Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE BLADE RETAINER
2840-01-434-7060 An item specifically designed to position and/or restrain the movement of one or more BLADE, or BLADE SET, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may be the full 360 degrees required for one turbine stage or a segment thereof.
Alternate Parts: 1387M99P04, 1387M99P03, 1387M99P01, 1387M99, 2840-01-434-7060, 01-434-7060, 2840014347060, 014347060
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 05, 1996 | 01-434-7060 | 52404 ( RETAINER, TURBINE BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-434-7060
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1387M99P04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1387M99P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1387M99P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1387M99 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-434-7060
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| OVERALL LENGTH | 1.660 INCHES MINIMUM AND 1.680 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 19.370 INCHES MINIMUM AND 19.380 INCHES MAXIMUM |
| SPECIAL FEATURES | USED ON THE LOW PRESSURE TURBINE;MATL NICKEL, COBALT, CHROMIUM ALLOY |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABKV$$AFEAT |
| END ITEM IDENTIFICATION | F110-GE-100 AIRCRAFT GAS TURBINE ENGINE |