Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT
2840-01-322-2051 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: 4071453, 2840-01-322-2051, 01-322-2051, 2840013222051, 013222051
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 29, 1990 | 01-322-2051 | 50603 ( SHROUD SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-322-2051
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4071453 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-322-2051
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 0.532 INCHES MINIMUM AND 0.542 INCHES MAXIMUM |
| OVERALL WIDTH | 3.825 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.050 INCHES MINIMUM AND 0.060 INCHES MAXIMUM |
| DIAMETER | 20.480 INCHES MINIMUM AND 20.500 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54; 35 HOLES EQ SP 0.520-0.540 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |