Part Details | AIRCRAFT GAS TURBINE ENGINE HEAT SHIELD
2840-00-117-4858 A rigid item, fabricated from a heat resistant allow, with or without insulation material added. Designed to protect parts, areas or systems of an ENGINE, GAS TURBINE, AIRCRAFT from excessive heat damage. See also INSULATION BLANKET, THERMAL, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 9632M28P15, 9632M28P12, 9632M28P07, 9632M28, 383019015, 3-830190-15, 383019012, 3-830190-12, 42H24847P07, 2840-00-117-4858, 00-117-4858, 2840001174858, 001174858
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 04, 1968 | 00-117-4858 | 50356 ( SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-117-4858
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9632M28P15 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9632M28P12 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9632M28P07 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9632M28 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 3-830190-15 | 54787 | THERMAL STRUCTURES, INC. |
| 3-830190-12 | 54787 | THERMAL STRUCTURES, INC. |
| 42H24847P07 | 22013 | TIGHITCO INC. |
Technical Data | NSN 2840-00-117-4858
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-TF39-4; GOES ON THE NOZZLE SECTION; STAGE 3; LOW PRESSURE TURBINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF-39 |