NSN 2840-00-862-5697
Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-00-862-5697 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: 105B1884P1, 105R984P17, 105B1884P1, 105R984P17, 2840-00-862-5697, 00-862-5697, 2840008625697, 008625697
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-862-5697 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-862-5697
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 105B1884P1 | 24446 | GENERAL ELECTRIC COMPANY |
| 105R984P17 | 24446 | GENERAL ELECTRIC COMPANY |
| 105B1884P1 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 105R984P17 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-862-5697
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 1.880 INCHES MINIMUM AND 1.910 INCHES MAXIMUM |
| OVERALL WIDTH | 0.200 INCHES MINIMUM AND 0.240 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-J79-44 FIG 34, IND 9 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$ACZCJ$$AABHP$$AABMK$$AFEAT |
| END ITEM IDENTIFICATION | ACFT ENG J47,J79,T58 AND T64 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME STRIP,SEALING,TURBINE ENGINE |