Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-192-7404 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: 4065120, 2840-01-192-7404, 01-192-7404, 2840011927404, 011927404
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 12, 1995 | 01-192-7404 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-192-7404
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4065120 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-192-7404
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 4 |
| SPECIAL FEATURES | REAR INLET; U/O 4070215-706; 4TH STG SYNCHRONIZING RIGN, CASE AND STATOR, DISK AND BLADES |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-24, FIG 143, IND 22 |
| END ITEM IDENTIFICATION | F100-PW-220/220E AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME AIRSEAL |