4059691CLL: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include special_features: T.O. 2J-F100-24, FIG 133, IND 32;1.769-1.787 SQ IN TOTAL AREA; 1 UNIT PER ASSY; HAS BORESCOPE HOLE FOR INSPECTION, end_item_identification: F100PW220 AIRCRAFT ENGINE, engine_section_location: TURBINE, criticality_code_justification: AGAV, part_name_assigned_by_controlling_agency: ORIGINAL NAME NOZZLE ASSEMBLY,TURBINE, AIRCRAFT GAS TURBINE ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-375-1413, 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.
| stage_number | 1 |
| special_features | T.O. 2J-F100-24, FIG 133, IND 32;1.769-1.787 SQ IN TOTAL AREA; 1 UNIT PER ASSY; HAS BORESCOPE HOLE FOR INSPECTION |
| end_item_identification | F100PW220 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME NOZZLE ASSEMBLY,TURBINE, AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-375-1413 |
| STAGE NUMBER | 1 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-24, FIG 133, IND 32;1.769-1.787 SQ IN TOTAL AREA; 1 UNIT PER ASSY; HAS BORESCOPE HOLE FOR INSPECTION |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME NOZZLE ASSEMBLY,TURBINE, AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | F100PW220 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.