This document describes the installation of fuel tank, piping, glow plug, fuel, and names of engine parts. It includes the Type 70A Carburetor, Cylinder Head, Drive Hub, Safety Lock-nut Assembly, Silicone Tubing, Crankcase, Needle Valve Cover Plate, PD-06 Fuel pump, etc.
This document provides general operating instructions and safety warnings for the O.S. max-1L40RX internal combustion engine. It emphasizes that the engine is designed specifically for model aircraft and should not be used for other purposes. Key safety points include using only the supplied silencer, ensuring propeller blades face forward, and avoiding enclosed spaces due to carbon monoxide risks.
The manual details installation procedures, including securing the engine with appropriate screws and locknuts, managing throttle linkage to prevent stalling, and installing a tuned silencer. It also covers fuel tank setup using specific tubing and pick-up weights, as well as glow plug considerations.
| Displacement | 23.0cc (1.404 cu.in.) |
|---|---|
| Practical R.P.M. | 4,800~10,000 r.p.m. |
| Power Output | 3.5PS/9,000 r.p.m. |
| Bore | 32.0mm (1.260 in.) |
| Stroke | 28.6mm (1.126 in.) |
| Weight | 830g (29.3oz) |
The displacement is 23.0cc (1.404 cu.in.).
The practical RPM range is from 4,800 to 10,000 r.p.m.