Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT
2840-01-313-6691 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: 9321M30P04, 2840-01-313-6691, 01-313-6691, 2840013136691, 013136691
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 13, 1990 | 01-313-6691 | 50603 ( SHROUD SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-313-6691
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9321M30P04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-313-6691
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 1.400 INCHES MINIMUM AND 1.406 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.660 INCHES NOMINAL |
| DIAMETER | 15.190 INCHES MINIMUM AND 15.192 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F110-14; SEGMENT IS 15 DEG 39 MIN 8 SEC OF FULL CIRCLE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110GE100/F110GE129 ACFT ENG |