Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-318-7550 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: 407561103, 4075611-03, 2840-01-318-7550, 01-318-7550, 2840013187550, 013187550
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 25, 1990 | 01-318-7550 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-318-7550
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4075611-03 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-318-7550
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 11 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 1.528 INCHES NOMINAL |
| OVERALL WIDTH | 0.912 INCHES NOMINAL |
| SPECIAL FEATURES | RADIUN CUT OF CAP IS 0.120 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 ENGINE/CORE MOD |