Part Details | AIRCRAFT GAS TURBINE ENGINE FAN DISK
2840-01-442-3557 An item having provisions on the outer periphery for attaching a designated number of BLADE, FAN, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, FAN, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 1559M93P03, 2840-01-442-3557, 01-442-3557, 2840014423557, 014423557
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 12, 1997 | 01-442-3557 | 50569 ( DISK, FAN, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-442-3557
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1559M93P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-442-3557
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | FAN |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 3.687 INCHES MINIMUM AND 4.807 INCHES MAXIMUM |
| DIAMETER | 23.255 INCHES MINIMUM AND 23.263 INCHES MAXIMUM |
| SPECIAL FEATURES | CID A197875INTRODUCES LPTR DISKS W/MODIFIED CUSP AND MISMATCH DEFINITIONS FOR THE DOVETAIL SLOT; NEW DOVETAIL SLOTS IMPROVE AND CLARIFY VARIATION ALLOWANCE DEFINITION OF ALLOWABLE SURFACE CONDITIONS; THESE DISK IMPROVEMENTS ALLOW MISMATCH SIZE AND LOCATION THATIMPROVE CONTROL OF THE SLOT FEATURE LIVES; REWORKED FROM P/N 1559M93P02 |
| END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |