1317M71P04: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include diameter: 2.368 INCHES NOMINAL IN, material: TITANIUM VANE, overall_length: 9.140 INCHES NOMINAL IN, special_features: 2ND END WIDTH 2.174; 2 GROOVES 0.300-0.310 DEEP,0.218-0.222 WIDE, blade_attachment_method: LOCK, end_item_identification: F110 ACFT ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-199-7390, 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 | 2.368 INCHES NOMINAL IN |
| material | TITANIUM VANE |
| stage_number | 1 |
| overall_length | 9.140 INCHES NOMINAL IN |
| special_features | 2ND END WIDTH 2.174; 2 GROOVES 0.300-0.310 DEEP,0.218-0.222 WIDE |
| blade_attachment_method | LOCK |
| end_item_identification | F110 ACFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-199-7390 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | LOCK |
| DIAMETER | 2.368 INCHES NOMINAL IN |
| OVERALL LENGTH | 9.140 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | 2ND END WIDTH 2.174; 2 GROOVES 0.300-0.310 DEEP,0.218-0.222 WIDE |
| END ITEM IDENTIFICATION | F110 ACFT ENGINE |
| MATERIAL | TITANIUM VANE |
No substitute or cross-reference records for this part.