Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER DUCT
2840-01-009-2400 A cylindrical shaped item or a segment thereof designed to direct air into or around a CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE. The internal iar is divided and directed to the burning chamber(s). The external air is used for cooling purposes.
Alternate Parts: 7015M13G05, 7015M13G01, 2840-01-009-2400, 01-009-2400, 2840010092400, 010092400
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 05, 1975 | 01-009-2400 | 52524 ( DUCT, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-009-2400
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 7015M13G05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 7015M13G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-009-2400
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 6.540 INCHES MINIMUM AND 6.600 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J79 ENGINE |