NSN 4430-01-320-7525
Part Details | ELECTRIC THERMAL DRYING OVEN
4430-01-320-7525 An oven capable of maintaining and confining heat intensities within close limits. It is designed to be used for aging, baking, curing, drying, heating and/or testing various mechanical equipment or substances.
Alternate Parts: 443041136367, 4430-4113-6367, DC366ASGHP, DC-366A-SGHP, 4430-01-320-7525, 01-320-7525, 4430013207525, 013207525
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
44 | JUN 02, 1990 | 01-320-7525 | 12824 ( OVEN, THERMAL DRYING, ELECTRIC ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4430-01-320-7525
Part Number | Cage Code | Manufacturer |
---|---|---|
4430-4113-6367 | 99998 | DEFENSE SUPPLY CENTER RICHMONDINDUSTRIAL PLANT EQUIPMENT /DLA/ |
DC-366A-SGHP | 89715 | SPX CORPORATION |
Technical Data | NSN 4430-01-320-7525
Characteristic | Specifications |
---|---|
CIRCULATION METHOD | FORCED |
WORK PROTECTION FROM HEAT SOURCE | COMPLETE |
WATTAGE RATING | 27.0 KILOWATTS |
CURRENT TYPE | AC |
VOLTAGE IN VOLTS | 480.0 |
FREQUENCY IN HERTZ | 60.0 |
PHASE | THREE |
MAXIMUM OPERATING TEMP | 600.0 DEG FAHRENHEIT |
NORMAL OPERATING TEMP RANGE | +1.0 TO +600.0 DEG FAHRENHEIT |
TEMP CONTROL METHOD | AUTOMATIC |
INSIDE WIDTH | 36.000 INCHES NOMINAL |
INSIDE DEPTH | 36.000 INCHES NOMINAL |
INSIDE HEIGHT | 48.000 INCHES NOMINAL |
OVERALL WIDTH | 67.000 INCHES NOMINAL |
OVERALL DEPTH | 54.000 INCHES NOMINAL |
OVERALL HEIGHT | 86.000 INCHES NOMINAL |
CABINET DOUBLE WALL CONSTRUCTION | PROVIDED |
INSULATED CABINET | PROVIDED |
CABINET DOOR QUANTITY | 1 |
CABINET EXHAUST VENT | PROVIDED |
ADJUSTABLE OPENING | PROVIDED |
CABINET FRESH AIR INTAKE | PROVIDED |
FRESH AIR INTAKE ADJUSTABLE OPENING | PROVIDED |
SPECIAL FEATURES | SIMILAR TO P/N DC-366A-FHP-1,BUT SPECIAL ORDERED WITH STAINLESS STEEL INTERIOR; USE OF SILLICONE RUBBER FOR DOOR AND OTHER SEALS ATTACHED WITH SILICONE SEALANT IN HEATING CHAMBER IS ACCEPTABLE |
FUNCTIONAL DESCRIPTION | USED TO CURE ADHESIVES AND SEALANTS AND TO DRY PREPARED BONDING SURFACES DURING REPAIR OF THE F-15 AFCT LINE REPLACEABLE UNIT CHASSIS AND CIRCUIT CARD ASSEMBLIES |