Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-184-8573 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: 4079076, 4064666, 2840-01-184-8573, 01-184-8573, 2840011848573, 011848573
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 24, 1984 | 01-184-8573 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-184-8573
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4079076 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4064666 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-184-8573
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 0.989 INCHES MINIMUM AND 1.349 INCHES MAXIMUM |
| DIAMETER | 13.495 INCHES MINIMUM AND 13.505 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-4, FIG 104, IND 3; BODY 11.907-11.917 OD; FLANGES 12.093-12.097 OD; HUB 11.780-11.790 OD; BORE 10.468-10.472 OD; FRONT COMPRESSOR INLET; TCTO 2J-F100(I)-512 |
| END ITEM IDENTIFICATION | ACFT ENG F-100 |