NSN 2840-00-166-2357
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-166-2357 An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 753213, 753213, 753013, 726713, 711413, 625513, 462813, 2840-00-166-2357, 00-166-2357, 2840001662357, 001662357
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | FEB 09, 1973 | 00-166-2357 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-166-2357
Part Number | Cage Code | Manufacturer |
---|---|---|
753213 | 8W315 | TURBINE ENGINE COMPONENTSTECHNOLOGIES CORPORATION |
753213 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
753013 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
726713 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
711413 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
625513 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
462813 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-166-2357
Characteristic | Specifications |
---|---|
DESIGN TYPE | COMPRESSOR |
ENGINE SECTION LOCATION | COMPRESSOR |
OVERALL LENGTH | 2.499 INCHES MINIMUM AND 2.508 INCHES MAXIMUM |
OVERALL WIDTH | 1.095 INCHES MINIMUM AND 1.106 INCHES MAXIMUM |
MATERIAL THICKNESS | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM |
SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
CRITICALITY CODE JUSTIFICATION | AGAV |
END ITEM IDENTIFICATION | ENGINE MODEL TF33 |