| AIRCRAFT LOCATION | FRAME INSTL-SIDE FUSELAGE |
| AIRCRAFT STATION NUMBER | 265.50 |
| AIRCRAFT MISSION DESIGN SERIES | EH-60A |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250-13 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.0630 INCHES NOMINAL |
| III MATERIAL | ALUMINUM ALLOY 7075 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CHANNEL |
| PROPRIETARY CHARACTERISTICS | PACS |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC SINGLE TREATMENT RESPONSE AND SS8486 MFR REF SINGLE TREATMENT RESPONSE |
| SURFACE TREATMENT | PRIMER EPOXY |