Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE BLADE RETAINER
2840-01-138-5658 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: 9104M10P07, 9104M10P06, 2840-01-138-5658, 01-138-5658, 2840011385658, 011385658
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 16, 1982 | 01-138-5658 | 52404 ( RETAINER, TURBINE BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-138-5658
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9104M10P07 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9104M10P06 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-138-5658
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| OVERALL LENGTH | 0.694 INCHES NOMINAL |
| OUTSIDE DIAMETER | 22.854 INCHES MINIMUM AND 22.885 INCHES MAXIMUM |
| STAGE NUMBER | 2 |
| REFERENCE DATA AND LITERATURE | 2J-TF39-4, FIG 59 IND 25 |
| SPECIAL FEATURES | HIGH PRESSURE TURBINE ROTOR ASSY;2ND STAGE; CBORE FOR 29 HOLES EQ SP, 29 POCKETS |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |