Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-01-333-4340 An item having provisions on the outer periphery for attaching a designated number of BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 4074511, 2840-01-333-4340, 01-333-4340, 2840013334340, 013334340
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 03, 1991 | 01-333-4340 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-333-4340
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4074511 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-333-4340
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 11 |
| OVERALL LENGTH | 3.766 INCHES MINIMUM AND 3.770 INCHES MAXIMUM |
| DIAMETER | 16.834 INCHES MINIMUM AND 16.843 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 139, IND 4 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMZ$$AAPGF$$ACZBJ$$ACZCJ |
| END ITEM IDENTIFICATION | F100-PW-100/200 AIRCRAFT ENGINES |
| FSC APPLICATION DATA | F-15 AIRCRAFT |