| AIRCRAFT LOCATION | FRAME INSTL-SIDE FUSELAGE |
| AIRCRAFT STATION NUMBER | 247.00 |
| AIRCRAFT MISSION DESIGN SERIES | EH-60A |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250-13 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.0320 INCHES NOMINAL |
| III MATERIAL | ALUMINUM ALLOY 7075 |
| III PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET |
| PROPRIETARY CHARACTERISTICS | PACS |
| SPECIAL FEATURES | APPLICABLE TO NEXT ASSEMBLY P/N 70081-21206-012, 70083-02303-042, 70086-22117-042, AND 70211-85219-042 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-85582 MIL SPEC SINGLE TREATMENT RESPONSE AND SS8486 MFR REF SINGLE TREATMENT RESPONSE |
| SURFACE TREATMENT | PRIMER EPOXY |