Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER LINER
2840-01-015-1751 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: 643E406G9, 2840-01-015-1751, 01-015-1751, 2840010151751, 010151751
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 15, 1976 | 01-015-1751 | 50349 ( LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-015-1751
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 643E406G9 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-015-1751
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 12.030 INCHES MINIMUM AND 12.080 INCHES MAXIMUM |
| SPECIAL FEATURES | USED ON -7B, -11A, -11B AND -19 SERIES ENGINES |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J-79 AIRCRAFT TURBINE ENGINES |