723688-103: CASE,COMBUSTION CHAMBER,AIRCRAFT.
CASE,COMBUSTION CHAMBER,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 7.450 INCHES MINIMUM AND 7.520 INCHES MAXIMUM IN, hardness_rating: 36.0 ROCKWELL C NOMINAL VANE, special_features: T.O. 2J-J69-44, FIG 16; REPL P/N 723688-102; CONTAINS SWIRL VANE P/N 713163, end_item_identification: J69-T-25A AIRCRAFT GAS TURBINE ENGINE A, engine_section_location: COMBUSTION CHAMBER.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-448-5790, 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 | NICKEL ALLOY OVERALL |
| overall_length | 7.450 INCHES MINIMUM AND 7.520 INCHES MAXIMUM IN |
| hardness_rating | 36.0 ROCKWELL C NOMINAL VANE |
| special_features | T.O. 2J-J69-44, FIG 16; REPL P/N 723688-102; CONTAINS SWIRL VANE P/N 713163 |
| end_item_identification | J69-T-25A AIRCRAFT GAS TURBINE ENGINE A |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | CZBJ AND ABHP AND FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME SHELL ASSEMBLY,COMPLETE OUTER COMBUSTOR |
| NSN | 2840-01-448-5790 |
| HARDNESS RATING | 36.0 ROCKWELL C NOMINAL VANE |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND FEAT |
| OVERALL LENGTH | 7.450 INCHES MINIMUM AND 7.520 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| SPECIAL FEATURES | T.O. 2J-J69-44, FIG 16; REPL P/N 723688-102; CONTAINS SWIRL VANE P/N 713163 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SHELL ASSEMBLY,COMPLETE OUTER COMBUSTOR |
| END ITEM IDENTIFICATION | J69-T-25A AIRCRAFT GAS TURBINE ENGINE A |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.