Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-320-6432 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: 4076459, 2840-01-320-6432, 01-320-6432, 2840013206432, 013206432
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 30, 1990 | 01-320-6432 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-320-6432
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4076459 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-320-6432
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 20.570 INCHES MINIMUM AND 20.630 INCHES MAXIMUM |
| SPECIAL FEATURES | REOP AND REID OF P/N 4072683 & 4057829; USED ON THE AUGMENTOR DIVERGENT NOZZLE SEAL SEGMENTS |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-24, FIG 146, IND 7 |
| END ITEM IDENTIFICATION | F100-229 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | T.O. NAME SEAL ASSEMBLY, AUGMENTOR DIVERGENT NOZZLE SEGMENT |