Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-374-8488 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: 408161104, 4081611-04, 408161104, 4081611-04, 408161104, 4081611-04, 407941104, 4079411-04, 4079411, 2840-01-374-8488, 01-374-8488, 2840013748488, 013748488
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 30, 1993 | 01-374-8488 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-374-8488
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4081611-04 | 1645F | HANWHA TECHWIN CO.,LTDDIV PS BUSINESS UNIT |
| 4081611-04 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4081611-04 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4079411-04 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4079411 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-374-8488
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 11 |
| OVERALL LENGTH | 1.598 INCHES NOMINAL |
| OVERALL WIDTH | 0.810 INCHES MINIMUM AND 0.818 INCHES MAXIMUM |
| SPECIAL FEATURES | BLADE ATTACHMENT IS DOVETAIL; T.O. 2J-F100-54; 2 UNITS PER ASSY; USE ONLY ON 4079287-01,4080405-01,4080720-01,4080812-01,AND 4080884-01 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE/CORE |