Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE RETAINER
2840-01-412-2803 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: 1854M45G01, 2840-01-412-2803, 01-412-2803, 2840014122803, 014122803
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 14, 1995 | 01-412-2803 | 52400 ( RETAINER, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-412-2803
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1854M45G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-412-2803
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL CORROSION RESISTING |
| STAGE NUMBER | 1 |
| REFERENCE DATA AND LITERATURE | AFTO:2J-TF39-4 |
| CRITICALITY CODE JUSTIFICATION | AMATT$$AAGAV |
| END ITEM IDENTIFICATION | C-5A AIRCRAFT;TF-39 ENGINE. |