NSN 2840-00-227-8889
Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-00-227-8889 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: 555665, 555665, 309770, 2840-00-227-8889, 00-227-8889, 2840002278889, 002278889
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 03, 1969 | 00-227-8889 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-227-8889
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 555665 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 555665 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 309770 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-227-8889
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 10 |
| OVERALL LENGTH | 1.134 INCHES MINIMUM AND 1.154 INCHES MAXIMUM |
| DIAMETER | 24.900 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-J75-4, FIG 13, IND 12; CASE-REAR COMPRESSOR FRONT |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$ASFTT$$AABMZ$$AABHP$$AFEAT |
| END ITEM IDENTIFICATION | J-75 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME RING,COMPRESSOR ROTOR,AIRCRAFT GAS TURBINE ENGINE |
