NSN 2840-00-767-8337
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-00-767-8337 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: 254513, 364913, 254513, 364913, 254513, 364913, 2840-00-767-8337, 00-767-8337, 2840007678337, 007678337
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | JAN 01, 1962 | 00-767-8337 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-767-8337
Part Number | Cage Code | Manufacturer |
---|---|---|
254513 | 33755 | AIRFOIL TEXTRON INCSUB OF TEXTRON INC |
364913 | 65115 | TURBINE ENGINE COMPONENTS TEXTRON |
254513 | 8W315 | TURBINE ENGINE COMPONENTSTECHNOLOGIES CORPORATION |
364913 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
254513 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
364913 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-767-8337
Characteristic | Specifications |
---|---|
DESIGN TYPE | COMPRESSOR |
ENGINE SECTION LOCATION | COMPRESSOR |
OVERALL LENGTH | 2.478 INCHES MINIMUM AND 2.507 INCHES MAXIMUM |
OVERALL WIDTH | 1.096 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 | TF33 AIRCRAFT ENGINE |