THE PLT CLEARED SOME POWER LINES AND DESCENDED TO SPRAY A SUNFLOWER FIELD. THE ACFT DESCENDED UNTIL IT CONTACTED THE FLOWERS WITH THE LANDING GEAR. THE TALL FLOWERS DESTROYED THE LEADING EDGES OF THE ACFT WINGS AND THE LANDING GEAR. THE DRAG SLOWED THE ACFT BUT IT CONTINUED FLT TO AN ADJACENT FIELD WHERE IT LANDED ON THE FUSELAGE.
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
WHILE ASSISTING THE OWNER/OPERATOR WITH A PREVENTIVE MAINTENANCE OPERATION, A CRACK WAS DISCOVERED ON THE FRONT SIDE OF THE NR 1 CYLINDER MOUNT PAD AREA. THE CRACK, ALTHOUGH CLEARLY VISIBLE, WAS CONFIRMED WITH DYE PENETRANT. THE CRACK DID NOT APPEAR TO BE LEAKING OIL. THE CAUSE IS UNKNOWN AT THIS…
From FAA Service Difficulty Reports; matched by N-number and serial number.