NSN 2840-00-166-2356
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-166-2356 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: 753212, 726712, 625512, 2840-00-166-2356, 00-166-2356, 2840001662356, 001662356
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | FEB 09, 1973 | 00-166-2356 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-166-2356
Part Number | Cage Code | Manufacturer |
---|---|---|
753212 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
726712 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
625512 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-166-2356
Characteristic | Specifications |
---|---|
DESIGN TYPE | COMPRESSOR |
ENGINE SECTION LOCATION | COMPRESSOR |
OVERALL LENGTH | 2.782 INCHES MINIMUM AND 2.791 INCHES MAXIMUM |
OVERALL WIDTH | 1.160 INCHES MINIMUM AND 1.170 INCHES MAXIMUM |
MATERIAL THICKNESS | 0.493 INCHES MINIMUM AND 0.499 INCHES MAXIMUM |
SPECIAL FEATURES | TOLARANCE, FIT |
CRITICALITY CODE JUSTIFICATION | FEAT |
END ITEM IDENTIFICATION | ENGINE MODEL TF33 |