Part Details | AIRCRAFT GAS TURBINE ENGINE HEAT SHIELD
2840-01-368-5693 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: 1364M44G04, 1364M44G04, 1364M44G04, 2840-01-368-5693, 01-368-5693, 2840013685693, 013685693
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 04, 1992 | 01-368-5693 | 50356 ( SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-368-5693
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1364M44G04 | 51226 | ASSOCIATED AEROSPACE ACTIVITIES INC |
| 1364M44G04 | 60168 | ENGINETICS CORPORATIONDBA ENGINETICS AERO SPACE |
| 1364M44G04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-368-5693
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 7.300 INCHES MINIMUM AND 7.340 INCHES MAXIMUM |
| OVERALL WIDTH | 0.920 INCHES MINIMUM AND 0.960 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F110-14; ITEM FITS OVER TURBINE FRAME STRUT EDGE; IS FOLDED IN V-SHAPED |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT ENGINE |