Part Details | AIRCRAFT GAS TURBINE ENGINE REAR FRAME
2840-01-118-3521 A frame used for and part of the rear section of an aircraft gas turbine engine. May include struts.
Alternate Parts: 4009T25G08, 2840-01-118-3521, 01-118-3521, 2840011183521, 011183521
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 02, 1981 | 01-118-3521 | 52347 ( FRAME, REAR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-118-3521
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4009T25G08 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-118-3521
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| OVERALL LENGTH | 4.524 INCHES NOMINAL |
| OUTSIDE DIAMETER | 17.000 INCHES NOMINAL |
| INSIDE DIAMETER | 15.515 INCHES NOMINAL |
| NUMBER OF VARIABLE GUIDE VANES | 6 |
| REFERENCE DATA AND LITERATURE | T.O. 2J-J85-74, FIG 3, IND 53 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABKV$$AAARX |
| END ITEM IDENTIFICATION | ACFT ENG J-85 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME FRAME ASSY,MAIN |