First I would try to get feedbacks from the Cessna 182 owner/operators that operate with it; As any piece of equipment has its pros and cons you should get honest feedbacks (avoid SMA distributors/dealers since they may be biased).
When you ask them check for at least:
- Propeller reliability (can only handle composite props due to instanteneous torque),
- Exhaust system reliability,
- Crankcase reliability,
- Corrodability (worst if you live close to the ocean).
My recollection is that the basic engine has good reliability. If you go with it pay a lot of attention to cooling (oil and cylinders). Also, you should try to operate it in the mechanical mode ONLY and, only use the data acquisition and engine map modules of the ECU (avoid the servo'd part, many issues and un-necessary complexities); Get an output from the engine map module to create a gauge showing you the actual calculated power vs the maximum authorized calculated power for the conditions say in %; Keep the MP gauge as a sanity check and back-up; Then you will truly get a "Single Lever" as opposed to the current configuration in full ECU mode that requires a mode change lever (manual reversion); You really need to get rid of all the bull **** and hazards associated with the manual reversion mode (trust me, some of the failure cases are not pretty); BELL Helicopter learned the hard way (5 accidents with casualties) that automatic reversion is the only acceptable way to do reversion on engines; Manual reversion like the one offered by the SMA engine should be avoided at all costs.
Pay close attention to oil drainage at the governor. Avoid the negative g hardware (accumulators, etc.) that are required to comply with 23.943.