Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-316-7139 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: 4066171, 2840-01-316-7139, 01-316-7139, 2840013167139, 013167139
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 14, 1990 | 01-316-7139 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-316-7139
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4066171 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-316-7139
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| SPECIAL FEATURES | GOES ON THE COMPRESSOR ROTOR; T.O2J-F100-54, FIG 70, INDEX 4 |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ABGLW$$ACZBJ$$ACZCJ |
| END ITEM IDENTIFICATION | F100PWO229 ENGINE/FAN MODULE |