What was found
(CAN) PILOT REPORTED AIRFRAME VIBRATION WHEN POWER RETARDED DURING DESCENT (FROM 94 TO 88 PERCENT). ITT FLUCTUATING AS LOW AS 200 DEGREES. ENGINE N1 & N2 FLUCTUATES .5 TO 1.5 PERCENT DURING CRUISE WITH LOW BUZZING.UPON INSPECTION OF INLET, FOUND FOD DAMAGE ON 3 LP COMPRESSOR STATOR BLADE (2 BENT BLADE) REAR ACOUSTICLINER AROUND THE 12 O'CLOCK POSITION AND BLADE RUB STRIPE AROUND THE THE 10 O'CLOCK POSITION.