Part Details | AIRCRAFT GAS TURBINE ENGINE HEAT SHIELD
2840-01-187-8261 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: 9523M58P01, 9523M58P01, 9523M58P01, 2840-01-187-8261, 01-187-8261, 2840011878261, 011878261
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 25, 1984 | 01-187-8261 | 50356 ( SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-187-8261
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9523M58P01 | 58828 | CFM INTERNATIONAL, INC. |
| 9523M58P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9523M58P01 | 03350 | GENERAL ELECTRIC COMPANYDBA GE STRUCTURED SERVICES DIV |
Technical Data | NSN 2840-01-187-8261
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 2.230 INCHES MINIMUM AND 2.250 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.028 INCHES MINIMUM AND 0.036 INCHES MAXIMUM |
| DIAMETER | 16.360 INCHES MINIMUM AND 16.380 INCHES MAXIMUM |
| SPECIAL FEATURES | MATL B50TF14 CL-A (INCO 718) |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F108 AIRCRAFT ENGINE |