As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FLAP AND PUSHER CAWS LIGHT ILLUMINATED AFTER TAKEOFF. PAGE 3-32 (A) OF PC12/45 POH REV 11 DATED MARCH 1ST, 2003 INDICATES POSSIBLE FLAP ASYMMETRY PAGE 7-5 OF PC12/45 POH REV 11 DATED MARCH 1ST 2003, THE ASYMMETRY MAY BE IN EXCESS OF 2 DEGREES. RESET FLAP CONTROL WARNING UNIT. MALFUNCTION COULD NOT BE DUPLICATED. (K)