Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-438-8397 A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 1559M63G02118, 1559M63G02-118, 2840-01-438-8397, 01-438-8397, 2840014388397, 014388397
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 20, 1996 | 01-438-8397 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-438-8397
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1559M63G02-118 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
Technical Data | NSN 2840-01-438-8397
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 6.143 INCHES MINIMUM AND 6.163 INCHES MAXIMUM |
| DIAMETER | 17.300 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F110-14, FIG 67, IND 5 UNDER P/N 1559M63G02; INCLUDES STAGE 2; ALSO CONSISTS NO. 1 DISK AND NO. 2 DISK AND FORWARD SHAFT THAT MAKES A 1 PIECE CONSTRUCTION THAT HOLDS BOTH STGS; WEIGHTS 40.3 LBS; BASIC P/N CAN BE USED ON ALL ENGINE TYPES, BUT ONCE USED ON THE F118, IT CAN ONLY BE USED ON AN F118 ENGINE; REIDENTIFICATION WILL CONSIST OF ADDING THE ENGINE TYPE AS A DASH NUMBER FOLLOWING THE P/N |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$AABHP$$AABMZ$$ACZBJ |
| END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SPOOL,COMPRESSOR ROTOR |