Part Details | AIRCRAFT GAS TURBINE ENGINE FRONT FRAME
2840-01-190-9258 A frame used for and part of the front section of an aircraft gas turbine engine. May include struts with or without variable guide vanes.
Alternate Parts: 9521M53G01, 9521M13G02, 9521M13G01, 9521M53G01, 9521M53G01, 2840-01-190-9258, 01-190-9258, 2840011909258, 011909258
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 04, 1984 | 01-190-9258 | 52345 ( FRAME, FRONT, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-190-9258
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9521M53G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9521M13G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9521M13G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9521M53G01 | 5U018 | ISRAEL AIRCRAFT INDUSTRIES LTDMARKETING DIRECTORATE |
| 9521M53G01 | 98912 | JET ENGINE TECHNOLOGY CORPORATION |
Technical Data | NSN 2840-01-190-9258
| Characteristic | Specifications |
|---|---|
| NUMBER OF VARIABLE GUIDE VANES | 17 |
| REFERENCE DATA AND LITERATURE | 2J-F110-4, FIG 1, IND 1 |
| SPECIAL FEATURES | AXIAL COMPRESSOR; FRAME ASSY HAS VARIABLE STRUTS |
| END ITEM IDENTIFICATION | F110 ACFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE AND NOZZLE ASSEMBLY,TURBINE,AIRCRAFT |