Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER LINER
2840-01-111-1894 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: 3040M75P01, 2840-01-111-1894, 01-111-1894, 2840011111894, 011111894
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 12, 1981 | 01-111-1894 | 50349 ( LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-111-1894
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3040M75P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-111-1894
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 0.490 INCHES MINIMUM AND 0.530 INCHES MAXIMUM |
| OVERALL WIDTH | 1.110 INCHES MINIMUM AND 1.150 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF 39 |