Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2840-01-448-6996 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.
Alternate Parts: 4083973, 2840-01-448-6996, 01-448-6996, 2840014486996, 014486996
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1997 | 01-448-6996 | 50337 ( CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-6996
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083973 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-448-6996
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 100, IND 35; COMBUSTION CHAMBER ASSY; USE ONLY ON P/NS 4083194, 4083560 AND 4083565; 96QA053 RETROFIT OF 1997 ENGINE ENHANCEMENTS PACKAGE |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CHAMBER,COMBUSTION,INNER |