Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-171-0876 A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an ENGINE, GAS TURBINE, AIRCRAFT. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.
Alternate Parts: AGC 3247, 9941M63P03, 9941M63P02, 9941M63P01, SY99203, SY9920-3, 2840-01-171-0876, 01-171-0876, 2840011710876, 011710876
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 03, 1984 | 01-171-0876 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-171-0876
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AGC 3247 | 98500 | AGC ACQUISITION LLC |
| 9941M63P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9941M63P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9941M63P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| SY9920-3 | 95272 | STILLMAN SEAL CORPORATION |
Technical Data | NSN 2840-01-171-0876
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 1.780 INCHES MINIMUM AND 1.820 INCHES MAXIMUM |
| OVERALL WIDTH | 1.080 INCHES MINIMUM AND 1.120 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F101-4, FIG 70, IND 14; USED IN THE AUGMENTOR LINER |
| CRITICALITY CODE JUSTIFICATION | AMATT$$AABHP$$AABMK$$AAGAV |
| END ITEM IDENTIFICATION | ACFT ENG F101 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL,FUEL |