Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-00-037-6715 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: 243381, 226373, 206207, 2840-00-037-6715, 00-037-6715, 2840000376715, 000376715
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-037-6715 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-037-6715
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 243381 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 226373 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 206207 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-037-6715
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5517 ASSN STD SINGLE MATERIAL RESPONSE |
| HARDNESS RATING | 63.0 ROCKWELL A MINIMUM AND 68.0 ROCKWELL A MAXIMUM |
| OVERALL WIDTH | 0.305 INCHES MINIMUM AND 0.315 INCHES MAXIMUM |
| OVERALL LENGTH | 1.351 INCHES MINIMUM AND 1.361 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | ACQFM$$AABMK |
| END ITEM IDENTIFICATION | ACFT ENG J57 |