NSN 2840-01-458-6861 01-458-6861, 014586861
Product Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK
2840-01-458-6861 An item having provisions on the outer periphery for attaching a designated number of BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Part Alternates: 2840-01-458-6861, 01-458-6861, 2840014586861, 014586861
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 | 01-458-6861 | 50571 ( DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
Request a Quote
What Our Customers Say
Thank you very much for the excellent service and professional customer care.
The service was excellent. I can think of no improvements to date that you can make regarding internet sales.
The representative for WBParts was efficient & handled our request in a timely & professional manner.
Tried two other sources, neither of them responded, was all done online, never spoke to anyone.
The response is quick and the price is often very good. We are completely satisfied.
Compare
Related Products | NSN 2840-01-458-6861
Technical Data | NSN 2840-01-458-6861
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY OVERALL |
| MATERIAL DOCUMENT AND CLASSIFICATION | RENE 95 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 3.979 INCHES MINIMUM AND 3.989 INCHES MAXIMUM |
| OVERALL WIDTH | 18.900 INCHES MINIMUM AND 19.007 INCHES MAXIMUM |
| DIAMETER | 24.102 INCHES MINIMUM AND 24.110 INCHES MAXIMUM |
| SPECIAL FEATURES | MATERIAL CHGING FROM -140 MESH R95 TO -270 MESH R95; SAME AS 1385M23P04 BUT USED ONLY ON THE 118-100 ENGINE |
| CRITICALITY CODE JUSTIFICATION | APGF AND ABHP AND ABMK AND ABMZ AND FEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 52, IND 18 |
| III END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| III PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME DISK, HIGH PRESSURE TURBINE ROTOR |
| MANUFACTURERS CODE | 07482 |
| DESIGN CONTROL REFERENCE | 1385M23P04-118 |
Restrictions/Controls & Freight Information | NSN 2840-01-458-6861
| 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 | ||