519892-4: MOTOR,ENGINE STARTER,ELECTRICAL.
MOTOR,ENGINE STARTER,ELECTRICAL. Key specifications include current_type: DC OUTPUT, overall_width: 2.240 INCHES IN, spline_length: 0.050 INCHES MINIMUM AND 0.053 INCHES MAXIMUM SINGLE END IN, cooling_method: NONVENTILATED, overall_height: 3.200 INCHES IN, overall_length: 7.275 INCHES IN. This part is cataloged in the U.S.
Government catalog under NSN 2920-01-112-9308, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| current_type | DC OUTPUT |
| overall_width | 2.240 INCHES IN |
| spline_length | 0.050 INCHES MINIMUM AND 0.053 INCHES MAXIMUM SINGLE END IN |
| cooling_method | NONVENTILATED |
| overall_height | 3.200 INCHES IN |
| overall_length | 7.275 INCHES IN |
| shaft_diameter | 0.099 INCHES MINIMUM AND 1.010 INCHES MAXIMUM SINGLE END IN |
| mounting_method | RIGID RING |
| enclosure_feature | OPEN PROTECTED |
| spline_minor_diameter | 0.339 INCHES MINIMUM AND 0.342 INCHES MAXIMUM SINGLE END IN |
| end_item_identification | APU-A10 AIRCRAFT; USED ON GTCP36-50 |
| inclosure_specification | MIL-STD-108 |
| NSN | 2920-01-112-9308 |
| MOUNTING FACILITY TYPE AND QUANTITY | 4 UNTHREADED HOLE(S) |
| SPLINE MINOR DIAMETER | 0.339 INCHES MINIMUM AND 0.342 INCHES MAXIMUM SINGLE END IN |
| SHAFT DIAMETER | 0.099 INCHES MINIMUM AND 1.010 INCHES MAXIMUM SINGLE END IN |
| CURRENT TYPE | DC OUTPUT |
| OVERALL LENGTH | 7.275 INCHES IN |
| MOUNTING METHOD | RIGID RING |
| SPLINE LENGTH | 0.050 INCHES MINIMUM AND 0.053 INCHES MAXIMUM SINGLE END IN |
| COOLING METHOD | NONVENTILATED |
| SHAFT ROTATION DIRECTION | CLOCKWISE SINGLE END |
| CONNECTION TYPE AND VOLTAGE RATING IN VOLTS | 18.500 LINE TO NEUTRAL SINGLE OUTPUT |