Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER LINER
2840-01-421-9742 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: 4083065, 4083065, 2840-01-421-9742, 01-421-9742, 2840014219742, 014219742
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 17, 1995 | 01-421-9742 | 50349 ( LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-421-9742
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083065 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4083065 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-421-9742
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 6.291 INCHES MINIMUM AND 6.403 INCHES MAXIMUM |
| OVERALL WIDTH | 1.764 INCHES NOMINAL |
| SPECIAL FEATURES | THERMAL BARRIER COATING ADDED PER ECN 95QA006 |
| CRITICALITY CODE JUSTIFICATION | ASTDC$$ACZBJ$$AABHP$$AABMK$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | LINER SEGMENT,COMBUSTION CHAMBER DUCT, 5 OD |