Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-087-6637 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: 4051621, 4051621, 2840-01-087-6637, 01-087-6637, 2840010876637, 010876637
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 21, 1979 | 01-087-6637 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-087-6637
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4051621 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4051621 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-087-6637
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 0.135 INCHES MINIMUM AND 0.145 INCHES MAXIMUM |
| DIAMETER | 16.800 INCHES MINIMUM AND 16.820 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-100 |