Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-451-5473 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: 4083150, 2840-01-451-5473, 01-451-5473, 2840014515473, 014515473
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 19, 1997 | 01-451-5473 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-451-5473
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083150 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-451-5473
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 0.664 INCHES NOMINAL |
| DIAMETER | 19.448 INCHES NOMINAL |
| SPECIAL FEATURES | USED ON THE FRONT COMPRESSOR ROTOR AND STATOR ASSEMBLY; REPLACED P/N 4071083 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AABHP$$AABMZ$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54, FIG 70, IND 25 |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |