Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-161-0474 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: 747059R1, 747059R1, 2840-01-161-0474, 01-161-0474, 2840011610474, 011610474
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 31, 1983 | 01-161-0474 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-161-0474
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 747059R1 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 747059R1 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-161-0474
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 9 |
| OVERALL LENGTH | 0.775 INCHES MINIMUM AND 0.805 INCHES MAXIMUM |
| DIAMETER | 20.585 INCHES MINIMUM AND 20.595 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF33-4, FIG 16, IND 15; UUSED ON THE INTERMEDIATE COMPRESSOR; NO. 2, 2 1/2 & 3 BEARINGS |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMZ$$ACZBJ$$AFEAT |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME RING,AIRSEAL,COMPRESSOR |