Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE SUPPORT
2840-01-187-8178 A support used for a NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 9993M67G02, 1285M66G02, 9993M67G02, 2840-01-187-8178, 01-187-8178, 2840011878178, 011878178
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 25, 1984 | 01-187-8178 | 51909 ( SUPPORT, TURBINE NOZZLE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-187-8178
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9993M67G02 | 58828 | CFM INTERNATIONAL, INC. |
| 1285M66G02 | 58828 | CFM INTERNATIONAL, INC. |
| 9993M67G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-187-8178
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| MOUNTING HOLE QUANTITY | 23 |
| MOUNTING HOLE DIAMETER | 0.481 INCHES MINIMUM AND 0.490 INCHES MAXIMUM |
| OVERALL LENGTH | 1.897 INCHES NOMINAL |
| OUTSIDE DIAMETER | 24.860 INCHES NOMINAL |
| INSIDE DIAMETER | 20.586 INCHES NOMINAL |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14, FIG. 72-41-00-1, IND. 30 |
| SPECIAL FEATURES | MATERIAL INCOLOY 903 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F108 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SUPPORT-SEAL OUTER HPT STTR. |