Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE LOCK
2840-01-307-6361 An item used to maintain the position of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: KDS 28404003, KDS 2840-4003, 1441M31P06, 2840-01-307-6361, 01-307-6361, 2840013076361, 013076361
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 14, 1989 | 01-307-6361 | 50458 ( LOCK, TURBINE ROTOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-307-6361
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| KDS 2840-4003 | 3999F | DEFENSE ACQUISITION PROGRAMADMINISTRATION, R.O.K |
| 1441M31P06 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-307-6361
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM |
| MATERIAL DOCUMENT AND CLASSIFICATION | C50TF70,CL-A MFR REF SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.074 INCHES MINIMUM AND 0.083 INCHES MAXIMUM |
| OVERALL WIDTH | 0.658 INCHES NOMINAL |
| OVERALL LENGTH | 0.666 INCHES MINIMUM AND 0.676 INCHES MAXIMUM |
| SPECIAL FEATURES | USED ON THE REAR HIGH PRESSURE TURBINE |
| END ITEM IDENTIFICATION | F110GE129 ACFT ENGINE |