Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-198-7322 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: 9395M62G02, 9395M62G02, 1304M93G08, 1304M93G05, 1304M93G02, 2840-01-198-7322, 01-198-7322, 2840011987322, 011987322
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 11, 1985 | 01-198-7322 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-198-7322
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9395M62G02 | 60168 | ENGINETICS CORPORATIONDBA ENGINETICS AERO SPACE |
| 9395M62G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1304M93G08 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1304M93G05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1304M93G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-198-7322
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 1.435 INCHES MINIMUM AND 1.455 INCHES MAXIMUM |
| DIAMETER | 38.280 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-TF39-4; 3 PIECES FORMING OUTER RADIUS OF 180 DEGREES OF FULL CIRCLE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |