Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE
2840-01-435-8548 A component of a VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.
Alternate Parts: P221P05, 2840-01-435-8548, 01-435-8548, 2840014358548, 014358548
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 04, 1996 | 01-435-8548 | 50611 ( VANE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-435-8548
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P221P05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-435-8548
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | PIN |
| SPECIAL FEATURES | T.O. 2J-F110-14, FIG 62 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$ACZCJ$$ABGLW$$AFEAT |
| END ITEM IDENTIFICATION | F110 AIRCRAFT GAS TURBINE ENGINE |