Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK AND HUB
2840-00-979-8432 An item that consists of a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 110041705, 1-100-417-05, 110041702, 1-100-417-02, 110041705, 1-100-417-05, 2840-00-979-8432, 00-979-8432, 2840009798432, 009798432
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 12, 1966 | 00-979-8432 | 50561 ( DISK AND HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-979-8432
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-100-417-05 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1-100-417-02 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1-100-417-05 | D0272 | ROLLS-ROYCE DEUTSCHLAND LTD & CO KGDBA ROLLS-ROYCE DEUTSCHLAND |
Technical Data | NSN 2840-00-979-8432
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | TITANIUM ALLOY,M3400 FSCM 91547,ROCKWELL C SCALE 36 MAX HARDNESS,PAINTED FINISH,P6441 FSCM 91547,2.351 IN. NOM O/A LG,TAPERED OD DISK,7.274 IN. MIN,7.284 IN. MAX LARGEST OD DISK,7.146 IN. MIN,7.156 IN. MAX SMALLEST OD DISK,0.677 IN. MIN,0.682 IN. MAX LG DISK,38 BLADE GROOVES EQUALLY SPACED ON OUTER PERIPHERY,2 HUBS,1ST END 4.430 IN. MIN,4.440 IN. MAX OD HUB,1.202 IN. MIN,1.212 IN. MAX DISTANCE FROM 1ST END TO DISK,2ND END 4.421 IN. MIN,4.422 IN. MAX OD HUB,0.453 IN. MIN,0.466 IN. MAX DISTANCE FROM 2ND END TO DISK,4.082 IN. MIN,4.087 IN. MAX DIA BORE |