Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-01-451-5504 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: 4083240, 2840-01-451-5504, 01-451-5504, 2840014515504, 014515504
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 19, 1997 | 01-451-5504 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-451-5504
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083240 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-451-5504
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 0.852 INCHES MINIMUM AND 0.862 INCHES MAXIMUM |
| DIAMETER | 16.725 INCHES MINIMUM AND 16.735 INCHES MAXIMUM |
| SPECIAL FEATURES | INSIDE DIAMETER 14.550-14.530 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMZ$$ACZBJ$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54 FIG 73 IND 50 |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |