Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER LINER
2840-01-365-0139 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: 4074047, 4074047, 2840-01-365-0139, 01-365-0139, 2840013650139, 013650139
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 30, 1992 | 01-365-0139 | 50349 ( LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-365-0139
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4074047 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4074047 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-365-0139
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.040 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| DIAMETER | 24.178 INCHES MINIMUM AND 24.198 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100/200 ENG CORE MODULE |