Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER LINER
2840-01-448-7036 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: 4084087, 4084087, 2840-01-448-7036, 01-448-7036, 2840014487036, 014487036
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1997 | 01-448-7036 | 50349 ( LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-7036
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4084087 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4084087 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-448-7036
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 6.157 INCHES MINIMUM AND 6.269 INCHES MAXIMUM |
| OVERALL WIDTH | 1.456 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 100, IND 21; USE ONLY ON P/N 4084089 AND 4083194; 96QA074 IMPROVED DURABLILITY LINER SEGMENT THRU NORMAL ATTRITION OF PARTS |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMK$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME LINER SEGMENT,COMBUSTION CHAMBER |