Part Details | AIRCRAFT GAS TURBINE ENGINE AIR SEAL
2840-00-111-7745 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: 9686M18P38, 9686M18P13, 9686M18P09, 9686M18P38, 2840-00-111-7745, 00-111-7745, 2840001117745, 001117745
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 21, 1968 | 00-111-7745 | 50595 ( SEAL, AIR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-111-7745
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9686M18P38 | 02653 | BERKSHIRE MANUFACTURED PRODUCTS,INC. |
| 9686M18P13 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9686M18P09 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9686M18P38 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-111-7745
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.765 INCHES MINIMUM AND 1.785 INCHES MAXIMUM |
| OVERALL WIDTH | 0.135 INCHES MINIMUM AND 0.145 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.008 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-TF39-4;TURBINE NOZZLE ASSY |
| END ITEM IDENTIFICATION | ACFT ENG TF-39 |