Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-416-1134 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: 30907422, 3090742-2, 2840-01-416-1134, 01-416-1134, 2840014161134, 014161134
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 13, 1995 | 01-416-1134 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-416-1134
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3090742-2 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-416-1134
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| OVERALL LENGTH | 0.623 INCHES MINIMUM AND 0.649 INCHES MAXIMUM |
| DIAMETER | 21.890 INCHES MINIMUM AND 21.900 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F1042-4, FIG 72, IND 1; RING, RETAINING SHOUD SEGMENT; NICKEL ELECTROPLATED |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AABHP$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | PACER DAWN |