Part Details | AIRCRAFT GAS TURBINE ENGINE THERMAL INSULATION BLANKET
2840-00-113-6507 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: 9682M38P04, 9682M38P02, 42H261002, 42H26100-2, 38302014, 3-830201-4, 38302012, 3-830201-2, 42H261002, 42H26100-2, 2840-00-113-6507, 00-113-6507, 2840001136507, 001136507
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 04, 1968 | 00-113-6507 | 50579 ( INSULATION BLANKET, THERMAL, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-113-6507
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9682M38P04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9682M38P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 42H26100-2 | 78741 | HITCO CARBON COMPOSITES, INC. |
| 3-830201-4 | 54787 | THERMAL STRUCTURES, INC. |
| 3-830201-2 | 54787 | THERMAL STRUCTURES, INC. |
| 42H26100-2 | 22013 | TIGHITCO INC. |
Technical Data | NSN 2840-00-113-6507
| Characteristic | Specifications |
|---|---|
| OVERALL WIDTH | 2.640 INCHES MINIMUM AND 2.760 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |