Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR FRAME
2840-01-268-2008 A frame used for and part of a COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE. May include struts with or without variable guide vanes.
Alternate Parts: 4007T78G08, 4007T78G07, 2840-01-268-2008, 01-268-2008, 2840012682008, 012682008
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 25, 1987 | 01-268-2008 | 52339 ( FRAME, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-268-2008
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4007T78G08 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 4007T78G07 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-268-2008
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 4.427 INCHES MINIMUM AND 4.431 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 16.995 INCHES MINIMUM AND 17.005 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | T.O. 2J-J85-94 FIG 11 IND 1 OR FIG 3 IND 13 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABKV |
| END ITEM IDENTIFICATION | J85-GE-21B AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MAINFRAME AND BRACKET ASSY |