Below is information from the Rotax installation and Heavy Maintenance Manual (Links at the bottom):
Pitting in the gearbox can lead to high-frequency vibrations, causing various issues as the vibration is transferred through the engine to connected parts. These problems include:
- Wear on the gearbox (gear profile and contact faces)
- Wear on external alternative accessories
- Wear on the exhaust system
- Leaking of the sealing surface of the crankcase
Note: Dynamic engine analysis units, commonly used for propeller adjustments, can detect this vibration. The normal vibration level for the engine ranges approximately between 1.27 cm and 2.45 cm per second. Alternatively, refer to the values specified by the aircraft manufacturer for the respective installation.
Please ensure to verify the moment of inertia for your propeller, adhering to the specified system limits:
- Minimum moment of inertia on propeller: 1500 kg cm2 (3.559 lb ft2)
- Maximum moment of inertia on propeller: 6000 kg cm2 (14.238 lb ft2)
It is necessary to conduct a dynamic balancing of the propeller as prescribed by the propeller manufacturer.
Visually inspect the dog hub for any visible pitting on the gear-tooth system or in the engagement faces of the dogs, referring to section 72-10-00 for wear limits (GB08).
Note: The cam peaks of the gear should never rest in the trough of the dog hub.
Measure the gap between the cam peak and the cam trough, referring to section 72-10-00 for wear limits (GB07).
Note: Slight to moderate traces of wear and pitting on the dogs are permissible.
https://www.rotax-owner.com/pdf/IM_912_iSeries_ED2_R1.pdf
https://www.rotax-owner.com/manuals/MMH_912i_Series_ED1_R3.pdf