Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE ASSEMBLY
2840-01-372-1069 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: 408017901, 4080179-01, 407834901, 4078349-01, 2840-01-372-1069, 01-372-1069, 2840013721069, 013721069
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 03, 1993 | 01-372-1069 | 50607 ( VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-372-1069
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4080179-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4078349-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-372-1069
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 9 |
| OVERALL LENGTH | 6.680 INCHES NOMINAL |
| OVERALL WIDTH | 2.715 INCHES MINIMUM AND 2.727 INCHES MAXIMUM |
| DIAMETER | 23.321 INCHES MINIMUM AND 23.325 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 96, IND 104, 105 AND 106; USE ONLY ON 4080084-05, -06, -08 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PWO229 AIRCRAFT ENGINE |