| AIRCRAFT LOCATION | THROTTLE CONTROL FORWARD AND CENTER FUSELAGE |
| AIRCRAFT MISSION DESIGN SERIES | F-4 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-S-763 FED SPEC 1ST MATERIAL RESPONSE AND QQ-A-601 FED SPEC 2ND MATERIAL RESPONSE |
| III MATERIAL | STEEL CORROSION RESISTING AND ALUMINUM ALLOY |
| PROPRIETARY CHARACTERISTICS | NPAC |
| OVERALL LENGTH | 10.802 INCHES MINIMUM AND 10.866 INCHES MAXIMUM |
| OVERALL WIDTH | 3.990 INCHES MINIMUM AND 4.010 INCHES MAXIMUM |
| SPECIAL FEATURES | MANUFACTURER SUGGESTED NAME-THROTTLE BOX AND TORQUE SHAFT ASSEMBLY;SHAFT HAS EXPANDABLE TRAVEL OF UP TO 4.500 INCHES |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MACSPEC32-90000 MFR REF ALL TREATMENT RESPONSES |
| SURFACE TREATMENT | PAINT |