Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2840-01-110-8108 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: 728783, 2840-01-110-8108, 01-110-8108, 2840011108108, 011108108
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 06, 1981 | 01-110-8108 | 50337 ( CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-110-8108
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 728783 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-110-8108
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 11.980 INCHES MINIMUM AND 12.040 INCHES MAXIMUM |
| DIAMETER | 6.800 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-TF30-24; 1 OF 8 COMBUSTION CANS |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF 30 |