What was found
FOUND .50 INCH CRACK IN STIFFENER ON RIB, PIPER PN 40423-13. REPAIRED IAW AC43.13. CRACK IS LOCATED ADJACENT TO WHEEL BUMPER IN UPPER WHEELWELL AND SUSPECT WAS CAUSED BY FATIGUE FROM GEAR RETRACTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND .50 INCH CRACK IN STIFFENER ON RIB, PIPER PN 40423-13. REPAIRED IAW AC43.13. CRACK IS LOCATED ADJACENT TO WHEEL BUMPER IN UPPER WHEELWELL AND SUSPECT WAS CAUSED BY FATIGUE FROM GEAR RETRACTION.