Part Details | AIRCRAFT TURBINE ENGINE TURBINE BLADE DAMPER
2840-01-124-0707 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: 4057120, 4057120, 4057120, 2840-01-124-0707, 01-124-0707, 2840011240707, 011240707
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 27, 1981 | 01-124-0707 | 50557 ( DAMPER, TURBINE BLADE, AIRCRAFT TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-124-0707
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4057120 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4057120 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4057120 | 03823 | WYMAN-GORDON INVESTMENT CASTINGS,INC |
Technical Data | NSN 2840-01-124-0707
| Characteristic | Specifications |
|---|---|
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 0.847 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT F100-PW-229 (F15E, F16C/D); ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E) |