4056200: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include overall_width: 5.535 INCHES MINIMUM AND 5.545 INCHES MAXIMUM IN, overall_length: 20.600 INCHES NOMINAL IN, end_item_identification: F100PW100/200 ACFT ENGINE, engine_section_location: HIGH PRESSURE TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-164-9087, 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.
| overall_width | 5.535 INCHES MINIMUM AND 5.545 INCHES MAXIMUM IN |
| overall_length | 20.600 INCHES NOMINAL IN |
| special_features | T.O. 2J-F110-4; AUGMENTOR NOZZLE LEVER; BALANCE & CONVERGENT NOZZLE SEGMENT; 15 UNITS PER ASSY; 0.159-0.163 IN. DIA OF 1 HOLE; 0.190-0.192 IN. DIA THRU 2 LUGS IN |
| end_item_identification | F100PW100/200 ACFT ENGINE |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-164-9087 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 20.600 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.535 INCHES MINIMUM AND 5.545 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | T.O. 2J-F110-4; AUGMENTOR NOZZLE LEVER; BALANCE & CONVERGENT NOZZLE SEGMENT; 15 UNITS PER ASSY; 0.159-0.163 IN. DIA OF 1 HOLE; 0.190-0.192 IN. DIA THRU 2 LUGS IN |
| END ITEM IDENTIFICATION | F100PW100/200 ACFT ENGINE |
No substitute or cross-reference records for this part.