Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE ASSEMBLY
2840-01-322-6280 A stationary item designed for the purpose of directing air at the proper angle and velocity from a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle.
Alternate Parts: 1476M28G01, 1476M28G01, 1476M28G01, 2840-01-322-6280, 01-322-6280, 2840013226280, 013226280
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 11, 1990 | 01-322-6280 | 50607 ( VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-322-6280
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1476M28G01 | 33617 | ELECTRO-METHODS INC |
| 1476M28G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1476M28G01 | 50595 | TWIGG CORPORATION |
Technical Data | NSN 2840-01-322-6280
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 8 |
| OVERALL LENGTH | 5.869 INCHES MINIMUM AND 5.875 INCHES MAXIMUM |
| OVERALL WIDTH | 1.196 INCHES NOMINAL |
| DIAMETER | 19.304 INCHES NOMINAL |
| SPECIAL FEATURES | 11 VANES BASED UPON 110 VANES EQ SP; SECTION IS 35 DEG 25 MIN 9 SEC OF WHOLE ASSY |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110GE100 AIRCRAFT ENGINE |