TM-9-2815-205-24 Technical Manual for M113 Engine 6V53 6V53T Download
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Table 1. Repair Specifications List - Continued. (1) POINT OF MEASUREMENT (2) NEW MINIMUM INCHES (MM) (3) NEW MAXMUM INCHES (MM) (4) WEAR LIMIT INCHES (MM) Thrust plate to thrust washers 0.0025 (0.06) 0.0050 (0.13) * Rotor to air outlet side of housing 0.0040 (0.10) * Rotor to air inlet side of housing 0.0100 (0.25) * Rotor to front end plate (turbocharged) 0.0100 (0.25) * Rotor to front end plate (nonturbocharged) 0.0080 (0.20) * Rotor to rear end plate (turbocharged) 0.0120 (0.30) * Rotor to rear end plate (nonturbocharged) 0.0100 (0.25) * Rotor to rotor (turbocharged) 0.0130 (0.33) * Rotor to rotor (nonturbocharged) 0.0090 (0.23) * OIL PUMP Lobe clearance (inner and outer rotors) 0.0005 (0.01) 0.0110 (0.28) * Clearance (pump body to side of inner and outer rotor) 0.0010 (0.03) 0.0035 (0.09) * FUEL INJECTOR Follower spring load at 1.028 inches (26.11 mm) (length) 70 lb (31.75 kg) * Valve spring load at 0.4358 inches (11.07 mm) (length) 41 lb (18.60 kg) * END OF WORK PACKAGE TM 9-2815-205-24 0106 0106-10