Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-367-4828 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: 408160903, 4081609-03, 407930903, 4079309-03, 408160903, 4081609-03, 407930903, 4079309-03, 2840-01-367-4828, 01-367-4828, 2840013674828, 013674828
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 13, 1992 | 01-367-4828 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-367-4828
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4081609-03 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4079309-03 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4081609-03 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4079309-03 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-367-4828
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 9 |
| OVERALL LENGTH | 1.905 INCHES NOMINAL |
| OVERALL WIDTH | 0.935 INCHES MINIMUM AND 0.943 INCHES MAXIMUM |
| SPECIAL FEATURES | SUPERSEDES P/N 4075609-03, 4077509-03 AND 4079309-03 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMK$$ACZBJ$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54, FIG 104, IND 35 |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT ENGINE |
