Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER LINER
2840-01-128-6611 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: 213111063, 2-131-110-63, 2840-01-128-6611, 01-128-6611, 2840011286611, 011286611
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 26, 1982 | 01-128-6611 | 50349 ( LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-128-6611
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-131-110-63 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-128-6611
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | MATERIAL METALLIC; C/O 1 EA SUPPORT,CURL,2 EA GUIDE,NOZZLE,4 EA SEAL ASSY,SPARK PLUG,1 EA LINER,INNER,1 EA LINER,OUTER; OD MIN 23.220 IN.,MAX 23.310 IN. |
| END ITEM IDENTIFICATION | T55-L-712ENGINE,AIRCRAFT,TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | LINER,COMBUSTION CHAMBER,TURBINE ENGINE |