Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-168-1326 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: 800219, 800219, 2840-01-168-1326, 01-168-1326, 2840011681326, 011681326
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 13, 1983 | 01-168-1326 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-168-1326
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 800219 | 9Y765 | NUMET MACHINING TECHNIQUES, INC.DIV NUMET MACHINING TECHNIQUES |
| 800219 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-168-1326
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 4 |
| OVERALL LENGTH | 1.950 INCHES MINIMUM AND 1.970 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF33-4; SAME AS PN 570634BUT REINDENTIFIED FOR PACER GRADE ENGINES |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG32, IND38 |
| END ITEM IDENTIFICATION | ACFT TF33 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RING AIR SEALING TURBINE 4 STAGE |