NSN 2840-00-395-7201
Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-00-395-7201 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: 4050979CL2, 4043279CL2, 2840-00-395-7201, 00-395-7201, 2840003957201, 003957201
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 12, 1974 | 00-395-7201 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-395-7201
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4050979CL2 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4043279CL2 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-395-7201
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 10 |
| OVERALL LENGTH | 1.705 INCHES MINIMUM AND 1.729 INCHES MAXIMUM |
| DIAMETER | 16.310 INCHES MINIMUM AND 16.330 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 138, IND 2 |
| END ITEM IDENTIFICATION | F-100 AIRCRAFT ENGINE |
| FSC APPLICATION DATA | F15 ACFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SEAL,COMPRESSOR |
