Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-448-7032 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: 408355901, 4083559-01, 4083559, 408323701, 4083237-01, 4083237, 2840-01-448-7032, 01-448-7032, 2840014487032, 014487032
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1997 | 01-448-7032 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-7032
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083559-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4083559 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4083237-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4083237 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-448-7032
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.475 INCHES MINIMUM AND 1.495 INCHES MAXIMUM |
| DIAMETER | 15.357 INCHES MINIMUM AND 15.367 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 86, IND 4; LOCATION NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY; USE ONLY ON P/NS 4084522-801 AND -802, 4082654-803 AND 4082657-808 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AABHP$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME RING-AIR SEALING,TURBINE ASSEMBLY |