Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER LINER
2840-01-230-5120 A cylindrical shaped item positioned inside the CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. It is designed to direct the flow of hot gasses to the TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 723706102, 723706-102, 2840-01-230-5120, 01-230-5120, 2840012305120, 012305120
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 15, 1986 | 01-230-5120 | 50349 ( LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-230-5120
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 723706-102 | 03104 | TELEDYNE TECHNOLOGIES INCORPORATEDDBA TELEDYNE TURBINE ENGINES |
Technical Data | NSN 2840-01-230-5120
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 7.020 INCHES MINIMUM AND 7.140 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT.ENG. J69-25/25A |