Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT
2840-01-175-3023 A stationary arched metal segment used to establish clearance and a seal for the tip of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a SEAL RING, LABYRINTH, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 9523M21P01, 9523M21P01, 9532M21P01, 9532M21P01, 9532M21P01, 9523M21P01, 9532M21P01, 9523M21P01, 9523M21P01, 9532M21P01, 9532M21P01, 9532M21P01, 9532M21P01, 9532M21P01, 9523M21P01, 9523M21P01, 9532M21P01, 2840-01-175-3023, 01-175-3023, 2840011753023, 011753023
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 29, 1984 | 01-175-3023 | 50603 ( SHROUD SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-175-3023
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9523M21P01 | 02GZ1 | ADOM ENGINEERING, INC. |
| 9523M21P01 | 58828 | CFM INTERNATIONAL, INC. |
| 9532M21P01 | 8U485 | COLUMBIA MANUFACTURING, INC |
| 9532M21P01 | 33617 | ELECTRO-METHODS INC |
| 9532M21P01 | 4J952 | GENERAL AVIATION |
| 9523M21P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9532M21P01 | 47940 | HI-TEK MFG INC |
| 9523M21P01 | 57488 | LKM INDUSTRIES, INC.DBA LKM |
| 9523M21P01 | 13779 | LPI INDUSTRIES CORPORATIONDBA L P I |
| 9532M21P01 | 13779 | LPI INDUSTRIES CORPORATIONDBA L P I |
| 9532M21P01 | 9Y765 | NUMET MACHINING TECHNIQUES, INC.DIV NUMET MACHINING TECHNIQUES |
| 9532M21P01 | 24115 | PALMER MANUFACTURING CO., LLCDBA P M C |
| 9532M21P01 | 34336 | TECT AEROSPACE INC.DBA TECT AEROSPACE SOUTHWEST |
| 9532M21P01 | 28884 | TSS TECHNOLOGIES, INC.DBA TSS MEDICAL |
| 9523M21P01 | 16190 | UNISON ENGINE COMPONENTS INC |
| 9523M21P01 | 03550 | VANGUARD ELECTRONICS COMPANY |
| 9532M21P01 | 58199 | W M Z MFG CO INC |
Technical Data | NSN 2840-01-175-3023
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 0.254 INCHES MINIMUM AND 0.375 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.077 INCHES MINIMUM AND 0.085 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F108-4; HIGH PRESSURE TURBINE SHROUD AND 1ST STAGE L.P. TURBINE NOZZLE; U-SHAPED CLIPS |
| END ITEM IDENTIFICATION | B1B ACFT/F108 ACFT ENGINE |