Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-444-7013 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: 1796M20G01, 2840-01-444-7013, 01-444-7013, 2840014447013, 014447013
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 14, 1997 | 01-444-7013 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-7013
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1796M20G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-444-7013
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 2.370 INCHES MINIMUM AND 2.450 INCHES MAXIMUM |
| DIAMETER | 28.730 INCHES MINIMUM AND 28.850 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF39-4, FIG 62, IND 31; ECP 369; DCN 97-37; HONEYCOMBED; INTERSSTAGE; REPL P/N 9083M60G05 BUT NOT TO BE GRPD PER ECP/DCN; WHOLE NEW CONFIGURATION; AS THE OLD CONFIG IS REPL BY TCTO KITS WITH THE NEW ITEMS, THE OLD CONFIG IS THROWN AWAY, NOT I&SABLE |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |