M33G02: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: TITANIUM ALLOY OVERALL, overall_length: 1.212 INCHES NOMINAL IN, special_features: T.O. 2J-F110-14; FAN ROTOR ASSY; DISKS,BLADES AND REAR SHAFT, end_item_identification: ACFT ENG F110, engine_section_location: TURBINE, criticality_code_justification: AGAV.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-198-3723, 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 | TITANIUM ALLOY OVERALL |
| stage_number | 3 |
| overall_length | 1.212 INCHES NOMINAL IN |
| special_features | T.O. 2J-F110-14; FAN ROTOR ASSY; DISKS,BLADES AND REAR SHAFT |
| end_item_identification | ACFT ENG F110 |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | A50TF156,CL-A MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-198-3723 |
| STAGE NUMBER | 3 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | A50TF156,CL-A MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 1.212 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F110-14; FAN ROTOR ASSY; DISKS,BLADES AND REAR SHAFT |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.