NSN 2840-00-828-5212
Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2840-00-828-5212 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: 628358, 568243, 704334, 2840-00-828-5212, 00-828-5212, 2840008285212, 008285212
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 28, 1967 | 00-828-5212 | 50337 ( CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-828-5212
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 628358 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 568243 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 704334 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-828-5212
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 17.260 INCHES MINIMUM AND 17.320 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF33-14, FIG 25, IND 9; USED ON THE TF33-P-7A ENGINE ONLY; T.O. 2J-TF33-4, FIG 27, IND 8; TO BE USED ON THE P-5 AND P-9 ENGINE ONLY; COMBUSTION CAN USED ON THE CASE OUTER FRONT AND OUTER REAR CHAMBER |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |