Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE
2840-01-436-9778 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: 4082750, 4082750, 2840-01-436-9778, 01-436-9778, 2840014369778, 014369778
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 02, 1996 | 01-436-9778 | 50611 ( VANE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-436-9778
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4082750 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4082750 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-436-9778
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 12.861 INCHES MINIMUM AND 12.901 INCHES MAXIMUM |
| OVERALL WIDTH | 2.075 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F100-24, FIG 121, IND 8; USED ON THE FAN INLET CASE, TT2 SENSING IMMERSION THERMOCOUPLE; USE ONLY ON P/N 4082495 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AABHP$$AABMK$$AFEAT |
| END ITEM IDENTIFICATION | F100-220 AIRCRAFT GAS TURBINE ENGINE |