NSN 4920-01-444-4183
Part Details | AIRCRAFT COMPOSITE REPAIR MOLD
4920-01-444-4183 A contoured fixture designed to facilitate the layup, forming, and curing of composite aircraft skin sections.
Alternate Parts: CTII2540MPC, CTII-2540-MPC, 4920-01-444-4183, 01-444-4183, 4920014444183, 014444183
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 49 | MAY 06, 1997 | 01-444-4183 | 51945 ( MOLD, COMPOSITE REPAIR, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4920-01-444-4183
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CTII-2540-MPC | 3J847 | CPI RADANT TECHNOLOGIES DIVISIONINC. |
Technical Data | NSN 4920-01-444-4183
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 84.000 INCHES NOMINAL |
| OVERALL WIDTH | 84.000 INCHES NOMINAL |
| OVERALL HEIGHT | 108.000 INCHES NOMINAL |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | THE USEFUL LIFE OF THE MOLD TO BE40 CYCLES THROUGH THE AUTOCLAVE |
| SPECIAL FEATURES | MANUFACTURED FROM AN EPOXY/FIBERGLASS COMPOSITE, LACED UP IN THE OML MOLD USING A WAX SHEET OFFSET; 1500LBS |
| END ITEM IDENTIFICATION | MC-130H |
| FUNCTIONAL DESCRIPTION | THIS MOLD IS REQUIRED TO FABRICATE REPLACEMENT COMPONENT PIECES FOR REPAIR OF DAMAGED TO THE NOSE |
| REFERENCE DATA AND LITERATURE | SERD NO. 6120; TO 35D8-7-4-1 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | INNER SKIN MOLD |