Part Details | AIRCRAFT GAS TURBINE ENGINE METALLIC SEAL
2840-01-387-7276 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: 1668M40G02, 1668M40G02, 1668M40, 1668M40G02, 1668M40G02, 1668M40G02, 1668M40G02, 2840-01-387-7276, 01-387-7276, 2840013877276, 013877276
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 10, 1994 | 01-387-7276 | 50597 ( SEAL, METALLIC, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-387-7276
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1668M40G02 | 33617 | ELECTRO-METHODS INC |
| 1668M40G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1668M40 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1668M40G02 | 50554 | METRO MACHINE WORKS, INC. |
| 1668M40G02 | 50595 | TWIGG CORPORATION |
| 1668M40G02 | 51992 | UNION MACHINE COMPANY OF LYNN, INC. |
| 1668M40G02 | 16126 | UNISON ENGINE COMPONENTS INC.DBA UNISON ENGINE COMPONENTS |
Technical Data | NSN 2840-01-387-7276
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| OVERALL LENGTH | 0.820 INCHES MINIMUM AND 0.840 INCHES MAXIMUM |
| DIAMETER | 15.150 INCHES MINIMUM AND 15.160 INCHES MAXIMUM |
| SPECIAL FEATURES | MATL SPEC B50TF14 CL-A; HONEYCOMB PATTERN; RIBBON THK 0.0027-0.0033; MATL OF RIBBON TITANIUM ALLOY, AMS 5536 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AAPGF$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | F110-100 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SEAL,HONEYCOMB |