| AIRCRAFT LOCATION | NACELLE |
| AIRCRAFT MISSION DESIGN SERIES | CH-53A/D/E |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/11 ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.080 INCHES NOMINAL |
| III MATERIAL | ALUMINUM ALLOY 7075 |
| III PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET,CAMLOC RECEPTACLE (LOWER FWD NACELLE) |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL LENGTH | 2.00 INCHES NOMINAL |
| OVERALL WIDTH | 2.00 INCHES NOMINAL |
| SPECIAL FEATURES | NEXT HIGHER ASSEMBLY 21C0882-1,65202-03059-014,CH/MH-53E;USE ON CH-53E AND MH-53E |