| AIRCRAFT LOCATION | WING,FAIRING UPPER,INBOARD STUB |
| AIRCRAFT MISSION DESIGN SERIES | C-17A |
| FABRICATION METHOD | LAMINATED AND COMPOSITE |
| MATERIAL DOCUMENT AND CLASSIFICATION | DMS2212 TYPE 1 MFR REF 1ST MATERIAL RESPONSE AND DMS2224 TYPE 1 CLASS W GRADE 5 MFR REF 2ND MATERIAL RESPONSE AND DMS2302 TYPE 2 CLASS 4 MFR REF 3RD MATERIAL RESPONSE |
| III MATERIAL | FIBER SYNTHETIC AND PLASTIC EPOXY AND ALUMINUM ALLOY 1145 |
| PROPRIETARY CHARACTERISTICS | NPAC |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| SPECIAL FEATURES | NHA 17P6W5325 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC SINGLE TREATMENT RESPONSE |
| SURFACE TREATMENT | PRIMER EPOXY |