Part Details | AIRCRAFT GAS TURBINE ENGINE THERMAL INSULATION BLANKET
2840-01-203-1966 A flexible covering, fabricated from appropriate insulating materials, designed to reduce thermal radiation in the hot section of an ENGINE, GAS TURBINE, AIRCRAFT. See also SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 7112M54P01, 7112M54P01, 10010361, 10-010361, 7112M54P01, 42H29927, 2840-01-203-1966, 01-203-1966, 2840012031966, 012031966
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 12, 1985 | 01-203-1966 | 50579 ( INSULATION BLANKET, THERMAL, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-203-1966
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 7112M54P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 7112M54P01 | 03350 | GENERAL ELECTRIC COMPANYDBA GE STRUCTURED SERVICES DIV |
| 10-010361 | 54787 | THERMAL STRUCTURES, INC. |
| 7112M54P01 | 22013 | TIGHITCO INC. |
| 42H29927 | 22013 | TIGHITCO INC. |
Technical Data | NSN 2840-01-203-1966
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 10.880 INCHES NOMINAL |
| OVERALL WIDTH | 10.260 INCHES NOMINAL |
| MATERIAL THICKNESS | 1.630 INCHES NOMINAL |
| TEMP RATING | 2000.0 DEG FAHRENHEIT |
| SPECIAL FEATURES | MATERIAL IS STEEL,CORROSION RESISTING & SHEET FIBER, CERAMIC; LAYER THICKNESS 0.004 IN. |