RDM14: OUTBOARD ENGINE.
The OUTBOARD ENGINE is a the manufacturer industrial component. Key specifications include fuel_type: GASOLINE, features_provided: GEAR REDUCTION AND INTEGRAL REVERSE GEAR, reduction_gear_ratio: 12TO21, propeller_blade_pitch: 10.000 INCHES NOMINAL IN, propeller_blade_diameter: 11.000 INCHES NOMINAL IN, nondefinitive_spec/std_data: II TYPE AND B CLASS. This part is cataloged in the U.S.
Government catalog under NSN 2805-00-056-8211, 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.
| fuel_type | GASOLINE |
| cylinder_quantity | 2 |
| features_provided | GEAR REDUCTION AND INTEGRAL REVERSE GEAR |
| reduction_gear_ratio | 12TO21 |
| propeller_blade_pitch | 10.000 INCHES NOMINAL IN |
| propeller_blade_diameter | 11.000 INCHES NOMINAL IN |
| propeller_blade_quantity | 3 |
| nondefinitive_spec/std_data | II TYPE AND B CLASS |
| NSN | 2805-00-056-8211 |
| PROPELLER BLADE DIAMETER | 11.000 INCHES NOMINAL IN |
| PROPELLER BLADE QUANTITY | 3 |
| REDUCTION GEAR RATIO | 12TO21 |
| FUEL TYPE | GASOLINE |
| FEATURES PROVIDED | GEAR REDUCTION AND INTEGRAL REVERSE GEAR |
| NONDEFINITIVE SPEC/STD DATA | II TYPE AND B CLASS |
| SPECIAL FEATURES | VERTICAL IN-LINE, 2.875 IN. BORE DIA, 2.750 IN. STROKE LG, CARBURETOR FUEL INDUCTION, MAGNETO IGNITION, AUTOMATIC REWIND STARTER ROPE, ELECTROMAGTIC INTERFERENCE SUPPRESSION PROVIDED, POWER TRANSMITTED FROM VERTICAL DRIVE SHAFT THROUGH HEAVY DUTY REDUCTION GEARS TO HORIZONTAL PROPELLER SHAFT, FORWARD AND REVERSE OPERATION, W/SEPARATE FUEL TANK, 6 GALLON CAPACITY, W/CARRYING HANDLE AND FUEL GAGE, W/CHEST PROVIDED W/SKIDS IN |
| CYLINDER QUANTITY | 2 |
| PROPELLER BLADE PITCH | 10.000 INCHES NOMINAL IN |