NSN 2840-00-098-3141
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-00-098-3141 An item used to maintain the position of a BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: 220571, 2840-00-098-3141, 00-098-3141, 2840000983141, 000983141
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-098-3141 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-098-3141
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 220571 | 0AHP5 | CURTISS-WRIGHT CONTROLS, INCDIV SENSORS & CONTROLS |
Technical Data | NSN 2840-00-098-3141
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE |
| HARDNESS RATING | 19.0 ROCKWELL C MINIMUM AND 26.0 ROCKWELL C MAXIMUM |
| STAGE NUMBER | 1 |
| MATERIAL THICKNESS | 0.010 INCHES NOMINAL |
| OVERALL WIDTH | 0.112 INCHES MINIMUM AND 0.116 INCHES MAXIMUM |
| OVERALL LENGTH | 0.548 INCHES MINIMUM AND 0.552 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | 2J-J65-4 |
| SPECIAL FEATURES | GOES ON CENTER MAIN BEARING SUPPORT; COMPRESSOR STATOR; FRONT EXIT STAGE BLADE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J-65 AIRCRAFT ENGINE |