Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER DUCT
2840-00-834-7639 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: 111R668G04, 111R668G02, 2840-00-834-7639, 00-834-7639, 2840008347639, 008347639
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 25, 1966 | 00-834-7639 | 52524 ( DUCT, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-834-7639
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R668G04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R668G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-834-7639
| 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 | J-85 AIRCRAFT ENGINE |