Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2840-01-039-3369 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: 6871486, 23056130, 6871486, 23056130, 2840-01-039-3369, 01-039-3369, 2840010393369, 010393369
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 17, 1977 | 01-039-3369 | 50337 ( CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-039-3369
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6871486 | 73342 | ALLISON TRANSMISSION, INC. |
| 23056130 | 73342 | ALLISON TRANSMISSION, INC. |
| 6871486 | 63005 | ROLLS-ROYCE CORPORATION |
| 23056130 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-039-3369
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | CRES, AMS5521, 9.560 IN. NOM. O/A LG.; 6.524 IN. MIN.,6.536 IN. MAX. O/A OD; 1ST END FLANGE, 12 SLOTS EQUALLY SPACED ON OUTER PERIPHERY, 0.500 IN. NOM. DISTANCE FROM 1ST END TO SLOTS; 22 SLOTS EQUALLY SPACED ON OUTER PERIPHERY, 3.310 IN. NOM. DISTANCE FROM 2ND END TO SLOTS; 22 SLOTS EQUALLY SPACED ON OUTER PERIPHERY, 1.411 IN. NOM. DISTANCE FROM 2ND END TO SLOTS; 14 HOLES 0.375 IN. NOM. DIA. EQUALLY SPACED ON OUTER PERIPHERY; 2.090 IN. NOM. DISTANCE FROM 2ND END TO HOLE CENTERS, 6 HOLES 0.500 IN. NOM. DIA. AND 6 HOLES 0.562 IN. NOM. DIA. THROUGH BODY ALTERNATELY SPACED IN GROUPS OF 3 ON OUTER PERIPHERY, 2.720 IN. NOM. DISTANCE FROM 2ND END TO HOLE CENTERS |