Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-161-0467 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: 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 734824, 2840-01-161-0467, 01-161-0467, 2840011610467, 011610467
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 31, 1983 | 01-161-0467 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-161-0467
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 734824 | 26795 | A B A INDUSTRIES INC |
| 734824 | 54850 | AMBEL PRECISION MANUFACTURINGCORPORATION |
| 734824 | 32816 | BEACON INDUSTRIES, INC. |
| 734824 | 2V116 | DEMUSZ MFG. CO., INC. |
| 734824 | 33617 | ELECTRO-METHODS INC |
| 734824 | 01993 | FERROTHERM CORPORATION |
| 734824 | 06959 | FLANAGAN BROTHERS, INCDBA FLANAGAN INDUSTRIES |
| 734824 | 98839 | HANSEN ENGINEERING AND MACHINERYCO., INC. |
| 734824 | 55282 | J.T. SLOCOMB CORP |
| 734824 | 93596 | KERNS MANUFACTURING CORP. |
| 734824 | 57488 | LKM INDUSTRIES, INC.DBA LKM |
| 734824 | 8U294 | RDS MANUFACTURING, INC. |
| 734824 | 4A011 | STOWE MACHINE CO. INC. |
| 734824 | 31340 | THE BIRKEN MANUFACTURING COMPANY |
| 734824 | 15152 | TIMKEN AEROSPACE TRANSMISSIONS, LLC |
| 734824 | 33404 | TRW INC TRW COMPRESSOR COMPONENTS |
| 734824 | 51992 | UNION MACHINE COMPANY OF LYNN, INC. |
| 734824 | 50255 | UNISON ENGINE COMPONENTS, INC.DBA UNISON ENGINE COMPONENTS |
| 734824 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 734824 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-161-0467
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 1.350 INCHES MINIMUM AND 1.380 INCHES MAXIMUM |
| DIAMETER | 15.677 INCHES MINIMUM AND 15.679 INCHES MAXIMUM |
| SPECIAL FEATURES | 4TH STAGE INCLUDED |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |