Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-068-2048 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: 37D401302P103, 37D401302P103, 37D401302P103, 37D401302P103, 2840-01-068-2048, 01-068-2048, 2840010682048, 010682048
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 17, 1978 | 01-068-2048 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-068-2048
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37D401302P103 | 98247 | CANADIAN COMMERCIAL CORPORATION |
| 37D401302P103 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 37D401302P103 | 03350 | GENERAL ELECTRIC COMPANYDBA GE STRUCTURED SERVICES DIV |
| 37D401302P103 | 35013 | ORENDA AEROSPACE CORPORATION |
Technical Data | NSN 2840-01-068-2048
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 1.450 INCHES MINIMUM AND 1.453 INCHES MAXIMUM |
| DIAMETER | 10.440 INCHES MINIMUM AND 10.450 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-J85-54; LIFE LIMITED |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J85-GE-5,-13,-17 |