Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-320-5344 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: 407574101, 4075741-01, 407574101, 4075741-01, 407574101, 4075741-01, 407574101, 4075741-01, 2840-01-320-5344, 01-320-5344, 2840013205344, 013205344
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 26, 1990 | 01-320-5344 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-320-5344
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4075741-01 | 1645F | HANWHA TECHWIN CO.,LTDDIV PS BUSINESS UNIT |
| 4075741-01 | 16126 | UNISON ENGINE COMPONENTS INC.DBA UNISON ENGINE COMPONENTS |
| 4075741-01 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4075741-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-320-5344
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 1.866 INCHES MINIMUM AND 1.906 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.040 INCHES MINIMUM AND 0.050 INCHES MAXIMUM |
| DIAMETER | 18.335 INCHES MINIMUM AND 18.345 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 ENGINE/FDT MOD |