Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-025-9538 An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 6021T18P01, 5126T62P21, 5126T62P05, 2840-00-025-9538, 00-025-9538, 2840000259538, 000259538
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 01, 1972 | 00-025-9538 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-025-9538
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6021T18P01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 5126T62P21 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 5126T62P05 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-025-9538
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| BLADE ATTACHMENT METHOD | DOVETAIL |
| OVERALL LENGTH | 1.108 INCHES NOMINAL |
| OVERALL HEIGHT | 0.3765 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF34 AIRCRAFT ENGINE |