There is no AD or requirement to tear down.
No specific AD, but TCM does have their own requirements in their standard practices manual. I would recommend it with an unknown engine.
Standard Practice Maintenance Manual 6-153
30 May 2016 CHANGE 1
Engine Inspection and Service
6-5. Unscheduled Maintenance
6-5.1. Propeller Strike
A propeller strike is any incident (whether or not the engine is operating) in which the
propeller contacts a foreign object that 1)results in the necessity to repair the propeller
blade(s) (other than minor blade dressing) or 2)results in loss of engine RPM at the time of
contact. Propeller strikes can cause engine and component damage even if the propeller
continues to rotate. This damage can result in catastrophic engine failure.
WARNING
Do not attempt to dress a propeller blade without consulting
the propeller manufacturer's instructions. Stresses imposed on
the propeller are more concentrated in areas that are nicked
and cut. They may act as stress risers. Stress risers weaken the
blade and can eventually cause the blade to fracture.
In cases where a small foreign object such as a small stone, strikes the propeller during
operation, inspect and repair the propeller according to the propeller manufacturer’s
instructions. If foreign object damage requires removal of the propeller for repair(s)
perform the “Propeller Strike Inspection” in Section 6-5.1.1.
6-5.1.1. Propeller Strike Inspection
Following any propeller strike, disassemble and inspect all rotating engine components
prior to further flight; correct all unserviceable conditions. Inspect all engine driven
components according to the manufacturer’s instructions for continued airworthiness.
Procedure
1. Remove the propeller; inspect according to propeller manufacturer’s instructions.
2. Remove the engine from the aircraft according to the instructions in Section 5-1.
3. Disassemble the engine completely according to instructions in the primary ICA
(Ref: Section 1-1.1).
4. Regardless of condition, replace all counterweight pins, bushings, end plates and
snap rings. Replace all connecting rod nuts and bolts, regardless of condition.
5. Thoroughly clean the crankshaft according to instructions in Chapter 12; all
surfaces, especially those forward of the front main bearing, must be free of paint,
sludge, or any substance that may mask cracks.
6. Perform a “Magnetic Particle Inspection” on the crankshaft, connecting rods, gears
and remaining steel internal engine parts according to instructions in Section 11-3.
7. Strip the crankcase of all paint and clean the crankcase thoroughly according to
instructions in Chapter 12; all surfaces must be free of paint, sludge, or any
substance that may mask reliable inspection.
8. Perform a “Fluorescent Penetrant Inspection” on the crankcase according to
instructions in Section 11-2, paying particular attention to the forward crankcase
bearing support and adjacent structure.
9. Inspect the remainder of the engine according to the instructions in the primary ICA
(Section 1-1.1).
10. Perform the aircraft inspections required by the aircraft manufacturer.
11. Inspect all engine accessories according to the manufacturer’s instructions.
12. Assemble the engine according to instructions in the primary ICA (Section 1-1.1).
13. Install the engine in the aircraft according to the instructions in Section 5-2.