Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER DUCT
2840-01-254-6883 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: 2186053, 2186053, 594334, 2186053, 2840-01-254-6883, 01-254-6883, 2840012546883, 012546883
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 08, 1987 | 01-254-6883 | 52524 ( DUCT, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-254-6883
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2186053 | 85291 | B. H. AIRCRAFT COMPANY, INC. |
| 2186053 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 594334 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 2186053 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-254-6883
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 5.657 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-TF30-24; SUPPORTS THE COMBUSTION CANS,KEEPS THEM IN LINE AND HELPS ALIGN THE DUCT,COMBUSTION CHAMBERTO ATTACH TO THE CANS |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT.ENG. TF30 |
