Part Details | AIRCRAFT GAS TURBINE ENGINE FRONT FRAME
2840-01-347-6914 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: 30911066, 3091106-6, 2840-01-347-6914, 01-347-6914, 2840013476914, 013476914
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 27, 1991 | 01-347-6914 | 52345 ( FRAME, FRONT, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-347-6914
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3091106-6 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-347-6914
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | EMS54914, TI6-4 MFR REF SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 4.718 INCHES MINIMUM AND 5.738 INCHES MAXIMUM |
| OUTSIDE DIAMETER | 20.660 INCHES NOMINAL |
| INSIDE DIAMETER | 12.480 INCHES NOMINAL |
| NUMBER OF VARIABLE GUIDE VANES | 20 |
| REFERENCE DATA AND LITERATURE | 2J-F1042-4, FIG 87, IND 100 |
| CRITICALITY CODE JUSTIFICATION | AABKV$$AAARX$$AABHP |
| END ITEM IDENTIFICATION | PACER DAWN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME FRAME ASSEMBLY,TURBINE ENGINE |