Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2840-01-008-5984 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: 111016206, 1-110-162-06, 2840-01-008-5984, 01-008-5984, 2840010085984, 010085984
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 26, 1975 | 01-008-5984 | 50337 ( CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-008-5984
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-110-162-06 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-008-5984
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | CRES, AMS5536, ROCKWELL 15T SCALE 83 MIN., 92.5 MAX. HARDNESS, 15.500 IN. NOM. O/A OD; 2.480 IN. NOM. O/A LG.; 0.040 IN. MIN., 0.044 IN. MAX. THK MATERIAL, 88 SLOTS 0.020 IN. MIN., 0.030 IN. MAX. W ON OD BREAKING INTO 88 HOLES 0.094 IN. NOM. DIA EQUALLY SPACED ON OD; 0.640IN. NOM. DISTANCE FROM END TO HOLE CENTERS; 11.712 IN. NOM. OD INNER WALL; 50 LOUVERS EQUALLY SPACED ON INNER WALL, 0.390 IN. NOM. EFFECTIVE LG. LOUVER; 0.0795 IN. NOM. INSIDE H LOUVER |