NSN 2840-00-146-7800
Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2840-00-146-7800 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: 716055, 2840-00-146-7800, 00-146-7800, 2840001467800, 001467800
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 12, 1971 | 00-146-7800 | 50337 ( CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-146-7800
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 716055 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-146-7800
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | DIFFUSER |
| SPECIAL FEATURES | T.O. 2J-J57-24, FIG 22, IND 4; USED ON THE J57-P-21B AND P-23B ENGINE ONLY; T.O. 2J-J57-54, FIG 21, IND 23; USED ON THE P43W, P43WA, P43WB, P59W ENGINES ONLY; T.O. 2J-J57-74, FIG 19, IND 4; USED ON THE P55A ENGINE ONLY; T.O. 2J-TF33-4, FIG 26, IND 9; USED ON THE P-3 AND THE PW103 ENGINE ONLY; COMBUSTION CAN USED ON THE CASE OUTER FRONT AND OUTER REAR CHAMBER |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J-57 AND TF-33 AIRCRAFT GAS TURBINE ENGINE |
