Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-448-7033 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: 408274801, 4082748-01, 4082748, 408274801, 4082748-01, 2840-01-448-7033, 01-448-7033, 2840014487033, 014487033
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1997 | 01-448-7033 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-7033
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4082748-01 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4082748 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4082748-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-448-7033
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 0.154 INCHES MINIMUM AND 0.166 INCHES MAXIMUM |
| OVERALL WIDTH | 0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM |
| DIAMETER | 19.626 INCHES MINIMUM AND 19.630 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 86, IND 19G; SEAL CONTAINS BRUSH WIRE PACK THAT HAS 2250-2650 WIRES PER CIRCUMFERENTIAL INCH; USE ONLY ON P/NS 4083194, 4083560 AND 4083565; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY, TURBINE STATOR SUPPORT |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMZ$$AABMK$$ACZBJ$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BRUSHSEAL,INNER |