Part Details | AIRCRAFT GAS TURBINE ENGINE METALLIC SEAL
2840-01-022-0859 A single or multi-piece item of metallic construction, specifically designed to form either a tight fuel or oil seal in an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 565720, 565720, 565720, 565720, 2840-01-022-0859, 01-022-0859, 2840010220859, 010220859
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 24, 1976 | 01-022-0859 | 50597 ( SEAL, METALLIC, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-022-0859
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 565720 | 76468 | MORGANITE INC |
| 565720 | 33870 | PRAXAIR SURFACE TECHNOLOGIES, INC.DBA PRAXAIR |
| 565720 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 565720 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-022-0859
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 1.215 INCHES MINIMUM AND 1.225 INCHES MAXIMUM |
| DIAMETER | 6.873 INCHES MINIMUM AND 6.875 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF33-14, FIG 4, IND 41A; USED ON THE NO. 1 BEARING, SUPPORT COMPRESSOR INLET CONE; MATL IS GRAPHITE CARBON |
| CRITICALITY CODE JUSTIFICATION | AMATT$$ACZBJ$$AABHP$$AABMZ |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CARBON SEAL,ENGINE |