Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-160-9206 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: 745094, 745094, 2840-01-160-9206, 01-160-9206, 2840011609206, 011609206
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 29, 1983 | 01-160-9206 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-160-9206
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 745094 | 81753 | CONNECTICUT SPRING & STAMPINGCORPORATION THE |
| 745094 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-160-9206
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5517 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 3.326 INCHES MINIMUM AND 3.338 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF33-4; GOES ON THE COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |