Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-159-6761 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: 479314, 2840-01-159-6761, 01-159-6761, 2840011596761, 011596761
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 12, 1983 | 01-159-6761 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-159-6761
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 479314 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-159-6761
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 1.100 INCHES MINIMUM AND 1.120 INCHES MAXIMUM |
| DIAMETER | 18.490 INCHES MINIMUM AND 18.510 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF33-34 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |