Part Details | AIRCRAFT GAS TURBINE ENGINE FAN BLADE LOCK
2840-01-215-3610 An item used to maintain the position of a BLADE, FAN, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, FAN, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: 1317M74P02, 1317M74P02, 2840-01-215-3610, 01-215-3610, 2840012153610, 012153610
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 23, 1985 | 01-215-3610 | 50456 ( LOCK, FAN BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-215-3610
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1317M74P02 | 02653 | BERKSHIRE MANUFACTURED PRODUCTS,INC. |
| 1317M74P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-215-3610
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5537 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 1 |
| MATERIAL THICKNESS | 0.007 INCHES MINIMUM AND 0.009 INCHES MAXIMUM |
| OVERALL WIDTH | 0.210 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
| OVERALL LENGTH | 10.832 INCHES NOMINAL |
| SPECIAL FEATURES | WIDTH OF RESTRAINED 0.214-0.218; T.O. 2J-F110-14,FAN STATOR ASSY |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |