Part Details | AIRCRAFT GAS TURBINE ENGINE HEAT SHIELD
2840-00-018-3114 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: 868C746P1, 868C746P1, 5017M30P01, 42H24781, 2840-00-018-3114, 00-018-3114, 2840000183114, 000183114
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 20, 1967 | 00-018-3114 | 50356 ( SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-018-3114
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 868C746P1 | 24446 | GENERAL ELECTRIC COMPANY |
| 868C746P1 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 5017M30P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 42H24781 | 78741 | HITCO CARBON COMPOSITES, INC. |
Technical Data | NSN 2840-00-018-3114
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 9.600 INCHES MINIMUM AND 9.840 INCHES MAXIMUM |
| OVERALL WIDTH | 5.710 INCHES MINIMUM AND 5.790 INCHES MAXIMUM |
| SPECIAL FEATURES | 4.270-4.310 WIDTH OF 2ND END |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMK$$ACZBJ$$AFEAT |
| END ITEM IDENTIFICATION | ACFT ENG J47 |