Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE CASE
2840-01-448-7540 A case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and protect a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 4083210, 4083210, 4083210, 2840-01-448-7540, 01-448-7540, 2840014487540, 014487540
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1997 | 01-448-7540 | 50553 ( CASE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-7540
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083210 | 1645F | HANWHA TECHWIN CO.,LTDDIV PS BUSINESS UNIT |
| 4083210 | 9Y765 | NUMET MACHINING TECHNIQUES, INC.DIV NUMET MACHINING TECHNIQUES |
| 4083210 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-448-7540
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 5.809 INCHES MINIMUM AND 5.813 INCHES MAXIMUM |
| DIAMETER | 28.330 INCHES MINIMUM AND 28.350 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 89, IND 71; USE ONLY ON P/N 4084522-800, -801, -802, 4082654-803, AND 4082657-808; LOCATION NEAR NO. 4 BEARING FRONT AIR SEALING RING, FRONT SEAL ASSY, COMPRESSOR EXIT STATOR AND DIFFUSER CASE |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AABMZ$$AABHP$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |