Part Details | AIRCRAFT GAS TURBINE ENGINE REAR FRAME
2840-01-268-2786 A frame used for and part of the rear section of an aircraft gas turbine engine. May include struts.
Alternate Parts: 4009T25G11, 2840-01-268-2786, 01-268-2786, 2840012682786, 012682786
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 26, 1987 | 01-268-2786 | 52347 ( FRAME, REAR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-268-2786
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4009T25G11 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-268-2786
| 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 85-GE-17,17A |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME FRAME ASSEMBLY,ENGINE |