Part Details | AIRCRAFT TURBINE ENGINE TURBINE BLADE DAMPER
2840-01-364-2282 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also acts as a seal. It may be of various shapes and cross sections.
Alternate Parts: 4079618, 4079618, 2840-01-364-2282, 01-364-2282, 2840013642282, 013642282
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 14, 1992 | 01-364-2282 | 50557 ( DAMPER, TURBINE BLADE, AIRCRAFT TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-364-2282
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4079618 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4079618 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-364-2282
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 0.847 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT ENGINE |