NSN 2840-00-348-6236
Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-00-348-6236 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: 4038410, 4038410, 4038410, 2840-00-348-6236, 00-348-6236, 2840003486236, 003486236
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 26, 1974 | 00-348-6236 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-348-6236
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4038410 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4038410 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4038410 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-348-6236
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 1.104 INCHES MINIMUM AND 1.106 INCHES MAXIMUM |
| OVERALL HEIGHT | 0.430 INCHES MINIMUM AND 0.450 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.005 INCHES MINIMUM AND 0.007 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-4; GOES ON THE AUGMENTOR CONVERGENT NOZZLE SEGMENT; METALLIC HARDNESS DPH 353 MIN OR EQUIVALENT |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE,ACFT,TURBO-FAN,MODEL F100PW100 |
