From AC20-37E
e. Blade Polishing. The FAA receives frequent inquiries from airplane owners and maintenance personnel asking whether it is acceptable to polish propeller blades. It is almost always not acceptable. Corrosion protection such as paint and anodize should not be removed from the surface of a propeller blade. Propeller blades must be maintained to the type design. If the original design had corrosion protection and the instructions for continued airworthiness call for corrosion protection, then the corrosion protection should be maintained to those instructions.
See anything forbidding it?
Ac35,4-1
4. DISCUSSION. The propeller type certification process requires the applicant to prepare ICA. The ICA provide information for proper maintenance that ensures that propellers of that type design are airworthy. For the purposes of this AC, a propeller is considered airworthy when it meets the following two conditions:
a. The propeller conforms to its type certificate (TC). A propeller conforms to its TC when the propeller configuration is consistent with the type design and other data that is part of the TC, as well as other approved data such as that related to repairs, modifications, or alterations.
b. The propeller is in a condition for safe operation. A propeller is in a condition for safe operation when factors such as wear, damage, and deterioration do not prevent the propeller from demonstrating compliance with those requirements of part 35 that relate to the safe operation of the propeller and do not result in an unsafe condition to the aircraft. This means, for example, that a propeller in a condition for safe operation should still comply with the centrifugal load requirements of §35.35.
IMHO, polishing a prop depends upon if it will meet its type design when polished.
the TCDS for the 1A102OCM 6948
P-918.pdf
Anyone know where to find "the type design" for the 1A102?