Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE RETAINER
2840-01-139-7398 An item specifically designed to position and/or restrain the movement of one or more BLADE, or BLADE SET, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may be the full 360 degrees required for one compressor stage or a segment thereof.
Alternate Parts: 4070T12P01, 10160173, 2840-01-139-7398, 01-139-7398, 2840011397398, 011397398
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 05, 1982 | 01-139-7398 | 52400 ( RETAINER, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-139-7398
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4070T12P01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 10160173 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
Technical Data | NSN 2840-01-139-7398
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| SPECIAL FEATURES | MATERIAL STEEL, AMS 5688;ANY ACCEPTABLE SURFACE TREATMENT;STRENGTH NOT RATED;MATERIAL HARDNESS RATING 60.0 ROCKWELL C MIN AND 72.0 ROCKWELL C MAX;NOT CASEHARDENED;INTERNAL RING STYLE;90 DEGREE PARALLEL END STYLE;INSIDE DIAMETER 15.562 IN. MIN AND 15.772 IN. MAX;OUTSIDE DIAMETER 15.870 IN. MIN AND 16.070 IN. MAX;CROSS-SECTIONAL SHAPE STYLE ROUNDED CORNERS;MAJOR THICKNESS 0.039 IN. MIN AND 0.041 IN. MAX;EXTERNAL USAGE DESIGN |