Ron Levy said:
The engine manufacturers provide guidelines, but there are no FAA regs on the subject, other than those which make the guidelines mandatory for 135 and 121 operators. For Lycoming engines, see Lycoming Service Letter L163C, an unofficial copy of which you can find at
http://www.prime-mover.org/Aviation/Bulletins/sl163.html and an official copy of which you can get faxed to you
free by calling Lycoming at 570-323-6181 from 8 AM to 5 PM (Eastern Time) Monday – Friday.
Generally speaking, a teardown is recommended if any part of the prop came off or if the engine was stopped by whatever it hit ("sudden stoppage"). If the engine kept running and the prop is still in one piece, a teardown is more dependent on the judgement of the mechanic that examines it. Usually they'll check the prop track, and if it's still true, will not tear down the engine. Keep in mind that in most cases, the teardown is covered by insurance if you have an accidental prop strike, and the insurance company would rather pay for a precautionary teardown than the results of a later engine failure.
Please read:
2004-10-14 Lycoming Engines (formerly Textron Lycoming):
Amendment 39-13644. Docket No. 89-ANE-10-AD. Supersedes AD 91-14-22, Amendment 39-6916.
Effective Date
(a) This AD becomes effective June 25, 2004.
Affected ADs
(b) This AD supersedes AD 91-14-22.
Applicability
(c) This AD applies to Lycoming Engines (formerly Textron Lycoming), direct-drive reciprocating engines (except O-145, O-320H, O-360E, LO-360E, LTO-360E, O-435, and TIO-541 series engines).
Unsafe Condition
(d) This AD results from a change to the definition of a propeller strike or sudden stoppage. The actions specified in this AD are intended to prevent loosening or failure of the crankshaft gear retaining bolt, which may cause sudden engine failure.
Compliance
(e) Compliance with this AD is required as indicated before further flight if the engine has experienced a propeller strike as defined in paragraphs (i) and (j) of this AD, unless already done.
(f) Inspect, and if necessary repair, the crankshaft counter bored recess, the alignment dowel, the bolt hole threads, and the crankshaft gear for wear, galling, corrosion, and fretting in accordance with steps 1 through 5 of Lycoming Mandatory Service Bulletin (MSB) No. 475C, dated January 30, 2003.
(g) Remove the existing gear retaining bolt and lockplate from service, and install a new bolt and lockplate, in accordance with steps 6 and 7 of Lycoming MSB No. 475C, dated January 30, 2003.
Prohibition of Retaining Bolt and Lockplate
(h) Do not install the gear retaining bolt and lockplate that were removed in paragraph (g) of this AD, into any engine.
Definition of Propeller Strike
(i) For the purposes of this AD, a propeller strike is defined as follows:
(1) Any incident, whether or not the engine is operating, that requires repair to the propeller other than minor dressing of the blades.
(2) Any incident during engine operation in which the propeller impacts a solid object that causes a drop in revolutions per minute (RPM) and also requires structural repair of the propeller (incidents requiring only paint touch-up are not included). This is not restricted to propeller strikes against the ground.
(3) A sudden RPM drop while impacting water, tall grass, or similar yielding medium, where propeller damage is not normally incurred.
(j) The preceding definitions include situations where an aircraft is stationary and the landing gear collapses causing one or more blades to be substantially bent, or where a hanger door (or other object) strikes the propeller blade. These cases should be handled as sudden stoppages because of potentially severe side loading on the crankshaft flange, front bearing, and seal.