NSN 2840-00-395-7030
Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-00-395-7030 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: 665E769G02, 665E769G02, 665E769G02, 2840-00-395-7030, 00-395-7030, 2840003957030, 003957030
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 12, 1974 | 00-395-7030 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-395-7030
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 665E769G02 | 60168 | ENGINETICS CORPORATIONDBA ENGINETICS AERO SPACE |
| 665E769G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 665E769G02 | 16126 | UNISON ENGINE COMPONENTS INC.DBA UNISON ENGINE COMPONENTS |
Technical Data | NSN 2840-00-395-7030
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 1.380 INCHES MINIMUM AND 1.420 INCHES MAXIMUM |
| DIAMETER | 36.400 INCHES MINIMUM AND 36.440 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF39-4, FIG 62, IND 60 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$ACZCJ$$AABHP$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | ENGINE,ACFT,MODEL-TF39-1A |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL,SUPPORT,NOZZLE |
