Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-430-8689 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: 4083269, 4083269, 4083269, 2840-01-430-8689, 01-430-8689, 2840014308689, 014308689
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 03, 1996 | 01-430-8689 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-430-8689
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083269 | 8M212 | KENTUCKY METALS INC |
| 4083269 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4083269 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-430-8689
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 5 |
| OVERALL LENGTH | 31.932 INCHES MINIMUM AND 31.976 INCHES MAXIMUM |
| OVERALL WIDTH | 0.418 INCHES MINIMUM AND 0.428 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 165 IND 22D;USE ONLY ON P/N 4060645; CELLULAR STRUCTURAL HONEYCOMB |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$ACZCJ$$AABHP$$AABMK$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-100/200 AIRCRAFT GAS TURBINE ENGINE |