1317M71P02: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: TITANIUM VANE, overall_width: 3.368 INCHES NOMINAL IN, overall_length: 9.140 INCHES NOMINAL IN, special_features: BOTTOM WIDTH,2ND END 2.174 IN.; 2 GROOVES NEAR BOTTOM 0.225 BY 0.220 IN.; MATL C50TF22 IN, blade_attachment_method: LOCK, end_item_identification: F110 ACFT ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-200-8832, 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 VANE |
| stage_number | 1 |
| overall_width | 3.368 INCHES NOMINAL IN |
| overall_length | 9.140 INCHES NOMINAL IN |
| special_features | BOTTOM WIDTH,2ND END 2.174 IN.; 2 GROOVES NEAR BOTTOM 0.225 BY 0.220 IN.; MATL C50TF22 IN |
| blade_attachment_method | LOCK |
| end_item_identification | F110 ACFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-200-8832 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 9.140 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.368 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | BOTTOM WIDTH,2ND END 2.174 IN.; 2 GROOVES NEAR BOTTOM 0.225 BY 0.220 IN.; MATL C50TF22 IN |
| END ITEM IDENTIFICATION | F110 ACFT ENGINE |
| MATERIAL | TITANIUM VANE |
No substitute or cross-reference records for this part.