Sensenich Propeller Mfg. Co.
Approved Techniques For Repair Of Blade Damage

The following examples of aluminum propeller damage are to be used as a benchmark for what repairs should be performed by a certified mechanic, in the field. If the finished repairs would be greater than those shown below, the propeller should be removed and sent to an FAA approved repair facility.

Re-pitch of a fixed-pitch propeller may be beneficial only if the propeller will be installed on an airplane significantly faster or slower than the one for which It was originally purchased, or when the airplane's principal base of operation is changed (for example, to a much higher elevation - requiring compromise for take-off & climb at the expense of cruise) . If re-pitch is necessary then the rules given here should be followed.

1) Because a verifiable record of a propeller's history is usually not available, study the stamping in the hub for evidence of previous re-pitching (possibly shown by overstamping). Previous re-pitching may also be indicated by a wavy appearance of the trailing edge between the 30% and 45% blade radius stations.
2) Propeller pitch must remain within the pitch range shown in SCRM 478 for the propeller series. Also, re-pitching of an aluminum propeller shall not exceed 8 inches, minus the difference between its initial pitch and the median pitch. For example, a SENSENICH 76EM8-0-63 (median pitch 60) may be set to 66 inches pitch, however; it will then be permissable to reduce pitch no further than to 64. The same propeller (originally a 76EM8-0-63) may be twisted to 58 pitch if it had not been previously set to a higher pitch.

3) No twisting shall be accomplished at a blade section which is greater than 1.100 inches thick.

4) Twists to change pitch should not be made at the same radius location more than one time. Large twists in a blade should be made in several steps at locations between 30% and 45% blade radius.


SENSENICH CORPORATION
Robert E. Bristol
Propeller Engineering Manager