NSN 2840-01-323-9310 01-323-9310, 013239310
Product Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-323-9310 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT.
Part Alternates: 2840-01-323-9310, 01-323-9310, 2840013239310, 013239310
Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | 01-323-9310 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
Cross Reference | NSN 2840-01-323-9310
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4077513-01 | 77445 | UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS |
| 4079413-01 | 77445 | UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS |
| 4081613-01 | 52661 | UNITED TECHNOLOGIES CORPORATION DBA PRATT & WHITNEY |
| 4081613-01 | 77445 | UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS |
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Related Products | NSN 2840-01-323-9310
Technical Data | NSN 2840-01-323-9310
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY BLADE |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 12 |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 1.371 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| III END ITEM IDENTIFICATION | ACFT ENG F100PW0229 |
| MANUFACTURERS CODE | 77445 |
| DESIGN CONTROL REFERENCE | 4077513-01 |
Restrictions/Controls & Freight Information | NSN 2840-01-323-9310
| Category | Code | Description |
|---|---|---|
| Hazardous Material Indicator Code | N | There is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials |
| Category | Code | Description |
|---|---|---|
| No Freight Information | ||



