Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-190-8191 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: 2183505, 2183505, 2183505, 2183505, 2183505, 2183505, 2183505, 2840-01-190-8191, 01-190-8191, 2840011908191, 011908191
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 02, 1984 | 01-190-8191 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-190-8191
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2183505 | 54850 | AMBEL PRECISION MANUFACTURINGCORPORATION |
| 2183505 | 32816 | BEACON INDUSTRIES, INC. |
| 2183505 | 02382 | EDAC TECHNOLOGIES CORPORATIONDBA GROS-IT INDUSTRIES |
| 2183505 | 15014 | MACHINE PRODUCTS CO INC |
| 2183505 | 50381 | MTU AERO ENGINE COMPONENTS INC |
| 2183505 | 60822 | PEGO CORP |
| 2183505 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-190-8191
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 11 |
| OVERALL LENGTH | 1.571 INCHES MINIMUM AND 1.588 INCHES MAXIMUM |
| DIAMETER | 14.877 INCHES MINIMUM AND 14.897 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF30-44, FIG 15, IND 6; REAR COMPRESSOR ROTOR |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AABHP$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | ACFT ENG TF30 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL,AIR,COMPRESSOR,STAGE 11 |