Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE DISK
2840-01-448-7539 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.
Alternate Parts: 4087201, 4085001, 2840-01-448-7539, 01-448-7539, 2840014487539, 014487539
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1997 | 01-448-7539 | 50571 ( DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-7539
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4087201 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4085001 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-448-7539
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.809 INCHES MINIMUM AND 1.811 INCHES MAXIMUM |
| DIAMETER | 36.696 INCHES MINIMUM AND 36.736 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 99, IND 42; USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AABMZ$$AABHP$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |