Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE ASSEMBLY
2840-01-345-4790 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: 407707901, 4077079-01, 2840-01-345-4790, 01-345-4790, 2840013454790, 013454790
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 19, 1991 | 01-345-4790 | 50607 ( VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-345-4790
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4077079-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-345-4790
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 9 |
| OVERALL LENGTH | 2.675 INCHES MINIMUM AND 2.687 INCHES MAXIMUM |
| DIAMETER | 23.321 INCHES MINIMUM AND 23.325 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 95, IND 118 OR FIG 96, IND 104 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AAPGF$$ACZBJ$$ACZCJ |
| END ITEM IDENTIFICATION | F100-PW0-229 ACFT ENG/CORE MOD |