Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE ASSEMBLY
2840-01-205-7700 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: 4086558, 4067478, 4062378, 2840-01-205-7700, 01-205-7700, 2840012057700, 012057700
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 11, 1985 | 01-205-7700 | 50607 ( VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-205-7700
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4086558 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4067478 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4062378 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-205-7700
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 8 |
| OVERALL LENGTH | 2.189 INCHES NOMINAL |
| DIAMETER | 21.550 INCHES MINIMUM AND 21.570 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 168 IND 4; REID OF P/N 4064068; 15.712-15.716 IN. ID; IN COMPLETE SETS ONLY |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-220 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE |