Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER DUCT
2840-00-690-3727 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: 111R558G1, 111R558G2, 111R558G1, 2840-00-690-3727, 00-690-3727, 2840006903727, 006903727
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1961 | 00-690-3727 | 52524 ( DUCT, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-690-3727
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R558G1 | 24446 | GENERAL ELECTRIC COMPANY |
| 111R558G2 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R558G1 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-690-3727
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 6.190 INCHES MINIMUM AND 6.250 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J79, J85, T58, T64 |