NSN 4920-01-444-4181
Part Details | AIRCRAFT COMPOSITE REPAIR MOLD
4920-01-444-4181 A contoured fixture designed to facilitate the layup, forming, and curing of composite aircraft skin sections.
Alternate Parts: CTII2535MPC, CTII-2535-MPC, 4920-01-444-4181, 01-444-4181, 4920014444181, 014444181
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 49 | MAY 06, 1997 | 01-444-4181 | 51945 ( MOLD, COMPOSITE REPAIR, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4920-01-444-4181
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CTII-2535-MPC | 3J847 | CPI RADANT TECHNOLOGIES DIVISIONINC. |
Technical Data | NSN 4920-01-444-4181
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 84.000 INCHES NOMINAL |
| OVERALL WIDTH | 84.000 INCHES NOMINAL |
| OVERALL HEIGHT | 108.000 INCHES NOMINAL |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | MOLD IS LAYED UP WITH QUARTZ MATERIAL AND CURED IN AN AUTOCLAVE;MANUFACTURED FROM AN EPOXY/FIBERGLASS COMPOSITE, LAYED UP IN THE OML MOLD USING A WAX SHEET OFFSET |
| SPECIAL FEATURES | 1500LBS |
| END ITEM IDENTIFICATION | MC-130H |
| FUNCTIONAL DESCRIPTION | THIS MOLD IS REQUIRED TO FABRICATE REPLACEMENT COMPONENT PIECES FOR REPAIR OF DAMAGE TO THE INTERMEDIATE SKININ CLASS IV REPAIRS; USED TO FABRICATETHE COMPLETE OR SECTIONS OF THE INTERMEDIATE SKIN |
| REFERENCE DATA AND LITERATURE | SERD NO. 6119; TO 35D8-7-4-1 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | INTERMEDIATE SKIN MOLD |