Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR CASE
2840-01-189-2633 A case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and protect a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 9992M69G40, 9513M64G02, 1276M13G11, 1276M13G08, 1276M13G07, 1276M13G05, 1276M13G04, 1276M13G05, 2840-01-189-2633, 01-189-2633, 2840011892633, 011892633
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 13, 1984 | 01-189-2633 | 50547 ( CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-189-2633
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9992M69G40 | 58828 | CFM INTERNATIONAL, INC. |
| 9513M64G02 | 58828 | CFM INTERNATIONAL, INC. |
| 1276M13G11 | 58828 | CFM INTERNATIONAL, INC. |
| 1276M13G08 | 58828 | CFM INTERNATIONAL, INC. |
| 1276M13G07 | 58828 | CFM INTERNATIONAL, INC. |
| 1276M13G05 | 58828 | CFM INTERNATIONAL, INC. |
| 1276M13G04 | 58828 | CFM INTERNATIONAL, INC. |
| 1276M13G05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-189-2633
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 22.000 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14 FIG 72-32-00-05 IND 400L |
| END ITEM IDENTIFICATION | ACFT ENG F108 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CASE ASSY-FRONT & EXTENSION CPRSR STTR |