As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ON APPLICATION OF POWER IN CLIMB, THE ENGINE EXPERIENCED A COMPRESSOR STALL ACCOMPANIED BY AN UNCOMMANDED POWER REDUCTION, PARAMETER FLUCTUATIONS AND A FADEC FAULT INDICATION. SUBSEQUENT INVESTIGATION LED TO REPLACEMENT OF THE ENGINE INLET GUIDE VANE ACTUATOR. (TC NR 20070314018)