Part Details | AIRCRAFT GAS TURBINE ENGINE HEAT SHIELD
2840-01-117-4508 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: 4001452, 4001452, 2840-01-117-4508, 01-117-4508, 2840011174508, 011174508
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 14, 1981 | 01-117-4508 | 50356 ( SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-117-4508
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4001452 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4001452 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-117-4508
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 2.023 INCHES MINIMUM AND 2.133 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.007 INCHES MINIMUM AND 0.012 INCHES MAXIMUM |
| SPECIAL FEATURES | MATL IS ALSO COBALT ALLOY PWA SPEC 1042 |
| END ITEM IDENTIFICATION | ACFT ENG F100 |