| AIRCRAFT LOCATION | BALANCE PANEL ELEVATOR,AFT RUDDER |
| AIRCRAFT MISSION DESIGN SERIES | KC-135 AIRCRAFT |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5000 MIL SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 2.10 INCHES NOMINAL |
| MATERIAL | STEEL |
| III PART NAME ASSIGNED BY CONTROLLING AGENCY | TRACK GRIP |
| PROPRIETARY CHARACTERISTICS | PACS |
| OVERALL LENGTH | 2.70 INCHES NOMINAL |
| OVERALL WIDTH | 2.20 INCHES NOMINAL |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416 ASSN STD SINGLE TREATMENT RESPONSE |
| SURFACE TREATMENT | CADMIUM |