Part Details | AIRCRAFT GAS TURBINE ENGINE FAN FRAME
2840-01-266-5905 A frame used for and part of the fan section of an aircraft gas turbine engine. May include struts with or without variable guide vanes.
Alternate Parts: 5052M50G19, 5052M50, 5052M50G19, 2840-01-266-5905, 01-266-5905, 2840012665905, 012665905
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 28, 1987 | 01-266-5905 | 52343 ( FRAME, FAN, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-266-5905
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5052M50G19 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 5052M50 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 5052M50G19 | 98912 | JET ENGINE TECHNOLOGY CORPORATION |
Technical Data | NSN 2840-01-266-5905
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5643 ASSN STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 6.945 INCHES MINIMUM AND 6.969 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 35.983 INCHES MINIMUM AND 35.987 INCHES MAXIMUM |
| INSIDE DIAMETER | 14.360 INCHES MINIMUM AND 14.400 INCHES MAXIMUM |
| NUMBER OF VARIABLE GUIDE VANES | 6 |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 9, IND 133 |
| END ITEM IDENTIFICATION | ACFT.ENG. F110 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE,COMPRESSOR,TURBINE ENGINE |